Title of Invention	"METHOD OF CONSTRUCTION OF MODULED PRODUCTS"
Abstract	A method of construction of a moulded product which includes the steps of impregnating non-metallic fibres in epoxy resin whereby said impregnated fibres may be placed to form a sheet of said fibres; cutting a plurality of pre-pregs from said sheet; forming successive layers of said pre-pregs so that said layers are placed in stacked relationship (preferably formed of pre-pregs having fibres placed in an intersecting orientation which alternate with pre-pregs having fibres placed in a longitudinal and/or latitudinal orientation) in a mould cavity of a compression mould; compression moulding at elevated temperature; and removing the moulded product from the compression mould. There is also provided a moulded product per se as well as a moulded product formed by the method of construction. The moulded product is preferably a prosthetic device including a J-shaped pylon (11) and sole plate (23)

Title of Invention

"METHOD OF CONSTRUCTION OF MODULED PRODUCTS"

Abstract

A method of construction of a moulded product which includes the steps of impregnating non-metallic fibres in epoxy resin whereby said impregnated fibres may be placed to form a sheet of said fibres; cutting a plurality of pre-pregs from said sheet; forming successive layers of said pre-pregs so that said layers are placed in stacked relationship (preferably formed of pre-pregs having fibres placed in an intersecting orientation which alternate with pre-pregs having fibres placed in a longitudinal and/or latitudinal orientation) in a mould cavity of a compression mould; compression moulding at elevated temperature; and removing the moulded product from the compression mould. There is also provided a moulded product per se as well as a moulded product formed by the method of construction. The moulded product is preferably a prosthetic device including a J-shaped pylon (11) and sole plate (23)

Full Text	TITLE "METHOD OF CONSTRUCTION OF MOULDED PRODUCTS" FIELD OF THE INVENTION THIS INVENTION relates to a method of construction of moulded products and moulded products constructed by the method. In particular, the invention relates to a method of construction of prosthetic devices and the specification will now describe in detail by way of example a method of construction of prosthetic devices although it should not be limited to this particular example. BACKGROUND ART In the past 15 years, there have been an increasing number of lower-limb amputees who have desired to enhance their quality of life by being able to have access to an affordable prosthesis that will provide not only basic mobility but which will also encourage and permit participation in low- to high-impact activities in the same manner as enjoyed by non-amputees. Numerous technological advances in the field of prosthetics have allowed this to happen and have provided a wide range of prosthetic legs to choose from. In coalition with the general type of prosthesis for normal gait activities, such as basic ambulant walking and work type activities, there has been a demand by amputees for prostheses that can enable them to lead a more active lifestyle and, thus, improve their quality of life. There has been much effort within the prosthetic industry to develop a lightweight and durable prosthesis that will allow amputees to participate in strenuous career options, such as laboring, farm work, etc, and various medium- to high-level activities, such as jogging, squash, climbing, tennis, etc, and very high-impact sports, such as running, sprinting, jumping, basketball and volleyball. Numerous different prostheses have been developed, each trying to replicate the function and appearance of the replaced body part. Lower leg prostheses present unique problems. They must be strong enough to support a person's weight and activity level and to withstand the forces encountered through gait movement. As a result, some prostheses developed in the past were very heavy and rigid and restricted the wearer's activity level, career, recreational and sport options. There are a number of different composite foot and leg prosthetic devices that have now been proposed, most of which utilize modern composite material technology to impart energy storage and release during use. Examples of prosthetic foot devices that have been fabricated with composite materials, with the intention of storing energy when the foot is placed on the ground and to release it and provide a lift or thrust as the foot is removed from the ground to aid in the patient's gait are disclosed in Abrogast et al. US Patent No 4,865,612, concerning an artificial foot having a pair of thin forwardly extending spring members connected to a keel and Shorter et al. US Patent No 5,116,383. US Patent No 5,116,383 describes an energy storing foot having a single piece carbon fibre reinforced keel having a lower spring portion connected at its posterior end as a cantilever to an upper ankle mounting portion. The energy storing foot is combined with a resilient ankle joint of the ball and socket type. Other lower leg prosthetic devices in the prior art have employed springs, including multiple leaf springs or flat spring-like members, in an attempt to approximate the response and performance of a natural foot. Examples include Merlette US Patent No 4,959,073 and Phillips US Patent No 4,547,913,4,822,363 and 5,776,205. An example of the abovementioned lower leg prosthetic device is a prosthesis known as the Flex-Foot, which provides a composite strut and foot configuration, which is specifically described in US Patent No 4,547,913. The spring-like action imparted by the materials used in such devices results in additional mobility and comfort to the wearer. Prior art prosthetic feet that utilize a plurality of springs, such as in Phillips US Patent No 5,776,205, tend to rock under vertical load as the load is distributed separately to the springs. Furthermore, the dynamic feet of the Flex-Foot system that are commercially available, do not have rigid ankle joints. However, this system embodied a rearward separate heel segment or heel portion secured to the main body of the foot, at the mid foot. While this system provides better performance than the former prostheses, this system embraces a plurality of components and joints which are less than optimum for transference of energy from heel strike through to toe-off because of the rearward heel segment deficiency of transmission of continual energy from a separate heel plate through to a separate toe portion on the J-pylon as described in US Patent No 4,822,363 and/or a full sole member described in US Patent No 5,976,191, This is because of the necessity to incorporate additional support members or increase in pylon thickness, which is necessary to provide suitable wearer support and prosthesis performance. Prior art prosthetic feet with a separate heel spring member and/or foam/rubber resilient material placed between foot and sole member tend to absorb vertical load either in the spring member or in the foam/rubber resilient material and, thus, dissipates the transfer of constant energy from heel strike to toe-off. US Patent Nos 4,822,363 and 4,547,913 refer specifically to a J-shaped pylon made from the composite material connected to a flat spring-like rearward heel plate. US Patent No 4,959,073 refers to a J-shaped pylon made from the composite material that is integrally formed with a heel member. Reference also may be made to US Patent No 5,037,444, which refers to a prosthetic foot made from the composite material alternatively known as the so-called "Seattle Foot". These devices make great advances in gait movement and activity levels and have a higher strength and stiffness to weight ratio of graphite to other materials, which results in almost complete return of input or stored energy, lighter weight, higher fatigue strength, and minimal creep. However, these devices also possess some disadvantages. For example, because of the higher strength and stiffness to weight ratio of graphite as compared to other materials, local stiffness, jolting and braking occurs because of material lay-up fabrication methods, which interferes with smooth and even flexing of the components during the wearer's stride. Furthermore, while substantially lighter in weight, they have an inherent rigidity because of the higher tensile strength resulting in greater stiffness to weight ratio of graphite to other material and also have areas more prone to fatigue stress failure. Prior art prosthetic feet that utilize a spring-loaded heel which operates on a spring separate from a spring in the toe section, such as in the Phillips and Merlette patents discussed above, effectively store energy in the heel, but are ineffective in transferring the energy from the heel to the toe portion of the prosthetic foot as the foot rolls forward during the gait cycle. These devices still require separate loading of a spring in the toe section. As a result, wearers notice a distinct and unnatural lag or hesitation in rolling the foot forward during the gait cycle, giving the foot an unnatural feel and causing an uneven stride. Some prior art prosthetic feet, such as the devices of Phillips US Patent Nos 4,547,913 and 4,822,363, can accommodate torsion movement about the longitudinal axis of the shin portion, but the shape of the shin portion is designed for spring strength and breaking strength, not torsion movement. The prior art devices of US Patent Nos 4,547,913,4,822,363 and 4,959,073 and others are made up exclusively from a composite material comprising high strength graphite filaments in a high-toughness epoxy thermosetting resin, constructed from uni-directional (UD) longitudinal fibres in their main core with woven latitudinal or woven angular fibres on their outer layers to improve their torsion strength. The latitudinal or angular woven materials come in the form of woven sleeves. These woven sleeves can easily slide over and cover the UD longitudinal fibres that are in the main core. These outer layers are woven sleeves and all their fibre filaments are continuous from start to finish. If this was not the case, it would not be possible to weave these filaments into a woven sleeve. Usually, the main core and the woven sleeves were formed by a number of plies or laminae that were placed in a rigid mould shaped to the final configuration and, subsequently, cured. This provides a result wherein each of the continuous filaments extend uninterrupted through an upper extremity, shin portion and foot portion of the prosthesis or from the top of leg portion downwardly through the ankle section, across the top of the foot or toe portion. Also, the heel plate and/or sole member have continuous filaments that extend uninterrupted from front extremity to heel extremity ie. all fibre filaments are continuous and uninterrupted longitudinally, latitudinal or angularly in their constructions. Similar construction methods are described in US Patent Nos 5,037,44, 5,156,631, 5,181,933, 5,493,456, 5,514,185 and 6,071,313. Such construction methods have the following disadvantages, ie: (a) It was necessary to thicken the upper extremity of the pylon to provide a rigid upper extremity. This may also be accomplished by expanding the width of said upper extremity; (b) It was important to increase the number of plies or laminae and, thus, the thickness of the pylon to accommodate users as their weight or activity level increases; (c) Additional laminates were added to maintain strength as the width of the pylon is reduced; (d) It was considered important to achieve a gradual reduction in the thickness of the pylon in the various dynamic areas thereof such that the foot portion is reduced in thickness compared to the ankle portion, and the ankle portion is reduced in thickness compared to the shin portion. The number of plies or laminations or layers varies in the different sections. As a consequence of (a), (b), (c) and (d) above, it was a general expectation from conventional methods of construction of prostheses as described above that, depending on the foot size and strength needed in a particular prosthesis, the number of plies employed can be increased or decreased as required. For example, fewer laminations may be required for a smaller prosthesis, or a prosthesis for a lightweight individual. A larger prosthesis, or a prosthesis for a heavier individual, may require more laminations. It was considered generally desirable to employ as few laminations as are needed for strength and stiffness to keep the prosthesis as light weight as practicable. From the discussion of prior art methods of construction above, it was necessary in the conventional manufacturing process to provide a plurality of different moulds or provide changes in mould cavity dimensions when additional plies or laminae were used to increase thicknesses or widths of prostheses. In other words it was necessary to use different mould cavity dimensions to correspond to different weights or different weight categories of prosthesis. The necessity of different thicknesses or widths was necessary to provide a variety of prostheses with different dimensions, thereby providing a disparity of thicknesses or widths to accommodate variations of pliability rates to support different exoskeleton and endoskeleton frames, body types and activity requirements of amputees. OBJECT OF THE INVENTION It has now been found that the above deficiencies of conventional manufacturing processes of conventional prostheses may now be reduced or overcome by the advent of the present invention where variations in requirements of individual users inclusive of amputees can be obtained by a process, as described hereinafter, which has the capability to make prosthesis inclusive of prostheses having a range of different weights or different weight categories in a single dimensional cavity mould, thus, making the process not only more efficient, but also less expensive. SUMMARY OF THE INVENTION In one aspect of the invention, there is provided a method of construction of a prosthesis for patients of various weight categories, , said method including the steps of: (a) impregnating non-metallic fibres in a thermosetting resin whereby said impregnated fibres are arranged to form a sheet of said fibres; (b) folding the sheet by bending adjoining parts of the sheet along adjacent fold lines therebetween so that said fibres are arranged in an intersecting orientation to form a prepeg having a double layer of fibres in different planes with the fibres in each layer having a different angle of orientation to a longitudinal axis of the prepeg; (c) cutting a plurality of pre-pegs from said sheet formed in step (b); (d) forming layers of said pre-pegs obtained from step (c) so that said layers are arranged in stacked relationship in a mould cavity of a compression mould whereby the mould cavity has a constant volume for each of the various weight categories; (e) compression moulding at elevated temperature; and (f) removing the prosthesis from the compression mould. In step (a) although the sheet can be produced by either solution drum winding or a hot melt technique as hereinafter described, it is preferable to use the drum winding technique so as to provide an intermediate composite sheet formed of the fibres supported on a sheet of release paper, whereby upon removal of the release paper, the final sheet formed by step (a) is obtained after cutting the intermediate sheet as it is supported on the drum. Preferably all of the fibres in the sheet are oriented in the same or similar direction and thus may be described as unidirectional (UD), In an alternative hot melt technique which may be used instead of the solution drum winding as described above in step (a) the pre-peg formed using said technique has fibers that are continuous and that are laid onto a continuous sheet of release paper after the hot melt resin impregnation. These hot melt unidirectional pre-pegs can be stored in rolls of e.g. 75m, 100m , 150m or 200m per roll. A significant difference between drum wound UD pre-peg and hot melt UD pre-peg is in the longitudinal length of these pre-pegs. The longitudinal length of drum wound UD pre-peg is determined by the circumference of the drum (eg. a drum with 1.90m circumference can only produce a UD pre-peg of 1.90m) whereas hot melt UD is continuous longitudinally and available in rolls of 75m, 100m, 150mm or 200mm per roll as referred to above. The intermediate sheet may be cut at a variety of different angles so as to provide the pre-pegs of intersecting fibres and such angles may be 15°, 221/2°, 30°, 45° or 60° or any other suitable angle so that the final sheet has sloping sides having the desired angle to vertical. Then the final sheet may be folded back upon itself so as to form a pre-peg or laminate sheet having intersecting fibres from which the pre-pegs may be cut out as hereinafter described. These pre-pegs may be alternated with pre-pegs that have each of the fibres arranged longitudinally or latitudinally to each other and which may be formed by the drum winding technique as discussed above so as to provide a final sheet which may be in the shape of a rectangle or square. Thus, pre-pegs having the longitudinally or latitudinally oriented fibres may then be cut out from the final sheet. The cutting of the intermediate sheet as described above may be carried out by cutting lines or grooves which are formed on an outer surface of the drum and arranged at the desired angle, e.g. 0° for forming pre-pegs of longitudinally or latitudinally arranged fibres and 60° or 45° for forming pre-pegs of intersecting fibres. Another significant difference between the solution drum winding as discussed above and the hot melt technique as discussed above is that instead of the cutting lines or grooves being formed on the drum in the solution drum winding technique in contrast in the hot melt technique the desired angles (say 15°, 221/2°, 30°, 45° or 60 degrees) will have to be cut physically on the pre-peg sheets, The method of construction of the invention allows the fabrication of a lightweight, inexpensive prosthesis made of composite material for amputees and, more particularly, to an improved lower limb prosthesis. Such a moulding method is effective for overcoming the limitations in the strength, dynamic endurance, weight problems of fibreglass and the stiffness/rigidity and fatigue limitations of prior art methods described above. The method of construction of the invention using non-metallic fibres in combination with an epoxy resin ensures that all individual fibres are impregnated to allow better dynamic endurance and a reduction in weight and thickness whilst retaining the natural flexibility and response of its fibres to allow the prosthesis to have a smoother transition from heel prosthesis to have a smoother transition from heel strike through to toe-off. Another advantage is that it allows better shock dispersion of the resilient constructed matrix that dissipates loads during heel strike. While the device of the present invention is preferably constructed of epoxy resin reinforced with laminates of carbon and/or glass fibres, it may be constructed of other non-metallic fibres such as aramid fibre, or recently developed synthetic fibres. Preferably the prosthesis is a pylon which suitably is J shaped. Preferably, said pylon, at least in outer extremities thereof having regard to a lateral dimension or thickness of the pylon, is formed from a laminate of alternating layer(s) of said intersecting fibres with some layer(s) of said fibres arranged in longitudinal and latitudinal orientation. The prosthesis may also comprise the J-shaped pylon in combination with a sole plate wherein the sole plate incorporates an anterior toe section and posterior heel section. The sole plate may also be formed from the same composite material as the J-shaped pylon. The * o prosthesis may also comprise the sole plate per se, The J-shaped pylon may have an upper shin mounting portion, a lower shin portion and an ankle zone. The ankle zone may taper in thickness from an upper part adjacent to the lower shin portion towards a lower end of the ankle zone. The upper shin mounting portion, preferably has a substantially constant thickness and width. The lower shin portion may have a width or lateral dimension that diverges outwardly as it approaches the ankle zone. The ankle zone, at or approaching a lower or free end thereof, may have a slight concave curvature. taper in thickness from an upper part adjacent to the lower shin portion towards a lower end of the ankle zone. The upper shin mounting portion, preferably has a substantially constant thickness and width. The lower shin portion may have a width or lateral dimension that diverges outwardly as it approaches the ankle zone. The ankle zone, at or approaching a lower or free end thereof, may have a slight concave curvature. Preferably, the sole plate is of substantial width compared to the ankle zone. It may comprise a heel portion and a toe portion. Preferably, the heel portion has a complementary or corresponding curvature to the ankle zone where they abut with each other. A resilient sole pad may be affixed to an underside of the sole plate in any suitable manner, eg by adhesive or the use of fasteners. Preferably, the sole plate is capable of being mounted to the underside of the ankle zone at a designated point of 90 to110mm from a toe end of the sole plate. Through the provision of two sole plates, it allows for the plurality of foot sizing ranging from 23cm-30cm. Suitably, for this purpose, the sole plate and ankle zone may be provided with holes which may be aligned to receive fasteners, such as bolts, there through to secure the sole plate to the ankle zone at selected positions. Suitably, two co-aligned holes are provided in the ankle zone and sole plate. Preferably, the sole plate is of substantially the same width as the ankle zone. Preferably, the heel portion is also substantially curved suitably on substantially the same radius as the leading end of the toe portion. The upper mounting shin portion of the J-shaped pylon may be secured to a mounting bracket, for example, by any suitable form of releasable attachment means, such as bolts or other suitable fasteners, to enable the upper mounting shin portion to be fixed to a distal end of a leg stump socket. The leg stump socket has a T-shaped bracket attachable thereto. Preferably, the bracket has a top flange, which is fixed to or fixable to the socket and a leg flange to which the mounting portion may be secured. Alternatively, the upper shin portion can be laminated directly to the distal end of the leg stump socket. The prosthetic device of the invention stores energy upon heel strike of the sole plate, with weight applied in the gait cycle, thereby transferring energy during heel strike-forward to mid foot (flat foot) and releases energy at toe-off point of sole plate to provide a stable and controlled propelling lift or thrust to the prosthetic device to aid in achieving a natural gait. The sole plate being fixed to the ankle zone, as described above, is capable of transferring smooth constant energy release from the heel strike through to toe-off of the sole plate during the gait cycle without lag, hesitation, jolting and/or braking, as a result of its one-piece design and fabrication. This is in contrast to prior art devices, such as US Patent No 4,822,363, that incorporate a releasable and attachable sole plate which has to transfer energy release through two separate members (ie. sole plate and pylon) to achieve energy release during the gait cycle. The prosthetic device of the present invention will accommodate angled or uneven terrain without the use of a separate ankle joint through the characteristics of the device that facilitate a continuous smoother transference of stored energy from heel strike through to toe-off. The device may include a plurality of toe and heel sections, wherein each of the toe and heel sections may be buffed to facilitate foot sizing. The prosthetic device of the invention is further capable of minimizing torsional movements and will accommodate stable and controlled lateral medial movements. Increased knee control allows increased ease of roll over of sole plate dissipating inertia and, thus, providing a smoother transition of movement regardless of the intensity of heel strike and mid-strike and toe-off. Preferably, the J-shaped pylon has a shank comprising both the upper shin mounting portion and the lower shin portion that has a uniform thickness and width for all weight categories. It can be cut off where required and adjusted to the wearer without affecting the above stated performance factors. BRIEF DESCRIPTION OF THE DRAWINGS In order that the invention may be more readily understood and put into practical effect, reference will now be made to the accompanying drawings that illustrate a moulded product of the invention in the form of a prosthetic device which is a preferred embodiment of the invention and wherein: FIG. 1 is a perspective view from the rear of the prosthetic device according to an embodiment of the invention; FIG. 2 is a side elevation of the prosthetic device according to an embodiment of the invention fitted to a stump socket; FIG. 3 is a front view of the prosthetic device detached from the stump socket and with mounting bracket removed; FIG. A is a plan view along line A-A of FIG. 2; FIG. 5 is a plan view of the sole plate; FIGS. 6 and 7 are perspective views illustrating steps (a) and (b) of the method of the invention; FIGS. 8 to 10 show drums that may be used in the method of the invention in FIGS. 6 and 7 having cutting lines or grooves arranged at varying orientations; FIGS. 11 to 13 show the formation of pre-pregs with fibres arranged in longitudinal orientation; FIGS. 14 to 18 show the formation of pre-pregs having fibres arranged in an intersecting orientation; and FIG. 19 is a general flow chart of a preferred embodiment of the method of the invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT Referring to the drawings and, firstly, to FIGS. 1 and 2, there is illustrated a prosthetic lower limb device 10 having a pylon 11 of generally J-shaped configuration in side elevation and which has an upper shin mounting portion 12, a lower shin portion 13, and a ankle zone 14. As illustrated and as more clearly shown in FIG. 2, the upper shin mounting portion 12, the lower shin portion 13 and the ankle zone 14 are of substantially uniform thickness. There is also provided a sole plate. As best shown in FIG. 3, the J-shaped pylon 11 has a constant width from the upper mounting portion 12 to a point 15. The lower shin portion 13 diverges symmetrically outwards the longitudinal axis of pylon 11 designated by Y-Y, thereby increasing in width to a second point 16, from which the J-shaped pylon 11 continues at a substantially constant width forming ankle zone 14. As shown in figs 1 to 2, the prosthetic lower limb device 10 also includes a T-shaped bracket 18 that has a leg 19 to which the upper mounting portion 12 of the J-shaped pylon 11 can be bolted via bolts 20. The T-shaped bracket 18 also includes a top flange 21 which can be laminated directly to a stump socket 22. Alternatively, the top flange 21 may have a variety of alignment connectors adjoined to it and then connected to the bottom of the stump socket 22 to provide adjustment and angle alignments to fine tune gait movements and complement socket fit. Fixed to the underside of the ankle zone 14 is an integrally formed sole plate 23, which is a one-piece component that incorporates in tandem both the heel portion 17A and toe portion 17. The toe portion 17 is slightly concave on its upper side and extends forward from bolts 26 which interconnect pylon 11 to sole plate 23 while the heel portion 17A is slightly convex on its upper side and extends rearward from bolts 26. The sole plate 23 is substantially the same width as ankle zone 14. There is also provided a sole pad 27. As shown also in FIGS. 4 and 5, there is provided in both sole plate 23 and pylon 11 a series of spaced pairs of co-aligned apertures 24 and 25 to permit the sole plate 23 to be secured to the ankle zone 14 by suitable bolts 26 through aligned apertures at a number of locations. As is apparent in FIG. 5, the leading end of the toe section 17 is of part circular form as is the heel end 17A of the sole plate 23. The above arrangements allow a variety of adjustments for the toe section 17 relative to the heel plate 23 of the prosthetic device 10, thus, permitting the toe section 17 and heel section 17A and sole plate 23 to accommodate subtle variations in the gait. A resilient sole material, such as a rubber or urethane pad 27, may be affixed to the underside of the sole plate 23 covering both the toe portion 17 and the heel portion 17A, and it extends continuously along the entire length of the sole plate 23. The rubber/urethane pad 27 imparts flexibility to the prosthetic lower limb device 10 and helps to absorb heel strike or torque loads that may be applied at the heel or axially along the lower shin portion 13. Further, the rubber or urethane pad 27 also provides energy dampening and increased comfort to the wearer. Typically, the rubber or urethane pad 27 is affixed in position by suitable adhesives. The rubber or urethane pad 27 can act as a non-slip surface to enable the prosthetic lower limb device 10 to be used without shoes. The configuration and design of the main support or J-shaped pylon 11, as described above, enable all stress concentrations to be dispersed more evenly from the shin-mounting portion 12, through the lower shin portion 13 and Into the ankle zone 14. The sole plate 23 is designed to provide greater stability and control of medial and lateral and for and aft movements. Furthermore, the prosthesis of the present invention and method of construction also increases the intrinsic strength and durability of the prosthetic tower limb or leg, which facilitates uniformity in a single dimensional design for all weight categories as well as novelty of resiliency rejoinder and return energy of the total prosthesis. It also facilitates distinctive variations of resiliency rates, smoother transition from heel impact to mid-strike to toe-off and allows better torsion movements, which can accommodate the many different exoskeleton and endoskeleton frames, body types and activity requirements of amputees, and a reduction in thigh and lower-back muscle fatigue and strain, compared to other prior art prostheses. The resulting J-shaped pylon 11 preferably has uniformity of thickness that extends from the upper mounting portion 12 and extends through the lower shin portion 13 through the ankle zone 14. The shape of sole plate 23 as shown facilitates smoother controlled toe-off. Furthermore, the configuration and construction of the J-shaped pylon 11 provides effective resilience and return energy of the total prosthesis 10 from upper shin mounting portion 12 through to the ankle zone 14 with the improved process of manufacture avoiding the necessity of prior art prosthesis require a variety of distinctive dimensional (width and/or thickness) pylons, heel plates/sole members to vary their rigidity. Typically, the length of the J-shaped pylon 11 to the lower surface of ankle zone 14 can vary from 255mm to 368mm. This, again, can be heightened through an increase of sole thickness (maximum 20mm), attachment of extension wedges to the top of T- shaped bracket 18 (3cm) and/or extension to the underside of the socket 22 (maximum 7.5cm). These methods of increasing prosthesis lower limb height will not influence performance of the prosthetic lower limb 10. The width of the J-shaped pylon 11 typically increases from 45mm at the mounting portion 12 and diverges outwardly at the point 15 to the position 16 (for a length of 80mm) to a width of 67mm, which then stays constant until ankle zone 14. Typically, the sole plate 23 also has a width of 67mm. The centres for holes 24 in FIG. 5 and holes 25 in FIG. 4 are typically positioned 15mm from the side edges of the sole plate 23 and ankle zone 14, respectively. The holes 24 in the sole plate 23 may be positioned between 90mm and 110mm from the front edge of the plate 23 while the holes 25 in the ankle zone 14 are suitably co-aligned with the holes 24 in the sole plate 23. This will allow for an increase or decrease in foot sizing. It should be highlighted that the above dimensions may be varied. The length of the upper shin-mounting portion 12 can be cut no less than 55mm to point 15 of the lower shin portion as shown in FIG 3 and adjusted to the wearer's requirement without affecting its performance. All of the J-shaped pylon 11 and sole plate 23 substantially have the same thickness, width and other dimensions throughout all weight classes from 30kg to 130kg at 10kg intervals. This is achieved through the novel method of the invention. In the present invention, single-dimensioned mould cavity moulds may be used for the moulding of J-shaped pylon 11 and sole plate 23. Thus, the J-shaped pylon will have uniform dimensions in thickness, in width, shape and sizes for all classes of weight categories. Similarly, the sole plate 23 will also have uniformity in dimensions for thickness, width, shape and sizes for all classes of weight categories. The toe section 17 and heel section 17A of the sole plate 23 can be buffed down to the appropriate size as required to provide for the increase in toe and/or heel rigidity to lessen the downward motion of heel strike length and/or toe-off. In relation to FIG. 6, it will be noted that carbon or glass filament 30 is unwound from a carbon bobbin 31 that is mounted and supported by axle 32. Axle 32 will rotate when the drum 36 pulls filament 30. Filament 30 is passed through a resin bath 34 containing the preferred epoxy resin solution 35. After passing through resin bath 34, the resin-impregnated filament 30A is then wound onto the drum 36 which has a sheet of release paper 37, preferably silicone coated release paper, attached thereto, wherein ends 38 and 39 may be overlapped and affixed together by double-sided tape at 40, so as to provide a continuous sheet of release paper 37 on drum 36. Resin-impregnated filament 30A may then be wound onto release paper 37 as drum 36 rotates. Drum 36 is being driven by suitable mechanical means (not shown) coupled to axle 41. Simultaneously as it rotates, the resin bath 34 together with axle 32 may travel in a linear direction indicated by arrows A or B causing the resin-impregnated filament 30A to be evenly spaced and laid (at a predetermined fibre area weight or fibre density) onto release paper 37, creating an intermediate pre-preg sheet 48A (in FIG. 12) from successive loops 42, as shown. Each of the successive loops 42 will overlap the preceding loop as they are wound onto the release paper 37 by the rotation of drum 36. The result is an intermediate pre-preg sheet 48A (in FIG. 12) that has binding integrity of its fibres from each resin-impregnated filament 30A and the intermediate pre-preg sheet 48A can be separated from release paper 37. Overlapping resin-impregnated filaments 30A are shown constituting the final appearance of sheet 48A at 42A. In an alternative arrangement, as shown in FIG. 7, the drum 36 may reciprocate in either direction A or B in relation to the stationary resin bath 34 and axle 32 so as to provide for the same result as described in FIG. 6. It will, however, be appreciated that the FIG. 6 arrangement is preferred. It will be noted from FIGS. 8, 9 and 10 that drum 36 may be provided with elongate grooves or cutting lines 43, 44 and 45 so as to facilitate cutting and removal of the composite sheet 46 from drum 36 at three cutting angles, typically but not exclusively at 0° or parallel to axle 41 for cutting line 43 as shown in FIG. 8, at 60° to axle 41 for cutting line 44 as shown in FIG. 9, or at 45° to axle 41 for cutting line 45 as shown in FIG.10. Cutting lines of other angles (although not shown in FIGS 8, 9 and 10) may be used to provide other intersecting angles for the unidirectional pre-pregs. It will also be appreciated that cutting lines 43, 44,45 or lines of other angles, may be provided on the same drum 36 or such cutting lines may be provided on different drums 36. However, having a plurality of cutting lines on the same drum is preferred for versatility and cost reasons. FIGS. 11 to 13 show the cutting of composite sheet 46 by cutting knife 47 along cutting line 43 so as to provide for an intermediate pre-preg sheet 48A. The intermediate pre-preg sheet 48A is then cut to the preferred shape and sizes as shown in pre-preg 49. Each intermediate pre-preg sheet 48A can provide for multiple cuttings of pre-pregs 49 having longitudinal or 0° carbon or glass fibres as shown. The example shown in FIG. 13 illustrates pre-preg 49 having a narrow part 50 and a broader part 51 as required by the preferred design. The cutting and removal of pre-pregs 49 leaves gaps 52 in sheet 48A. Resin-impregnated filament 30A are shown in longitudinal orientation or 0°. In a variation of the procedure described above, pre-pregs 49 may be formed not only by longitudinal orientation of the fibres (i.e.O0) but also by transverse or latitudinal orientation (i.e.90°) using intermediate pre-preg sheet 48A. FIG. 14 shows the cutting of composite sheet 46 along cutting line 44 so as to provide for intermediate sheet 48B shown in FIG. 15, which is then provided with crease or fold lines 52, 53, 54 and 55. The folding begins with part 58 being folded along fold line 55 as shown by arrow E, followed by part 59 being folded along fold line 54, as shown by arrow F. Subsequently, part 57 is folded along fold line 53, as shown by arrow D, and lastly, part 56 is folded along fold line 52, as shown by arrow C. Alternatively, part 60 may be folded along fold line 54, as indicated by arrow G, instead of part 59 along fold line 54 as indicated by arrow F. This procedure is further illustrated in FIGS. 16 and 17 to provide a final folded sheet 61 (shown in FIG. 17), from which multiple pre-pregs 62 (shown in FIG. 18) may be cut as shown in phantom in FIG. 17, leaving gaps 65. FIG. 18 also shows a pre-preg 62 having intersecting fibres from the resin-impregnated filaments 30A. The intersecting fibres are from the parts 56, 57, 60, 59 and 58 being folded along fold lines 52, 53, 54 and 55 back upon themselves. Optimum pliability rates, compressive strength, dynamic endurance, fore-and-aft and torsional rigidity in the various weight categories (30-130kg), may be achieved in the J-shaped pylon 11 and sole plate 23 (in FIG.1) by various carbon/carbon or carbon/glass fibre combinations with variations in fibre area weight and fibre orientation. All weight categories (30-130kg) in a preferred embodiment of the invention have the same number of layers of laminates in the construction. The intrinsic characteristics and mechanical strength of the preferred carbon and glass fibres has created a variety of possible configurations in material compositions, fibre area weight and fibre orientations and sequencing to optimise the compressive strength, flexibility, durability, dynamic endurance, fore-and-aft and torsional rigidity in a preferred embodiment. Carbon fibre possesses much higher tensile strength and tensile modulus as compared to glass fibres. However, glass fibres, though less strong, have higher flexibility and fatigue endurance. Higher percentage of carbon fibres and lower percentage of glass fibres in the construction will result in higher stiffness and strength in a preferred embodiment and flexibility will increase with a reduction in tensile strength if we use a higher percentage of glass fibres. Configurations of fibre orientation is another element in the present invention. Typically, placing longitudinal or 0° fibres along and parallel to the principle axis of J-shaped pylon 11 and sole plate 23 will result in very low torsional strength but very high stiffness, very high tensile and high compressive strength. Other fibre angles such, as 30°, 45° or 60° possess much higher torsional strength but lower tensile or compressive strength. It must be highlighted that the intrinsic mechanical properties of carbon and glass fibres are very different from each other and therefore it is natural to expect that their 0°, 30° and 45° angles produce very different results in torsion, tensile strength and compressive strength and this provides more options to configure and to optimise the compressive strength, flexibility, durability, dynamic endurance, fore-and-aft and torsion rigidity of each weight category in a preferred embodiment. Typical carbon/carbon and carbon/glass compositions for the J-shaped pylon 11 and sole plate 23 are set out in the Table attached hereto. The process of the invention ensures that all the fibres during resin impregnation are thoroughly "wetted" and properly impregnated with the epoxy resin. Typically, this method will produce carbon and glass pre-preg having a resin content range from 35% to 50%. The resin content is higher than most of the commercially available UD pre-preg. The epoxy resin functions as a glue to bind and encapsulate all fibres together. Higher resin content will ensure sufficient resin flow during moulding and will also provide a greater degree of control in the cross linking process, giving a much improved resin/fibre matrix. The result is an increase in strength and durability in a preferred embodiment. All conventional lower limb prosthetic devices are constructed from UD longitudinal fibres in their main core with continuous and uninterrupted woven latitudinal or woven angular fibres on the outer layers to improve their torsion strength. The use of pre-preg 49 (having either 0° or 90° degree fiber orientation) and pre-preg 62 (having other intersecting fiber orientation) in the present preferred embodiment creates a totally new concept and method of construction for moulded products generally inclusive of the lower limb prosthetic device of the invention and is uniquely different from prior art methods. In this present invention, fibre filaments do not have to be continuous and uninterrupted as shown by the method of producing pre- preg 49 and 62. It must be noted that the use of non-continuous fibre filaments constitutes a significant feature of the prosthetic device of the present invention. FIG. 19 refers to the preferred flow chart for the processes of the present invention in relation to manufacture of moulded products inclusive of lower limb prosthetic device. Epoxy resin solution may be formed by mixing the resin, catalyst, additives and solvent in stipulated proportions. The epoxy resin solution may have a 60% to 70% solid content with a cure time of 30 min at 130° degree Celsius and may possess toughness, flexibility, good thermal stability and chemical resistance, and having good bonding strength with the carbon and glass fibres which are the preferred fibres for use in the present invention. This method of the invention allows carbon and/or glass unidirectional pre-pregs to be produced with a wide selection of fibre area weights (ranging from 60grams to SOOgrams per square meter), resin content (ranging from 35% to 50% by weight) and fibre orientations and sequencing to be employ and it also provides the flexibility to "choose and optimize" pre-pregs from the various combinations of material compositions, fibre area weight, fibre orientation and resin content that are available. Typically, the carbon and glass fibres used in the preferred method of the present invention, are high strength filaments. The preferred drum wound technique ensures that all the fibres during resin impregnation are thoroughly "wetted" and properly impregnated with the epoxy resin. With adroit control in resin viscosity during the resin impregnation process, it is possible to control resin content within +2%. Controlled and consistent resin content are preferable in the maintenance of compressive strength, durability, dynamic endurance, pliability rates, fore-and-aft and torsional rigidity. The intermediate pre-preg sheets 48A and final folded pre-preg sheet 61 may be subjected to force drying in an oven to remove solvents and any other unwanted volatile components in the epoxy resin. Forced drying also makes the pre-preg sheets less tacky and more suitable for handling in the lay-up process. Suitable oven specifications are temperature of 50-65°C and drying time of 3 to 4 hours. Subsequently after the forced drying process, each intermediate pre-preg sheet 48A and final folded pre-preg sheet 61 may be weighed and cut into pre-preg 49 or pre-preg 62 as appropriate. It must be highlighted that weighing of the intermediate pre-preg sheets 48A and final folded pre-preg sheet 61 after forced drying is a desirable aspect of the process of the invention. This is to segregate pre-pregs that falls in the high or low end of the resin content range, and to combine these pre-pregs appropriately so that the weight of the moulded J-shaped pylon 11 or sole plate 23 remains relatively constant. As an example, a pre-preg having high resin content may be used in conjunction with another that has low resin content during lay-up process. After the lay-up of successive layers of pre-preg 49 and pre-preg 62 in the respective compression mould cavity, the compression mould may be heated to 135°C-150°C (and more preferably 140°C) suitably in combination with a hydraulic pressure of 200 kg/cm2 using a 200mm diameter hydraulic piston. After curing, de-moulding is undertaken to remove the moulded members, which are then prepared for assembly and final cosmetic treatment. It will be appreciated from the foregoing that in view of the fact that the moulded product of the invention can be made from a mould cavity of similar dimensions regardless of weight that this feature will also apply in a preferred embodiment to the moulded product of the invention such as the J shaped pylon or the sole plate. It therefore will be appreciated from the foregoing that the process of the invention provides a lower leg prosthesis which has considerable advantages over the prior art as will be apparent from the foregoing description. EXAMPLES EXAMPLE I A preferred method of lay up or sequencing of both pre-pregs 49 and 62 is described below in relation to manufacture of a J shaped pylon. All weight categories (30kg-130kg), in this preferred method, have the same number (58) of layers with variations to the fibre sequencing and fiber orientation to achieve the varied pliability rates for each weight category, viz: 30kg to 40kg - pylon 345g ±5g, 38 layers of 60° fiber and 20 layers of 0° and 90° fiber combination. 40kg to 50kg - pylon 345g ±5g, 38 layers of 60° fiber and 20 layers of 0° fiber combination. 50kg to 60kg - pylon 345g ±5g, 38 layers of 45° and 60° fiber combination with 20 layers of 0° and 90° fiber combination. 60kg to 70kg - pylon 345g ±5g, 38 layers of 45° and 60° fiber combination and 20 layers of 0° fiber. 70kg to 80kg - pylon 345g ±5g, 38 layers of 45° and 20 layers of 0° and 90° fiber combination. 80kg to 90kg - pylon 345g ±5g, 38 layers of 45° and 20 layers of 0° fiber. 90kg to 100kg - pylon 345g ±5g, 38 layers of 30° and 45° fiber combination and 20 layers of 0° and 90° fiber combination. 100kg to 110kg - pylon 345g ±5g, 38 layers of 30° and 45° fiber combination and 20 layers of 0° fiber. 110kg to 120kg - pylon 345g ±5g, 38 layers of 30° fiber and 20 layers of 0° and 90° fiber combination 120kg to 130kg - pylon 345g ±5g, 38 layers of 30° fiber and 20 layers of 0° fiber. For all pylon categories (30-130kg), the carbon/carbon pre-preg lay-up sequences are preferably the same. Thus, for the pylon having 58 layers which comprise 38 layers of angled fiber and 20 layers of 0° and 90° fiber combination, the lay-up sequence is 8 layers of angled carbon fiber with FAW 100 at 0,12mm, 6 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm, 10 layers of angled carbon fiber with FAW (Fibre Area Weight) 100 at 0.12mm, 6 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm, 10 layers of angled carbon fiber with FAW 100 at 0.12mm, 8 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm and 10 layers of angled carbon fiber with FAW 100 at 0.12mm. EXAMPLE H Maximisation of pliability rates, dynamic endurance, compressive strength, fore-and-aft and torsional rigidity of the different weight categories (30-130kg) may be achieved in the sole plate by a combination of carbon fibre angles (0°, 30°, 45°, 60° and 90°) and glass fibre angles (30°, 45° and 60°), varied fibre lengths, fibre alignment (using lateral, transverse and diagonal directions), combined carbon layer thicknesses (0.12mm FAW 100/sq.m and 0.15mm FAW 150g/sq.m) and/or glass fibre layer thickness (0.16mm FAW 126g/sq.m). All weight categories discussed above (30kg to 130kg) preferably have the same total number (52) of layers for either the entire carbon or combined carbon/glass fibre sole plate. Through the variations in the lay-up sequencing and fibre alignment for both carbon/carbon and carbon/glass fibre, the varied pliability rates for each weight category have been achieved, viz: 30kg to 40kg - Sole Plate 190g ±5g, Carbon/Glass 50%/50% 40kg to 50kg - Sole Plate 190g ±5g, Carbon/Glass 50%/50% 50kg to 60kg - Sole Plate 190g ±5g, Carbon/Glass 70%/30% 60kg to 70kg - Sole Plate 190g ±5g, Carbon/Glass 70%/30% 70kg to 80kg - Sole Plate 190g ±5g, Carbon 100% 80kg to 90kg - Sole Plate 190g ±5g, Carbon 100% 90kg to 100kg - Sole Plate 190g ±5g, Carbon 100% 100kg to 110kg - Sole Plate 190g ±5g, Carbon 100% 110kg to 120kg - Sole Plate 190g ±5g, Carbon 100% 120kg to 130kg - Sole Plate 190g ±5g, Carbon 100% For the following sole plate weight categories (30-130kg), the carbon/carbon and carbon/glass pre-preg lay-up sequence having regard to pre pegs 49 and 62 are: 30 to 40kg - 16 layers of 60° carbon fiber with FAW 100 at 0.12mm, 10 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm and 26 layers of 60° glass fiber with FAW 126 at 0.16mm 40 to 50kg - 16 layers of 60° carbon fiber with FAW 100 at 0.12mm, 10 layers of carbon 0° with FAW 150 at 0.15mm and 26 layers of 60° glass fiber with FAW 126 at 0.16mm 50 to 60kg -26 layers of 60° carbon fiber with FAW 100 at 0.12mm, 10 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm and 16 layers of 60° glass fiber with FAW 126 at 0.16mm 60 to 70kg - 26 layers of 60° carbon fiber with FAW 100 at 0.12mm, 10 layers of carbon 0° with FAW 150 at 0.15mm and 16 layers of 60° glass fiber with FAW 126 at 0.16mm 70 to 80kg - 36 layers of 45° and 60° carbon fiber combination with FAW 100 at 0,12mm, 16 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm 80 to 90kg - 36 layers of 45° and 60° carbon fiber combination with FAW 100 at 0.12mm, 16 layers of carbon 0° with FAW 150 at 0.15mm 90 to 100kg - 36 layers of 45° carbon fiber with FAW100 at 0.12mm, 16 layers of carbon fiber 0° and 90° carbon fiber combination with FAW 150 at 0.15mm 100 to 110kg - 36 layers of 45° carbon fiber with FAW 100 at 0.12mm, 16 layers of carbon fiber 0° with FAW 150 at 0.15mm 110 to 120 kg - 36 layers of 30° and 45° carbon fiber combination with FAW 100 at 0.12mm, 16 layers of carbon fiber 0° with FAW 150 at 0.15mm 120 to 130 kg - 36 layers of 30° carbon fiber with FAW 100 at 0.12mm, 16 layers of carbon fiber 0° with FAW 150 at 0.15mm. (Table Removed) We Claim: 1. A method of construction of a prosthesis device for patients of various weight categories, said method including the steps of: (a) impregnating non-metallic fibers in a thermosetting resin whereby said impregnated fibers are placed to form a sheet of said fibers; (b) folding the sheet by bending adjoining parts of the sheet along adjacent fold lines therebetween so that said fibres are placed in an intersecting orientation to form a prepeg (49) having a double layer of fibres in different planes with the fibres in each layer having a different angle of orientation to a longitudinal axis of the prepeg (49); (c) cutting a plurality of pre-pregs from said sheet formed in step (b); (d) forming layers of said pre-pregs (49) obtained from step (c) so that said layers are placed in stacked relationship in a mould cavity of a compression mould whereby the mould cavity has a constant volume for each of the various weight categories; (e) compression moulding at elevated temperature: and (f) removing the prosthesis from the compression mould. 2. A method as claimed in claim 1 comprising a sheet as obtain from step (a) said sheet is made of drum (36) winding technique whereby said impregnated fibres are would onto a drum (36) so as to provide an intermediate composite sheet (46) formed of the fibres supported on a sheet of release paper (37) on the drum (36), whereby upon removal of the release paper (37), the sheet formed by step (a) is obtained by cutting the intermediate sheet as it is supported on the drum (36). 3. A method as claimed in claim 1 wherein the said sheet is made up of hot melt technique the same is being made after hot melt resin impregnation of the fibres being laid onto a continuous sheet of release paper(37) and subsequently stored as rolls. 4. A method as claimed in claim 1 wherein in step (d) layers of said pre-pegs having fibres placed in an intersecting orientation are mixed with layers of pre-pegs which have all of their fibres placed in a latitudinal and/or longitudinal orientation. 5. A method as claimed in claim 1 wherein in step (d) layers of said pre-pegs having fibres placed in an intersecting orientation are alternated with layers of pre-pegs having all of their fibres placed in a latitudinal and/or longitudinal direction. 6. A method as claimed in claim 1 wherein in step (d) there is a lay up sequence in the mould cavity the said layers of pre-pegs having fibres are being placed in an intersecting orientation being followed by layers of pre-pegs having their fibres placed in a longitudinal and/or latitudinal orientation followed by layers of pre-pegs having their fibres placed in an intersecting orientation. 7. A method as claimed in claim 1 wherein in step (d) successive layers are formed of pre-pegs having fibres placed in an intersection orientation which alternate with pre-pegs having fibres placed in a longitudinal and/or latitudinal orientation. 8. A method as claimed in claim 1 wherein in step (c) the intermediate sheet is cut at a variety of different angles selected from the group consisting of 15°, 221/2°, 30°, 45° and 60° so that the final sheet has sloping sides having an acute angle to vertical before folding of the final sheet upon itself to form said pre-peg. 9. A method as claimed in claim 8 wherein the cut angle is selected from 30° and 45°. 10. A method as claimed in claim 2 wherein the cutting of the intermediate sheet is carried out by provision of cutting lines(43, 44, 45) or grooves which are formed in an outer surface of the drum (36) at an angle selected from the group consisting of 15°, 221/2°, 30°, 45° and 60° for pre-pegs of intersecting fibres. 11. A method as claimed in claim 4 wherein said pre-pegs having fibres placed in a latitudinal and/or longitudinal orientation are formed from an intermediate sheet which intermediate sheet is cut at an angle of 0° for longitudinal fibres and 90° for latitudinal fibres having regard to a longitudinal axis of a drum (36) supporting the intermediate sheet. 12. A method as claimed in claim 1 wherein step (d) is carried out in a mould cavity having the same dimensions for different weights or different weight categories of moulded product. 13. A prosthesis device constructed by a method as claimed in claim 1 for patients of various weight categories formed from composite materials having layers of non-metallic fibres impregnated with a thermosetting resin, characterized in that said prosthesis device is formed at least partly from double layers of non continuous or cut fibres in different planes wherein the fibres are placed in an intersecting orientation wherein the fibres in each layer have an accurately predetermined different angle of orientation to a longitudinal axis of the prosthesis whereby said prosthesis has varying areas of fibre area weight along its length to provide said prosthesis with differential locations of stiffness and flexibility to enhance whereby thereof and said prosthesis has the same dimensions or number of layers of fibres regardless of the weight category of the patient. 14. A prosthesis device as claimed in claim 13 wherein the said device is in the form of a pylon. 15. A prosthesis device as claimed in claim 13 wherein the said device is in the form of a J shaped pylon (11). 16. A prosthesis device as claimed in claim 13 wherein the said device in the form of a sole plate (23). 17. A prosthesis device as claimed in claim 13 wherein the said device in the form of a combination of a J shaped pylon (11) attached to a sole plate (23) so as to define a lower limb prosthetic device. 18. A prosthesis device as claimed in claim 13 wherein the pylon at least in outer extremities thereof is formed from a laminate of alternating layers of said intersecting fibres with layer(s) of said fibres placed in longitudinal and/or latitudinal orientation. 19. A prosthesis device as claimed in claim 15 wherein the J shaped pylon (11) has an upper shin mounting portion, a lower shin portion and an ankle zone (14). 20. A prosthesis device as claimed in claim 19 wherein the upper shin mounting portion has a constant thickness and width. 21. A prosthesis device as claimed in claim 19 wherein the lower shin portion has a width that diverges outwardly as it approaches the ankle zone (14). 22. A prosthesis as claimed in claim 19 wherein the ankle zone (14) at or approaching a lower or free end thereof has a slight concave curvature. 23. A prosthesis device as claimed in claim 17 wherein the sole plate (23) is of width compared to an ankle zone (14) of the J shaped pylon (11). 24. A prosthesis device as claimed in claim 16 wherein the sole plate (23) has a heel portion and a toe portion. 25. A prosthesis device as claimed in claim 23 wherein the heel portion has a complementary or corresponding curvature to the ankle zone (14) where they abut each other. 26. A prosthesis device as claimed in claim 13 which has the same dimensions and shape regardless of weight. 27. A method of construction of a prosthesis device for patients of various weight categories substantially as herein described with reference to the foregoing description, examples, tables and the accompanying drawings.

Full Text

TITLE
"METHOD OF CONSTRUCTION OF MOULDED PRODUCTS"
FIELD OF THE INVENTION
THIS INVENTION relates to a method of construction of moulded products and moulded products constructed by the method. In particular, the invention relates to a method of construction of prosthetic devices and the specification will now describe in detail by way of example a method of construction of prosthetic devices although it should not be limited to this particular example.
BACKGROUND ART
In the past 15 years, there have been an increasing number of lower-limb amputees who have desired to enhance their quality of life by being able to have access to an affordable prosthesis that will provide not only basic mobility but which will also encourage and permit participation in low- to high-impact activities in the same manner as enjoyed by non-amputees.
Numerous technological advances in the field of prosthetics have allowed this to happen and have provided a wide range of prosthetic legs to choose from. In coalition with the general type of prosthesis for normal gait activities, such as basic ambulant walking and work type activities, there has been a demand by amputees for prostheses that can enable them to lead a more active lifestyle and, thus, improve their quality of life. There has been much effort within the prosthetic industry to develop a lightweight and durable prosthesis that will allow amputees to participate in strenuous career options, such as laboring, farm work, etc,
and various medium- to high-level activities, such as jogging, squash, climbing, tennis, etc, and very high-impact sports, such as running, sprinting, jumping, basketball and volleyball.
Numerous different prostheses have been developed, each trying to replicate the function and appearance of the replaced body part. Lower leg prostheses present unique problems. They must be strong enough to support a person's weight and activity level and to withstand the forces encountered through gait movement. As a result, some prostheses developed in the past were very heavy and rigid and restricted the wearer's activity level, career, recreational and sport options.
There are a number of different composite foot and leg prosthetic devices that have now been proposed, most of which utilize modern composite material technology to impart energy storage and release during use. Examples of prosthetic foot devices that have been fabricated with composite materials, with the intention of storing energy when the foot is placed on the ground and to release it and provide a lift or thrust as the foot is removed from the ground to aid in the patient's gait are disclosed in Abrogast et al. US Patent No 4,865,612, concerning an artificial foot having a pair of thin forwardly extending spring members connected to a keel and Shorter et al. US Patent No 5,116,383. US Patent No 5,116,383 describes an energy storing foot having a single piece carbon fibre reinforced keel having a lower spring portion connected at its posterior end as a cantilever to an upper ankle mounting portion. The energy storing foot is combined with a resilient ankle joint of the ball
and socket type.
Other lower leg prosthetic devices in the prior art have employed springs, including multiple leaf springs or flat spring-like members, in an attempt to approximate the response and performance of a natural foot. Examples include Merlette US Patent No 4,959,073 and Phillips US Patent No 4,547,913,4,822,363 and 5,776,205.
An example of the abovementioned lower leg prosthetic device is a prosthesis known as the Flex-Foot, which provides a composite strut and foot configuration, which is specifically described in US Patent No 4,547,913. The spring-like action imparted by the materials used in such devices results in additional mobility and comfort to the wearer. Prior art prosthetic feet that utilize a plurality of springs, such as in Phillips US Patent No 5,776,205, tend to rock under vertical load as the load is distributed separately to the springs.
Furthermore, the dynamic feet of the Flex-Foot system that are commercially available, do not have rigid ankle joints. However, this system embodied a rearward separate heel segment or heel portion secured to the main body of the foot, at the mid foot. While this system provides better performance than the former prostheses, this system embraces a plurality of components and joints which are less than optimum for transference of energy from heel strike through to toe-off because of the rearward heel segment deficiency of transmission of continual energy from a separate heel plate through to a separate toe portion on the J-pylon as described in US Patent No 4,822,363 and/or a
full sole member described in US Patent No 5,976,191, This is because of the necessity to incorporate additional support members or increase in pylon thickness, which is necessary to provide suitable wearer support and prosthesis performance.
Prior art prosthetic feet with a separate heel spring member and/or foam/rubber resilient material placed between foot and sole member tend to absorb vertical load either in the spring member or in the foam/rubber resilient material and, thus, dissipates the transfer of constant energy from heel strike to toe-off.
US Patent Nos 4,822,363 and 4,547,913 refer specifically to a J-shaped pylon made from the composite material connected to a flat spring-like rearward heel plate. US Patent No 4,959,073 refers to a J-shaped pylon made from the composite material that is integrally formed with a heel member. Reference also may be made to US Patent No 5,037,444, which refers to a prosthetic foot made from the composite material alternatively known as the so-called "Seattle Foot". These devices make great advances in gait movement and activity levels and have a higher strength and stiffness to weight ratio of graphite to other materials, which results in almost complete return of input or stored energy, lighter weight, higher fatigue strength, and minimal creep. However, these devices also possess some disadvantages. For example, because of the higher strength and stiffness to weight ratio of graphite as compared to other materials, local stiffness, jolting and braking occurs because of material lay-up fabrication methods, which interferes with
smooth and even flexing of the components during the wearer's stride. Furthermore, while substantially lighter in weight, they have an inherent rigidity because of the higher tensile strength resulting in greater stiffness to weight ratio of graphite to other material and also have areas more prone to fatigue stress failure.
Prior art prosthetic feet that utilize a spring-loaded heel which operates on a spring separate from a spring in the toe section, such as in the Phillips and Merlette patents discussed above, effectively store energy in the heel, but are ineffective in transferring the energy from the heel to the toe portion of the prosthetic foot as the foot rolls forward during the gait cycle. These devices still require separate loading of a spring in the toe section. As a result, wearers notice a distinct and unnatural lag or hesitation in rolling the foot forward during the gait cycle, giving the foot an unnatural feel and causing an uneven stride.
Some prior art prosthetic feet, such as the devices of Phillips US Patent Nos 4,547,913 and 4,822,363, can accommodate torsion movement about the longitudinal axis of the shin portion, but the shape of the shin portion is designed for spring strength and breaking strength, not torsion movement.
The prior art devices of US Patent Nos 4,547,913,4,822,363 and 4,959,073 and others are made up exclusively from a composite material comprising high strength graphite filaments in a high-toughness epoxy thermosetting resin, constructed from uni-directional (UD) longitudinal fibres in their main core with woven latitudinal or woven
angular fibres on their outer layers to improve their torsion strength. The latitudinal or angular woven materials come in the form of woven sleeves. These woven sleeves can easily slide over and cover the UD longitudinal fibres that are in the main core. These outer layers are woven sleeves and all their fibre filaments are continuous from start to finish. If this was not the case, it would not be possible to weave these filaments into a woven sleeve. Usually, the main core and the woven sleeves were formed by a number of plies or laminae that were placed in a rigid mould shaped to the final configuration and, subsequently, cured.
This provides a result wherein each of the continuous filaments extend uninterrupted through an upper extremity, shin portion and foot portion of the prosthesis or from the top of leg portion downwardly through the ankle section, across the top of the foot or toe portion. Also, the heel plate and/or sole member have continuous filaments that extend uninterrupted from front extremity to heel extremity ie. all fibre filaments are continuous and uninterrupted longitudinally, latitudinal or angularly in their constructions. Similar construction methods are described in US Patent Nos 5,037,44, 5,156,631, 5,181,933, 5,493,456, 5,514,185 and 6,071,313.
Such construction methods have the following disadvantages, ie:
(a) It was necessary to thicken the upper extremity of the pylon to provide a rigid upper extremity. This may also be accomplished by expanding the width of said upper extremity;
(b) It was important to increase the number of plies or
laminae and, thus, the thickness of the pylon to accommodate users as
their weight or activity level increases;
(c) Additional laminates were added to maintain strength
as the width of the pylon is reduced;
(d) It was considered important to achieve a gradual
reduction in the thickness of the pylon in the various dynamic areas
thereof such that the foot portion is reduced in thickness compared to the
ankle portion, and the ankle portion is reduced in thickness compared to
the shin portion.
The number of plies or laminations or layers varies in the different sections. As a consequence of (a), (b), (c) and (d) above, it was a general expectation from conventional methods of construction of prostheses as described above that, depending on the foot size and strength needed in a particular prosthesis, the number of plies employed can be increased or decreased as required. For example, fewer laminations may be required for a smaller prosthesis, or a prosthesis for a lightweight individual. A larger prosthesis, or a prosthesis for a heavier individual, may require more laminations. It was considered generally desirable to employ as few laminations as are needed for strength and stiffness to keep the prosthesis as light weight as practicable.
From the discussion of prior art methods of construction above, it was necessary in the conventional manufacturing process to provide a plurality of different moulds or provide changes in mould cavity
dimensions when additional plies or laminae were used to increase thicknesses or widths of prostheses. In other words it was necessary to use different mould cavity dimensions to correspond to different weights or different weight categories of prosthesis. The necessity of different thicknesses or widths was necessary to provide a variety of prostheses with different dimensions, thereby providing a disparity of thicknesses or widths to accommodate variations of pliability rates to support different exoskeleton and endoskeleton frames, body types and activity requirements of amputees.
OBJECT OF THE INVENTION
It has now been found that the above deficiencies of conventional manufacturing processes of conventional prostheses may now be reduced or overcome by the advent of the present invention where variations in requirements of individual users inclusive of amputees can be obtained by a process, as described hereinafter, which has the capability to make prosthesis inclusive of prostheses having a range of different weights or different weight categories in a single dimensional cavity mould, thus, making the process not only more efficient, but also less expensive. SUMMARY OF THE INVENTION
In one aspect of the invention, there is provided a method of construction of a prosthesis for patients of various weight categories, , said method including the steps of:
(a) impregnating non-metallic fibres in a thermosetting resin whereby said impregnated fibres are arranged to form a sheet of said
fibres;
(b) folding the sheet by bending adjoining parts of the sheet
along adjacent fold lines therebetween so that said fibres are arranged in
an intersecting orientation to form a prepeg having a double layer of fibres
in different planes with the fibres in each layer having a different angle of
orientation to a longitudinal axis of the prepeg;
(c) cutting a plurality of pre-pegs from said sheet formed in step
(b);
(d) forming layers of said pre-pegs obtained from step (c) so
that said layers are arranged in stacked relationship in a mould cavity of a
compression mould whereby the mould cavity has a constant volume for
each of the various weight categories;
(e) compression moulding at elevated temperature; and
(f) removing the prosthesis from the compression mould.
In step (a) although the sheet can be produced by either solution drum winding or a hot melt technique as hereinafter described, it is preferable to use the drum winding technique so as to provide an intermediate composite sheet formed of the fibres supported on a sheet of release paper, whereby upon removal of the release paper, the final sheet formed by step (a) is obtained after cutting the intermediate sheet as it is supported on the drum. Preferably all of the fibres in the sheet are oriented in the same or similar direction and thus may be described as unidirectional (UD),
In an alternative hot melt technique which may be used instead of
the solution drum winding as described above in step (a) the pre-peg formed using said technique has fibers that are continuous and that are laid onto a continuous sheet of release paper after the hot melt resin impregnation. These hot melt unidirectional pre-pegs can be stored in rolls of e.g. 75m, 100m , 150m or 200m per roll.
A significant difference between drum wound UD pre-peg and hot melt UD pre-peg is in the longitudinal length of these pre-pegs. The longitudinal length of drum wound UD pre-peg is determined by the circumference of the drum (eg. a drum with 1.90m circumference can only produce a UD pre-peg of 1.90m) whereas hot melt UD is continuous longitudinally and available in rolls of 75m, 100m, 150mm or 200mm per roll as referred to above.
The intermediate sheet may be cut at a variety of different angles so as to provide the pre-pegs of intersecting fibres and such angles may be 15°, 221/2°, 30°, 45° or 60° or any other suitable angle so that the final sheet has sloping sides having the desired angle to vertical. Then the final sheet may be folded back upon itself so as to form a pre-peg or laminate sheet having intersecting fibres from which the pre-pegs may be cut out as hereinafter described.
These pre-pegs may be alternated with pre-pegs that have each of the fibres arranged longitudinally or latitudinally to each other and which may be formed by the drum winding technique as discussed above so as to provide a final sheet which may be in the shape of a rectangle or square. Thus, pre-pegs having the longitudinally or latitudinally oriented
fibres may then be cut out from the final sheet.
The cutting of the intermediate sheet as described above may be carried out by cutting lines or grooves which are formed on an outer surface of the drum and arranged at the desired angle, e.g. 0° for forming pre-pegs of longitudinally or latitudinally arranged fibres and 60° or 45° for forming pre-pegs of intersecting fibres.
Another significant difference between the solution drum winding as discussed above and the hot melt technique as discussed above is that instead of the cutting lines or grooves being formed on the drum in the solution drum winding technique in contrast in the hot melt technique the desired angles (say 15°, 221/2°, 30°, 45° or 60 degrees) will have to be cut physically on the pre-peg sheets,
The method of construction of the invention allows the fabrication of a lightweight, inexpensive prosthesis made of composite material for amputees and, more particularly, to an improved lower limb prosthesis. Such a moulding method is effective for overcoming the limitations in the strength, dynamic endurance, weight problems of fibreglass and the stiffness/rigidity and fatigue limitations of prior art methods described above.
The method of construction of the invention using non-metallic fibres in combination with an epoxy resin ensures that all individual fibres are impregnated to allow better dynamic endurance and a reduction in weight and thickness whilst retaining the natural flexibility and response of its fibres to allow the prosthesis to have a smoother transition from heel
prosthesis to have a smoother transition from heel strike through to toe-off. Another advantage is that it allows better shock dispersion of the resilient constructed matrix that dissipates loads during heel strike.
While the device of the present invention is preferably constructed of epoxy resin reinforced with laminates of carbon and/or glass fibres, it may be constructed of other non-metallic fibres such as aramid fibre, or recently developed synthetic fibres.
Preferably the prosthesis is a pylon which suitably is J shaped.
Preferably, said pylon, at least in outer extremities thereof having regard to a lateral dimension or thickness of the pylon, is formed from a laminate of alternating layer(s) of said intersecting fibres with some layer(s) of said fibres arranged in longitudinal and latitudinal orientation.
The prosthesis may also comprise the J-shaped pylon in
combination with a sole plate wherein the sole plate incorporates an anterior toe section and posterior heel section. The sole plate may also be formed from the same composite material as the J-shaped pylon. The
* o
prosthesis may also comprise the sole plate per se,
The J-shaped pylon may have an upper shin mounting portion, a lower shin portion and an ankle zone. The ankle zone may taper in thickness from an upper part adjacent to the lower shin portion towards a lower end of the ankle zone.
The upper shin mounting portion, preferably has a
substantially constant thickness and width. The lower shin portion may have a width or lateral dimension that diverges outwardly as it approaches the ankle zone. The ankle zone, at or approaching a lower or free end thereof, may have a slight concave curvature.
taper in thickness from an upper part adjacent to the lower shin portion towards a lower end of the ankle zone.
The upper shin mounting portion, preferably has a substantially constant thickness and width. The lower shin portion may have a width or lateral dimension that diverges outwardly as it approaches the ankle zone. The ankle zone, at or approaching a lower or free end thereof, may have a slight concave curvature.
Preferably, the sole plate is of substantial width compared to the ankle zone. It may comprise a heel portion and a toe portion. Preferably, the heel portion has a complementary or corresponding curvature to the ankle zone where they abut with each other.
A resilient sole pad may be affixed to an underside of the sole plate in any suitable manner, eg by adhesive or the use of fasteners. Preferably, the sole plate is capable of being mounted to the underside of the ankle zone at a designated point of 90 to110mm from a toe end of the sole plate. Through the provision of two sole plates, it allows for the plurality of foot sizing ranging from 23cm-30cm. Suitably, for this purpose, the sole plate and ankle zone may be provided with holes which may be aligned to receive fasteners, such as bolts, there through to secure the sole plate to the ankle zone at selected positions. Suitably, two co-aligned holes are provided in the ankle zone and sole plate.
Preferably, the sole plate is of substantially the same width as the ankle zone. Preferably, the heel portion is also substantially curved suitably on substantially the same radius as the leading end of the toe
portion.
The upper mounting shin portion of the J-shaped pylon may be secured to a mounting bracket, for example, by any suitable form of releasable attachment means, such as bolts or other suitable fasteners, to enable the upper mounting shin portion to be fixed to a distal end of a leg stump socket. The leg stump socket has a T-shaped bracket attachable thereto. Preferably, the bracket has a top flange, which is fixed to or fixable to the socket and a leg flange to which the mounting portion may be secured. Alternatively, the upper shin portion can be laminated directly to the distal end of the leg stump socket.
The prosthetic device of the invention stores energy upon heel strike of the sole plate, with weight applied in the gait cycle, thereby transferring energy during heel strike-forward to mid foot (flat foot) and releases energy at toe-off point of sole plate to provide a stable and controlled propelling lift or thrust to the prosthetic device to aid in achieving a natural gait.
The sole plate being fixed to the ankle zone, as described above, is capable of transferring smooth constant energy release from the heel strike through to toe-off of the sole plate during the gait cycle without lag, hesitation, jolting and/or braking, as a result of its one-piece design and fabrication. This is in contrast to prior art devices, such as US Patent No 4,822,363, that incorporate a releasable and attachable sole plate which has to transfer energy release through two separate members (ie. sole plate and pylon) to achieve energy release during the gait cycle.
The prosthetic device of the present invention will accommodate angled or uneven terrain without the use of a separate ankle joint through the characteristics of the device that facilitate a continuous smoother transference of stored energy from heel strike through to toe-off. The device may include a plurality of toe and heel sections, wherein each of the toe and heel sections may be buffed to facilitate foot sizing.
The prosthetic device of the invention is further capable of minimizing torsional movements and will accommodate stable and controlled lateral medial movements. Increased knee control allows increased ease of roll over of sole plate dissipating inertia and, thus, providing a smoother transition of movement regardless of the intensity of heel strike and mid-strike and toe-off.
Preferably, the J-shaped pylon has a shank comprising both the upper shin mounting portion and the lower shin portion that has a uniform thickness and width for all weight categories. It can be cut off where required and adjusted to the wearer without affecting the above stated performance factors.
BRIEF DESCRIPTION OF THE DRAWINGS
In order that the invention may be more readily understood and put into practical effect, reference will now be made to the accompanying drawings that illustrate a moulded product of the invention in the form of a prosthetic device which is a preferred embodiment of the invention and wherein:
FIG. 1 is a perspective view from the rear of the prosthetic device according to an embodiment of the invention;
FIG. 2 is a side elevation of the prosthetic device according to an embodiment of the invention fitted to a stump socket;
FIG. 3 is a front view of the prosthetic device detached from the stump socket and with mounting bracket removed;
FIG. A is a plan view along line A-A of FIG. 2;
FIG. 5 is a plan view of the sole plate;
FIGS. 6 and 7 are perspective views illustrating steps (a) and (b) of the method of the invention;
FIGS. 8 to 10 show drums that may be used in the method of the invention in FIGS. 6 and 7 having cutting lines or grooves arranged at varying orientations;
FIGS. 11 to 13 show the formation of pre-pregs with fibres arranged in longitudinal orientation;
FIGS. 14 to 18 show the formation of pre-pregs having fibres arranged in an intersecting orientation; and
FIG. 19 is a general flow chart of a preferred embodiment of the method of the invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring to the drawings and, firstly, to FIGS. 1 and 2, there is illustrated a prosthetic lower limb device 10 having a pylon 11 of generally J-shaped configuration in side elevation and which has an upper shin mounting portion 12, a lower shin portion 13, and a ankle zone 14.
As illustrated and as more clearly shown in FIG. 2, the upper shin mounting portion 12, the lower shin portion 13 and the ankle zone 14 are of substantially uniform thickness. There is also provided a sole plate.
As best shown in FIG. 3, the J-shaped pylon 11 has a constant width from the upper mounting portion 12 to a point 15. The lower shin portion 13 diverges symmetrically outwards the longitudinal axis of pylon 11 designated by Y-Y, thereby increasing in width to a second point 16, from which the J-shaped pylon 11 continues at a substantially constant width forming ankle zone 14.
As shown in figs 1 to 2, the prosthetic lower limb device 10 also includes a T-shaped bracket 18 that has a leg 19 to which the upper mounting portion 12 of the J-shaped pylon 11 can be bolted via bolts 20. The T-shaped bracket 18 also includes a top flange 21 which can be laminated directly to a stump socket 22. Alternatively, the top flange 21 may have a variety of alignment connectors adjoined to it and then connected to the bottom of the stump socket 22 to provide adjustment and angle alignments to fine tune gait movements and complement socket fit.
Fixed to the underside of the ankle zone 14 is an integrally formed sole plate 23, which is a one-piece component that incorporates in tandem both the heel portion 17A and toe portion 17. The toe portion 17 is slightly concave on its upper side and extends forward from bolts 26 which interconnect pylon 11 to sole plate 23 while the heel portion 17A is slightly convex on its upper side and extends rearward from bolts 26. The sole plate 23 is substantially the same width as ankle zone 14. There is
also provided a sole pad 27.
As shown also in FIGS. 4 and 5, there is provided in both sole plate 23 and pylon 11 a series of spaced pairs of co-aligned apertures 24 and 25 to permit the sole plate 23 to be secured to the ankle zone 14 by suitable bolts 26 through aligned apertures at a number of locations. As is apparent in FIG. 5, the leading end of the toe section 17 is of part circular form as is the heel end 17A of the sole plate 23. The above arrangements allow a variety of adjustments for the toe section 17 relative to the heel plate 23 of the prosthetic device 10, thus, permitting the toe section 17 and heel section 17A and sole plate 23 to accommodate subtle variations in the gait.
A resilient sole material, such as a rubber or urethane pad 27, may be affixed to the underside of the sole plate 23 covering both the toe portion 17 and the heel portion 17A, and it extends continuously along the entire length of the sole plate 23. The rubber/urethane pad 27 imparts flexibility to the prosthetic lower limb device 10 and helps to absorb heel strike or torque loads that may be applied at the heel or axially along the lower shin portion 13.
Further, the rubber or urethane pad 27 also provides energy dampening and increased comfort to the wearer. Typically, the rubber or urethane pad 27 is affixed in position by suitable adhesives. The rubber or urethane pad 27 can act as a non-slip surface to enable the prosthetic lower limb device 10 to be used without shoes.
The configuration and design of the main support or
J-shaped pylon 11, as described above, enable all stress concentrations to be dispersed more evenly from the shin-mounting portion 12, through the lower shin portion 13 and Into the ankle zone 14. The sole plate 23 is designed to provide greater stability and control of medial and lateral and for and aft movements.
Furthermore, the prosthesis of the present invention and method of construction also increases the intrinsic strength and durability of the prosthetic tower limb or leg, which facilitates uniformity in a single dimensional design for all weight categories as well as novelty of resiliency rejoinder and return energy of the total prosthesis.
It also facilitates distinctive variations of resiliency rates, smoother transition from heel impact to mid-strike to toe-off and allows better torsion movements, which can accommodate the many different exoskeleton and endoskeleton frames, body types and activity requirements of amputees, and a reduction in thigh and lower-back muscle fatigue and strain, compared to other prior art prostheses.
The resulting J-shaped pylon 11 preferably has uniformity of thickness that extends from the upper mounting portion 12 and extends through the lower shin portion 13 through the ankle zone 14. The shape of sole plate 23 as shown facilitates smoother controlled toe-off. Furthermore, the configuration and construction of the J-shaped pylon 11 provides effective resilience and return energy of the total prosthesis 10 from upper shin mounting portion 12 through to the ankle zone 14 with the improved process of manufacture avoiding the necessity of prior art

prosthesis require a variety of distinctive dimensional (width and/or thickness) pylons, heel plates/sole members to vary their rigidity.
Typically, the length of the J-shaped pylon 11 to the lower surface of ankle zone 14 can vary from 255mm to 368mm. This, again, can be heightened through an increase of sole thickness (maximum 20mm), attachment of extension wedges to the top of T- shaped bracket 18 (3cm) and/or extension to the underside of the socket 22 (maximum 7.5cm). These methods of increasing prosthesis lower limb height will not influence performance of the prosthetic lower limb 10. The width of the J-shaped pylon 11 typically increases from 45mm at the mounting portion 12 and diverges outwardly at the point 15 to the position 16 (for a length of 80mm) to a width of 67mm, which then stays constant until ankle zone 14. Typically, the sole plate 23 also has a width of 67mm.
The centres for holes 24 in FIG. 5 and holes 25 in FIG. 4 are typically positioned 15mm from the side edges of the sole plate 23 and ankle zone 14, respectively. The holes 24 in the sole plate 23 may be positioned between 90mm and 110mm from the front edge of the plate 23 while the holes 25 in the ankle zone 14 are suitably co-aligned with the holes 24 in the sole plate 23. This will allow for an increase or decrease in foot sizing. It should be highlighted that the above dimensions may be varied.
The length of the upper shin-mounting portion 12 can be cut no less than 55mm to point 15 of the lower shin portion as shown in FIG 3 and adjusted to the wearer's requirement without affecting its
performance. All of the J-shaped pylon 11 and sole plate 23 substantially have the same thickness, width and other dimensions throughout all weight classes from 30kg to 130kg at 10kg intervals. This is achieved through the novel method of the invention.
In the present invention, single-dimensioned mould cavity moulds may be used for the moulding of J-shaped pylon 11 and sole plate 23. Thus, the J-shaped pylon will have uniform dimensions in thickness, in width, shape and sizes for all classes of weight categories. Similarly, the sole plate 23 will also have uniformity in dimensions for thickness, width, shape and sizes for all classes of weight categories.
The toe section 17 and heel section 17A of the sole plate 23 can be buffed down to the appropriate size as required to provide for the increase in toe and/or heel rigidity to lessen the downward motion of heel strike length and/or toe-off.
In relation to FIG. 6, it will be noted that carbon or glass filament 30 is unwound from a carbon bobbin 31 that is mounted and supported by axle 32. Axle 32 will rotate when the drum 36 pulls filament 30. Filament 30 is passed through a resin bath 34 containing the preferred epoxy resin solution 35. After passing through resin bath 34, the resin-impregnated filament 30A is then wound onto the drum 36 which has a sheet of release paper 37, preferably silicone coated release paper, attached thereto, wherein ends 38 and 39 may be overlapped and affixed together by double-sided tape at 40, so as to provide a continuous sheet of release paper 37 on drum 36. Resin-impregnated filament 30A may
then be wound onto release paper 37 as drum 36 rotates. Drum 36 is being driven by suitable mechanical means (not shown) coupled to axle 41. Simultaneously as it rotates, the resin bath 34 together with axle 32 may travel in a linear direction indicated by arrows A or B causing the resin-impregnated filament 30A to be evenly spaced and laid (at a predetermined fibre area weight or fibre density) onto release paper 37, creating an intermediate pre-preg sheet 48A (in FIG. 12) from successive loops 42, as shown. Each of the successive loops 42 will overlap the preceding loop as they are wound onto the release paper 37 by the rotation of drum 36. The result is an intermediate pre-preg sheet 48A (in FIG. 12) that has binding integrity of its fibres from each resin-impregnated filament 30A and the intermediate pre-preg sheet 48A can be separated from release paper 37. Overlapping resin-impregnated filaments 30A are shown constituting the final appearance of sheet 48A at 42A.
In an alternative arrangement, as shown in FIG. 7, the drum 36 may reciprocate in either direction A or B in relation to the stationary resin bath 34 and axle 32 so as to provide for the same result as described in FIG. 6. It will, however, be appreciated that the FIG. 6 arrangement is preferred.
It will be noted from FIGS. 8, 9 and 10 that drum 36 may be provided with elongate grooves or cutting lines 43, 44 and 45 so as to facilitate cutting and removal of the composite sheet 46 from drum 36 at three cutting angles, typically but not exclusively at 0° or parallel to axle 41 for cutting line 43 as shown in FIG. 8, at 60° to axle 41 for cutting line 44
as shown in FIG. 9, or at 45° to axle 41 for cutting line 45 as shown in FIG.10. Cutting lines of other angles (although not shown in FIGS 8, 9 and 10) may be used to provide other intersecting angles for the unidirectional pre-pregs.
It will also be appreciated that cutting lines 43, 44,45 or lines of other angles, may be provided on the same drum 36 or such cutting lines may be provided on different drums 36. However, having a plurality of cutting lines on the same drum is preferred for versatility and cost reasons.
FIGS. 11 to 13 show the cutting of composite sheet 46 by cutting knife 47 along cutting line 43 so as to provide for an intermediate pre-preg sheet 48A. The intermediate pre-preg sheet 48A is then cut to the preferred shape and sizes as shown in pre-preg 49. Each intermediate pre-preg sheet 48A can provide for multiple cuttings of pre-pregs 49 having longitudinal or 0° carbon or glass fibres as shown. The example shown in FIG. 13 illustrates pre-preg 49 having a narrow part 50 and a broader part 51 as required by the preferred design. The cutting and removal of pre-pregs 49 leaves gaps 52 in sheet 48A. Resin-impregnated filament 30A are shown in longitudinal orientation or 0°.
In a variation of the procedure described above, pre-pregs 49 may be formed not only by longitudinal orientation of the fibres (i.e.O0) but also by transverse or latitudinal orientation (i.e.90°) using intermediate pre-preg sheet 48A.
FIG. 14 shows the cutting of composite sheet 46 along
cutting line 44 so as to provide for intermediate sheet 48B shown in FIG. 15, which is then provided with crease or fold lines 52, 53, 54 and 55. The folding begins with part 58 being folded along fold line 55 as shown by arrow E, followed by part 59 being folded along fold line 54, as shown by arrow F. Subsequently, part 57 is folded along fold line 53, as shown by arrow D, and lastly, part 56 is folded along fold line 52, as shown by arrow C.
Alternatively, part 60 may be folded along fold line 54, as indicated by arrow G, instead of part 59 along fold line 54 as indicated by arrow F. This procedure is further illustrated in FIGS. 16 and 17 to provide a final folded sheet 61 (shown in FIG. 17), from which multiple pre-pregs 62 (shown in FIG. 18) may be cut as shown in phantom in FIG. 17, leaving gaps 65. FIG. 18 also shows a pre-preg 62 having intersecting fibres from the resin-impregnated filaments 30A. The intersecting fibres are from the parts 56, 57, 60, 59 and 58 being folded along fold lines 52, 53, 54 and 55 back upon themselves.
Optimum pliability rates, compressive strength, dynamic endurance, fore-and-aft and torsional rigidity in the various weight categories (30-130kg), may be achieved in the J-shaped pylon 11 and sole plate 23 (in FIG.1) by various carbon/carbon or carbon/glass fibre combinations with variations in fibre area weight and fibre orientation. All weight categories (30-130kg) in a preferred embodiment of the invention have the same number of layers of laminates in the construction.
The intrinsic characteristics and mechanical strength of the
preferred carbon and glass fibres has created a variety of possible configurations in material compositions, fibre area weight and fibre orientations and sequencing to optimise the compressive strength, flexibility, durability, dynamic endurance, fore-and-aft and torsional rigidity in a preferred embodiment. Carbon fibre possesses much higher tensile strength and tensile modulus as compared to glass fibres. However, glass fibres, though less strong, have higher flexibility and fatigue endurance. Higher percentage of carbon fibres and lower percentage of glass fibres in the construction will result in higher stiffness and strength in a preferred embodiment and flexibility will increase with a reduction in tensile strength if we use a higher percentage of glass fibres.
Configurations of fibre orientation is another element in the present invention. Typically, placing longitudinal or 0° fibres along and parallel to the principle axis of J-shaped pylon 11 and sole plate 23 will result in very low torsional strength but very high stiffness, very high tensile and high compressive strength. Other fibre angles such, as 30°, 45° or 60° possess much higher torsional strength but lower tensile or compressive strength. It must be highlighted that the intrinsic mechanical properties of carbon and glass fibres are very different from each other and therefore it is natural to expect that their 0°, 30° and 45° angles produce very different results in torsion, tensile strength and compressive strength and this provides more options to configure and to optimise the compressive strength, flexibility, durability, dynamic endurance, fore-and-aft and torsion rigidity of each weight category in a preferred embodiment.
Typical carbon/carbon and carbon/glass compositions for the J-shaped pylon 11 and sole plate 23 are set out in the Table attached hereto.
The process of the invention ensures that all the fibres during resin impregnation are thoroughly "wetted" and properly impregnated with the epoxy resin. Typically, this method will produce carbon and glass pre-preg having a resin content range from 35% to 50%. The resin content is higher than most of the commercially available UD pre-preg. The epoxy resin functions as a glue to bind and encapsulate all fibres together. Higher resin content will ensure sufficient resin flow during moulding and will also provide a greater degree of control in the cross linking process, giving a much improved resin/fibre matrix. The result is an increase in strength and durability in a preferred embodiment.
All conventional lower limb prosthetic devices are constructed from UD longitudinal fibres in their main core with continuous and uninterrupted woven latitudinal or woven angular fibres on the outer layers to improve their torsion strength. The use of pre-preg 49 (having either 0° or 90° degree fiber orientation) and pre-preg 62 (having other intersecting fiber orientation) in the present preferred embodiment creates a totally new concept and method of construction for moulded products generally inclusive of the lower limb prosthetic device of the invention and is uniquely different from prior art methods.
In this present invention, fibre filaments do not have to be continuous and uninterrupted as shown by the method of producing pre-
preg 49 and 62. It must be noted that the use of non-continuous fibre filaments constitutes a significant feature of the prosthetic device of the present invention.
FIG. 19 refers to the preferred flow chart for the processes of the present invention in relation to manufacture of moulded products inclusive of lower limb prosthetic device. Epoxy resin solution may be formed by mixing the resin, catalyst, additives and solvent in stipulated proportions. The epoxy resin solution may have a 60% to 70% solid content with a cure time of 30 min at 130° degree Celsius and may possess toughness, flexibility, good thermal stability and chemical resistance, and having good bonding strength with the carbon and glass fibres which are the preferred fibres for use in the present invention.
This method of the invention allows carbon and/or glass unidirectional pre-pregs to be produced with a wide selection of fibre area weights (ranging from 60grams to SOOgrams per square meter), resin content (ranging from 35% to 50% by weight) and fibre orientations and sequencing to be employ and it also provides the flexibility to "choose and optimize" pre-pregs from the various combinations of material compositions, fibre area weight, fibre orientation and resin content that are available.
Typically, the carbon and glass fibres used in the preferred method of the present invention, are high strength filaments. The preferred drum wound technique ensures that all the fibres during resin impregnation are thoroughly "wetted" and properly impregnated with the
epoxy resin. With adroit control in resin viscosity during the resin impregnation process, it is possible to control resin content within +2%. Controlled and consistent resin content are preferable in the maintenance of compressive strength, durability, dynamic endurance, pliability rates, fore-and-aft and torsional rigidity.
The intermediate pre-preg sheets 48A and final folded pre-preg sheet 61 may be subjected to force drying in an oven to remove solvents and any other unwanted volatile components in the epoxy resin. Forced drying also makes the pre-preg sheets less tacky and more suitable for handling in the lay-up process. Suitable oven specifications are temperature of 50-65°C and drying time of 3 to 4 hours. Subsequently after the forced drying process, each intermediate pre-preg sheet 48A and final folded pre-preg sheet 61 may be weighed and cut into pre-preg 49 or pre-preg 62 as appropriate.
It must be highlighted that weighing of the intermediate pre-preg sheets 48A and final folded pre-preg sheet 61 after forced drying is a desirable aspect of the process of the invention. This is to segregate pre-pregs that falls in the high or low end of the resin content range, and to combine these pre-pregs appropriately so that the weight of the moulded J-shaped pylon 11 or sole plate 23 remains relatively constant. As an example, a pre-preg having high resin content may be used in conjunction with another that has low resin content during lay-up process.
After the lay-up of successive layers of pre-preg 49 and pre-preg 62 in the respective compression mould cavity, the compression

mould may be heated to 135°C-150°C (and more preferably 140°C) suitably in combination with a hydraulic pressure of 200 kg/cm2 using a 200mm diameter hydraulic piston.
After curing, de-moulding is undertaken to remove the moulded members, which are then prepared for assembly and final cosmetic treatment.
It will be appreciated from the foregoing that in view of the fact that the moulded product of the invention can be made from a mould cavity of similar dimensions regardless of weight that this feature will also apply in a preferred embodiment to the moulded product of the invention such as the J shaped pylon or the sole plate.
It therefore will be appreciated from the foregoing that the process of the invention provides a lower leg prosthesis which has considerable advantages over the prior art as will be apparent from the foregoing description.
EXAMPLES EXAMPLE I
A preferred method of lay up or sequencing of both pre-pregs 49 and 62 is described below in relation to manufacture of a J shaped pylon.
All weight categories (30kg-130kg), in this preferred method, have the same number (58) of layers with variations to the fibre sequencing and fiber orientation to achieve the varied pliability rates for each weight category, viz:
30kg to 40kg - pylon 345g ±5g, 38 layers of 60° fiber and 20 layers of 0° and 90° fiber combination.
40kg to 50kg - pylon 345g ±5g, 38 layers of 60° fiber and 20
layers of 0° fiber combination.
50kg to 60kg - pylon 345g ±5g, 38 layers of 45° and 60° fiber
combination with 20 layers of 0° and 90° fiber combination.
60kg to 70kg - pylon 345g ±5g, 38 layers of 45° and 60° fiber
combination and 20 layers of 0° fiber.
70kg to 80kg - pylon 345g ±5g, 38 layers of 45° and 20
layers of 0° and 90° fiber combination.
80kg to 90kg - pylon 345g ±5g, 38 layers of 45° and 20
layers of 0° fiber.
90kg to 100kg - pylon 345g ±5g, 38 layers of 30° and 45°
fiber combination and 20 layers of 0° and 90° fiber
combination.
100kg to 110kg - pylon 345g ±5g, 38 layers of 30° and 45°
fiber combination and 20 layers of 0° fiber.
110kg to 120kg - pylon 345g ±5g, 38 layers of 30° fiber and
20 layers of 0° and 90° fiber combination
120kg to 130kg - pylon 345g ±5g, 38 layers of 30° fiber and
20 layers of 0° fiber.
For all pylon categories (30-130kg), the carbon/carbon pre-preg lay-up sequences are preferably the same. Thus, for the pylon having 58 layers which comprise 38 layers of angled fiber and 20 layers of 0° and 90° fiber combination, the lay-up sequence is 8 layers of angled carbon fiber with FAW 100 at 0,12mm, 6 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm, 10 layers of angled carbon fiber with FAW (Fibre Area Weight) 100 at 0.12mm, 6 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm, 10 layers of angled carbon fiber with FAW 100 at 0.12mm, 8 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm and 10 layers of angled carbon fiber with FAW 100 at 0.12mm. EXAMPLE H
Maximisation of pliability rates, dynamic endurance, compressive strength, fore-and-aft and torsional rigidity of the different weight categories (30-130kg) may be achieved in the sole plate by a combination of carbon fibre angles (0°, 30°, 45°, 60° and 90°) and glass
fibre angles (30°, 45° and 60°), varied fibre lengths, fibre alignment (using lateral, transverse and diagonal directions), combined carbon layer thicknesses (0.12mm FAW 100/sq.m and 0.15mm FAW 150g/sq.m) and/or glass fibre layer thickness (0.16mm FAW 126g/sq.m).
All weight categories discussed above (30kg to 130kg) preferably have the same total number (52) of layers for either the entire carbon or combined carbon/glass fibre sole plate. Through the variations in the lay-up sequencing and fibre alignment for both carbon/carbon and carbon/glass fibre, the varied pliability rates for each weight category have been achieved, viz:
30kg to 40kg - Sole Plate 190g ±5g, Carbon/Glass
50%/50%
40kg to 50kg - Sole Plate 190g ±5g, Carbon/Glass
50%/50%
50kg to 60kg - Sole Plate 190g ±5g, Carbon/Glass
70%/30%
60kg to 70kg - Sole Plate 190g ±5g, Carbon/Glass
70%/30%
70kg to 80kg - Sole Plate 190g ±5g, Carbon 100%
80kg to 90kg - Sole Plate 190g ±5g, Carbon 100%
90kg to 100kg - Sole Plate 190g ±5g, Carbon 100%
100kg to 110kg - Sole Plate 190g ±5g, Carbon 100%
110kg to 120kg - Sole Plate 190g ±5g, Carbon 100%
120kg to 130kg - Sole Plate 190g ±5g, Carbon 100%
For the following sole plate weight categories (30-130kg), the carbon/carbon and carbon/glass pre-preg lay-up sequence having regard to pre pegs 49 and 62 are:
30 to 40kg - 16 layers of 60° carbon fiber with FAW 100 at 0.12mm, 10 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm and 26 layers of 60° glass fiber with FAW 126 at 0.16mm
40 to 50kg - 16 layers of 60° carbon fiber with FAW 100 at 0.12mm, 10 layers of carbon 0° with FAW 150 at 0.15mm and 26 layers of 60° glass fiber with FAW 126 at 0.16mm
50 to 60kg -26 layers of 60° carbon fiber with FAW 100 at 0.12mm, 10 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm and 16 layers of 60° glass fiber with FAW 126 at 0.16mm
60 to 70kg - 26 layers of 60° carbon fiber with FAW 100 at 0.12mm, 10 layers of carbon 0° with FAW 150 at 0.15mm and 16 layers of 60° glass fiber with FAW 126 at 0.16mm
70 to 80kg - 36 layers of 45° and 60° carbon fiber combination with FAW 100 at 0,12mm, 16 layers of carbon 0° and 90° combination with FAW 150 at 0.15mm
80 to 90kg - 36 layers of 45° and 60° carbon fiber combination with FAW 100 at 0.12mm, 16 layers of carbon 0° with FAW 150 at 0.15mm
90 to 100kg - 36 layers of 45° carbon fiber with FAW100 at 0.12mm, 16 layers of carbon fiber 0° and 90° carbon fiber combination with FAW 150 at 0.15mm
100 to 110kg - 36 layers of 45° carbon fiber with FAW 100 at 0.12mm, 16 layers of carbon fiber 0° with FAW 150 at 0.15mm
110 to 120 kg - 36 layers of 30° and 45° carbon fiber combination with FAW 100 at 0.12mm, 16 layers of carbon fiber 0° with FAW 150 at 0.15mm
120 to 130 kg - 36 layers of 30° carbon fiber with FAW 100 at 0.12mm, 16 layers of carbon fiber 0° with FAW 150 at 0.15mm.
(Table Removed)

We Claim:
1. A method of construction of a prosthesis device for patients of various weight categories, said
method including the steps of:
(a) impregnating non-metallic fibers in a thermosetting resin whereby said impregnated fibers are placed to form a sheet of said fibers;
(b) folding the sheet by bending adjoining parts of the sheet along adjacent fold lines therebetween so that said fibres are placed in an intersecting orientation to form a prepeg (49) having a double layer of fibres in different planes with the fibres in each layer having a different angle of orientation to a longitudinal axis of the prepeg (49);
(c) cutting a plurality of pre-pregs from said sheet formed in step (b);
(d) forming layers of said pre-pregs (49) obtained from step (c) so that said layers are placed in stacked relationship in a mould cavity of a compression mould whereby the mould cavity has a constant volume for each of the various weight categories;
(e) compression moulding at elevated temperature: and
(f) removing the prosthesis from the compression mould.

2. A method as claimed in claim 1 comprising a sheet as obtain from step (a) said sheet is made of drum (36) winding technique whereby said impregnated fibres are would onto a drum (36) so as to provide an intermediate composite sheet (46) formed of the fibres supported on a sheet of release paper (37) on the drum (36), whereby upon removal of the release paper (37), the sheet formed by step (a) is obtained by cutting the intermediate sheet as it is supported on the drum (36).
3. A method as claimed in claim 1 wherein the said sheet is made up of hot melt technique the same is being made after hot melt resin impregnation of the fibres being laid onto a continuous sheet of release paper(37) and subsequently stored as rolls.
4. A method as claimed in claim 1 wherein in step (d) layers of said pre-pegs having fibres placed in an intersecting orientation are mixed with layers of pre-pegs which have all of their fibres placed in a latitudinal and/or longitudinal orientation.
5. A method as claimed in claim 1 wherein in step (d) layers of said pre-pegs having fibres placed in an intersecting orientation are alternated with layers of pre-pegs having all of their fibres placed in a latitudinal and/or longitudinal direction.
6. A method as claimed in claim 1 wherein in step (d) there is a lay up sequence in the mould cavity the said layers of pre-pegs having fibres are being placed in an intersecting orientation being followed by layers of pre-pegs having their fibres placed in a longitudinal and/or latitudinal orientation followed by layers of pre-pegs having their fibres placed in an intersecting orientation.

7. A method as claimed in claim 1 wherein in step (d) successive layers are formed of pre-pegs having fibres placed in an intersection orientation which alternate with pre-pegs having fibres placed in a longitudinal and/or latitudinal orientation.
8. A method as claimed in claim 1 wherein in step (c) the intermediate sheet is cut at a variety of different angles selected from the group consisting of 15°, 221/2°, 30°, 45° and 60° so that the final sheet has sloping sides having an acute angle to vertical before folding of the final sheet upon itself to form said pre-peg.
9. A method as claimed in claim 8 wherein the cut angle is selected from 30° and 45°.
10. A method as claimed in claim 2 wherein the cutting of the intermediate sheet is carried out by provision of cutting lines(43, 44, 45) or grooves which are formed in an outer surface of the drum (36) at an angle selected from the group consisting of 15°, 221/2°, 30°, 45° and 60° for pre-pegs of intersecting fibres.
11. A method as claimed in claim 4 wherein said pre-pegs having fibres placed in a latitudinal and/or longitudinal orientation are formed from an intermediate sheet which intermediate sheet is cut at an angle of 0° for longitudinal fibres and 90° for latitudinal fibres having regard to a longitudinal axis of a drum (36) supporting the intermediate sheet.
12. A method as claimed in claim 1 wherein step (d) is carried out in a mould cavity having the same dimensions for different weights or different weight categories of moulded product.
13. A prosthesis device constructed by a method as claimed in claim 1 for patients of various weight categories formed from composite materials having layers of non-metallic fibres impregnated with a thermosetting resin, characterized in that said prosthesis device is formed at least partly from double layers of non continuous or cut fibres in different planes wherein the fibres are placed in an intersecting orientation wherein the fibres in each layer have an accurately predetermined different angle of orientation to a longitudinal axis of the prosthesis whereby said prosthesis has varying areas of fibre area weight along its length to provide said prosthesis with differential locations of stiffness and flexibility to enhance whereby thereof and said prosthesis has the same dimensions or number of layers of fibres regardless of the weight category of the patient.
14. A prosthesis device as claimed in claim 13 wherein the said device is in the form of a pylon.
15. A prosthesis device as claimed in claim 13 wherein the said device is in the form of a J shaped pylon (11).
16. A prosthesis device as claimed in claim 13 wherein the said device in the form of a sole plate (23).
17. A prosthesis device as claimed in claim 13 wherein the said device in the form of a combination of a J shaped pylon (11) attached to a sole plate (23) so as to define a lower limb prosthetic device.

18. A prosthesis device as claimed in claim 13 wherein the pylon at least in outer extremities thereof is formed from a laminate of alternating layers of said intersecting fibres with layer(s) of said fibres placed in longitudinal and/or latitudinal orientation.
19. A prosthesis device as claimed in claim 15 wherein the J shaped pylon (11) has an upper shin mounting portion, a lower shin portion and an ankle zone (14).
20. A prosthesis device as claimed in claim 19 wherein the upper shin mounting portion has a constant thickness and width.
21. A prosthesis device as claimed in claim 19 wherein the lower shin portion has a width that diverges outwardly as it approaches the ankle zone (14).
22. A prosthesis as claimed in claim 19 wherein the ankle zone (14) at or approaching a lower or free end thereof has a slight concave curvature.
23. A prosthesis device as claimed in claim 17 wherein the sole plate (23) is of width compared to an ankle zone (14) of the J shaped pylon (11).
24. A prosthesis device as claimed in claim 16 wherein the sole plate (23) has a heel portion and a toe portion.
25. A prosthesis device as claimed in claim 23 wherein the heel portion has a complementary or corresponding curvature to the ankle zone (14) where they abut each other.
26. A prosthesis device as claimed in claim 13 which has the same dimensions and shape regardless of weight.
27. A method of construction of a prosthesis device for patients of various weight categories substantially as herein described with reference to the foregoing description, examples, tables and the accompanying drawings.

Documents:

13-DELNP-2006-Abstract-(27-04-2009).pdf

13-DELNP-2006-Abstract-(30-04-2009).pdf

13-delnp-2006-abstract.pdf

13-DELNP-2006-Assignment-(29-04-2009).pdf

13-DELNP-2006-Claims-(27-04-2009).pdf

13-DELNP-2006-Claims-(30-04-2009).pdf

13-delnp-2006-claims.pdf

13-DELNP-2006-Correspondence-Others(12-05-2009).pdf

13-DELNP-2006-Correspondence-Others-(11-05-2009).pdf

13-DELNP-2006-Correspondence-Others-(27-04-2009).pdf

13-DELNP-2006-Correspondence-Others-(29-04-2009).pdf

13-DELNP-2006-Correspondence-Others.pdf

13-delnp-2006-description(complete).pdf

13-DELNP-2006-Drawings(12-05-2009).pdf

13-delnp-2006-drawings.pdf

13-DELNP-2006-Form-1(30-04-2009).pdf

13-DELNP-2006-Form-1-(27-04-2009).pdf

13-delnp-2006-form-1.pdf

13-DELNP-2006-Form-18.pdf

13-DELNP-2006-Form-2(30-04-2009).pdf

13-DELNP-2006-Form-2-(27-04-2009).pdf

13-delnp-2006-form-2.pdf

13-DELNP-2006-Form-26-(27-04-2009).pdf

13-DELNP-2006-Form-3-(27-04-2009).pdf

13-delnp-2006-form-3.pdf

13-delnp-2006-form-5.pdf

13-DELNP-2006-GPA(30-04-2009).pdf

13-delnp-2006-pct-210.pdf

13-delnp-2006-pct-409.pdf

13-DELNP-2006-Petition-137(12-05-2009).pdf

13-DELNP-2006-Petition-137-(11-05-2009).pdf

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Patent Number

234278

Indian Patent Application Number

13/DELNP/2006

PG Journal Number

23/2009

Publication Date

05-Jun-2009

Grant Date

15-May-2009

Date of Filing

02-Jan-2006

Name of Patentee

EGAN, JOSEPH, STEVEN

Applicant Address

178 AVOCA DRIVE, GREEN POINT, NEW SOUTH WALES 2251, AUSTRALIA.

Inventors:

#	Inventor's Name	Inventor's Address
1	EGAN, JOSEPH, STEVEN	178 AVOCA DIRVE, GREEN POINT, NEW SOUTH WALES 2251, AUSTRALIA.
2	CHING-HENG, WONG	APARTMENT BLOCK 795, WOODLANDS DRIVE 72, 08-09, 730795, SINGAPORE.

PCT International Classification Number

B29C 70/46

PCT International Application Number

PCT/AU2003/000796

PCT International Filing date

2003-06-25

PCT Conventions:

#	PCT Application Number	Date of Convention	Priority Country
1	PCT/AU2003/000796	2003-06-25	PCT