Title of Invention

A SINGLE OR MULTI-BLADED ROTOR

Abstract

A single or multi-bladed rotor for use with a fluid flow generator or reactor, said rotor comprising a central portion which is adapted to be mounted to a rotatable shaft, the rotor comprising at least one radial blade mounted at one end to the central portion, each blade having a leading edge and a trailing edge between its one end and its radially outer most extremity, said at least one blade having a fluid reactive face which has the configuration of at least one logarithmic curve conforming to the Golden Section, the at least one blade having a remote face which is remote from the reactive face, characterized in that said remote face also has the configuration of at least one logarithmic curve conforming to the Golden Section and said trailing or leading edge of the rotor has a curvature corresponding to at least one logarithmic. curve conforming to the Golden Section.

Full Text

This invention relates to a rotor and in particular a single or multi-bladeci rotor. The rotor according to the invention may be one which is intended to induce a fuid flow or alternatively may be one which is intended to be influenced fay a fluid flow, resulting in rotation of the rotor as a result of that influence. Examples of the application of the rotor according to the invention comprise use as a: fen blade which is used to generate an air flow; a turbine blade which is used to generate a fluid flow, an impeller for use in a pump or compressor, or one which is reactive to a fluid flow; or a propeller which may be used with watercraft and aircraft. Background art The invention comprises a development of the rotor which is disclosed in Australian Patent 694679 (AU-B-62946/96) which comprises a rotor which has a configuration which conforms generally to the curve of a logarithmic configuration substantially conforming to an equiangular spiral of the Golden Section which is also known as the Phi ratio. The content of Australian patent 694679 is incorporated herein by reference. Rotors such as impellers, propellers turbine blades and fan blades have scarcely changed over the years and are relatively inefficient. In addition, it is a common characteristic of such fan blades that their use results in the generation of a considerable amount of noise and in a fluid flow from the rotor which is turtiulent. Furthermore, where rotors are used in a liquid environment, if the rotors eire caused to rotate too fast, this can result in cavitation on the surface and tips of the rotor which not only reduces the operational efficiency of the rotor but can result in destructive influences on the rotor and the surrounding housing associated with the rotor. The discussion throughout this specification, of the background and prior art to the invention is intendsl only to faclitate an understanding of the present invention. It should be appredated that the discussion is not an acknowledgement or admission that any of the material referred to was part of the common general knowledge in Australia as at the priority date of the application. It is an object of this invention to provide a single or multi-btaded rotor which can react to or induce a fluid flow and whereby the usage of that rotor results in a reduction of the degree of extraneous turbulence and tip vortices exerted on the fluid in its passage past the rotor with the resultant energy loss and noise generation when compared to conventional rotors which are currently In use. Disclosure of the Invention Accordingly, the invention resides in a single or multi-bladed rotor for use with a fluid flow generator or reactor, said rotor comprising a central portion which is adapted to be mounted to a rotatable shaft, the rotor further comprising at (east one radial blade mounted at one end to the central portion, each blade having a leading edge and a trailing edge between its one end and its radially outer most extremity, said at least one blade having a fluid reactive face which has the configuration of at least one logarithmic cun/e substantially conforming to the Golden Section, the at least one blade having a remote face which is remote from the reactive face, said remote face also having the configuration of at least one logarithmic curve substantially conforming to the Golden Section, said trailing and/or leading edge of the rotor having a curvature corresponding to at least one logarithmic curve substantially conforming to the Golden Section. According to a preferred feature of the invention the one blade is mounted to the centra! portion and the central portion supports a countenweight positioned to balance the rotor in use. According to a preferred feature of the invention at least two blades are mounted to the central portion said blades being spaced angularly equidistant around the central portion, According to a prefened feature of the invention the curvature of the reactive face is uni-dimensional. According to one embodiment the curvature of the reactive face according to the at ieast one logarithmic curve substantially conforming to the Golden Section is about an axis which is substantially radial to the axis. According to another embodiment the curvature of the reactive face according to tfie at least one logarithmic curve substantially conforming to the Golden Section is about an axis which is substantially tangential to the rotation path about said axis. According to another embodiment the curvature of the reactive face according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis which is substantially coaxial with or substantially parallel with said axis. According to a preferred feature of the invention the curvature of the reactive face is bi-dimensional. According to one embodiment the curvature of the reactive face according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis which is substantially radial to the rotation path of the blade about said axis and an axis which is substantially tangential to the rotation path about said axis. According to another embodiment the curvature of the reactive face according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis which is substantially radial to the axis and an axis which is substantially coaxial with or substantially parallel with said axis. According to another embodiment the curvature of the reactive face according to the at least one logarithmic cun/e substantially conforming to the Golden Section is about an axis which is substantially tangential to the rotation path about said axis and an axis which is substantially coaxial with or substantially parallel with said axis. According to a preferred feature of the invention the curvatue of the reactive fece is three dimensional. According to one embodiment the curvature of the reactive face according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis an axis which is substantially ranial to the rotation path, an axis which is substantially tangential to the rotation path about said axis and an axis which is substantially coaxial with or substantiaffy parallel with said axis. According to a prefen^ed feature of the invention the trailing edgeofthe rotorhas a curvature corresponding to at least one logarithmic curve conforming to the Golden Section. According to a preferred feature of the invention the leading edge of the rotor has a curvature corresponding to at least one logarithmic curve conforming to the Golden Section. According to a preferred feature of the invention the leading edge and the trailing edge of the rotor has a curvature corresponding to at least one logarithrric curve conforming to the Golden Section. According to a preferred feature of the invention the rotor comprises a three bladed rotor. According to a preferred feature of the invention the rotor comprises a fan blade which is intended to induce or react to a gaseous flow past the rotor. According to a preferred feature of the invention the rotor comprises an aircraft propeller. According to a preferred feature of the invention the rotor comprises a watercraft propeller. According to a preferred feature of the invention the rotor comprises a pump rotor. According to a preferred feature of the invention the rotor comprises a turbine rotor. According to a preferred feature of the invention the rotor comprises a mixer rotor, According to a preferred feature of the invention the curvature of reactive face and remote face are of a suiDSlantialiy equivalent form. Accordingto a prefen^ed feature of the invention the curvature of the remote face is uni-dimensional. According to one embodiment the curvature of the remote face according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis which is substantially radial to the axis. According to another embodiment the curvature of the remote face according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis which is substantially tangential to the rotation path about said axis. According to another embodiment the curvature of the remote face according to the at least one loganthmic curve substantially conforming to the Golden Section is about an axis which is substantially coaxial with or substantially parallel with said axis. According to a preferred feature of the invention the curvature of the remote face is bi-dimensionai. According to one embodiment the curvature of the remote face according to the at least one logarithmic curve substantially conforming to.the Golden Section is about an axis which is substantially radial to the rotation path of the blade about said axis and an axis which is substantially tangential to the rotation path about said axis. According to another embodiment the curvature of the remote face according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis which Is substantially radial to the axis and an axis which is substantially coaxial with or substantially parallel with said axis. According to another embodiment the cun/ature of the remote face according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis which is substantially tangential to the rotation path about said axis and an axis which is substantially coaxial with or substantially parallel with said axis. According to a preferred feature of the invention the curvature of the remote face is three dimensional. According to one embodiment the curvature of the blades according to the at least one logarithmic curve substantially conforming to the Golden Section is about an axis an axis which is substantially radial to the rotation path, an axis which is substantially tangential to the rotation path about said axis and an axis which is substantially coaxial with or substantially parallel with said ax_is- The invention will be more fully understood in the light of the following description of several specific embodiments. Brief Description of the Drawings The description is made with reference to the accompanying drawings of which: Figure 1 is an isometric view of a rotor according to the first embodiment with the convex face uppermost; Figure 2 is a plan view of the rotor according to the first embodiment in which the convex face of the rotor is uppermost; Figure 3 is an inverted view of the rotor according to the first embodiment as shown at Figure 2; Figure 4 is a side elevation of the rotor according to the first embodiment; Figure 5 is a sectional view along the line 5-5 of Figure 2; Figure 6 is a schematic isometric view of the first embodiment illustrating the fluid flow that it is believed is generated by the rotation of liie rotor; and Fig 7 is a graphical illustration of the performars of the rotor of the first embodiment when compared to the performance of a widely marketed conventional domestic exhaust fan blade. Detailed Description of Several Embodiments The first embodiment shown In the drawings comprises a rotor which can be utilised as a fan blade in order to induce an air flow and in particular which can be used as the fan blade of an exhaust fan. As shown in the drawings, the rotor comprises a hub (12) which supports a set of three radial blades (11). The hub (12) is formed with a central aperture (13) which Is adapted to be mounted to a rotatable shaft which comprises, in the case of a fan blade intended to induce fluid flow, a drive shaft driven from a suitable motor. Each of the blades are formed with an internal reactive face (14) which is of a concave configuration and which has a three dimensional curvature whereby the curvature in each dimension is about an axis which is radial to the central axis of the rotor, an axis which is tangential to the central axis of the rotor and an axis which is coincidental or parallel tb the centra! axis of the rotor. In each case the curvature is in accordance with a logarithmic curve conforming to the Golden Section. As a result, the blades (11) jointly define a generally concave face of the rotor. In addition, each blade has a remote reactive face (15) which is remote from the reactive face (14) and which also has a three dimensional curvature of a convex nature whereby the cun/ature in each dimension conforms with a logarithmic curve according to the Golden Section, and whereby the curvature in each dimension is of the same form as the curvature of the reactive face (14) In each dimension. As a resutic. the remote faces (15) jointly define a generally convex surface of the rotor. Each blacte (11) is formed with a pair of generally radial edges (16) and (17) which due to the curvature of the blade are of differing lengths whereby one edge (16) has a greater length than the other edge (17). In addition, each edge has a curvature which conforms to a logarithmic curve conforming to the Golden Section. The 1an blade according to the first embodiment Is intended to be used in an exhaosttan to induce a flow of air from one space to another whereby with rotation of the fan blade such that the one edge (16) forms the leading edge of each blade, fluid flow will be induced past the fan blade from the convex face to the concave face. Because of the curvature of the reactive face of each of the radial blades of the embodiment, the fan blade induces a vortical fluid flow in the air both as it approaches the fan blade and as it exhausts from the fan blade as illustrated at Rgure 6. It has beer: fccHid that in use of the first embodiment the rotation of tbe rotor generates a fluid flow through the rotor in which the flowing fluid maintains its own inertia and if the rotor is stopped the fluid flow will continue through the rotor for a period of time because of such inertia. It is believed that this is at least in part due to the circumstance that ttie use of the rotor of the first embodiment results in the generation of a fluid flow in which the pathway for the fluid flow though the rotor {as distinct from conventional rotors) is constant in its geometry from a position in advance of the entry to the rotor to a position beyond the exit from the rotor. Examples of the First Embodiment A. An example of a fan blade according to the first embodiment has been constructed and used to replace the existing blade of an exhaust fan marketed under the name NUTONE by Nortec Inc. (exhaust fan model 686). The existing fan blade of that exhaust fan comprises a five bladed fan where the blades have a conventional configuration. The exhaust fan incorporating the existing fan blade was tested both with and without flow straightening means which was provided with the fan. In addition, the exhaust fan was modified by replacing the existing Ian blade with a fan blade according to the embodiment and the modified exhaust fan was tested both with and without the conventional flow straightener. Figure 7 illustrates the performance of each of the fan blades in a graphical form where the efficiency of the conventional exhaust fan and the modified exhaust fan is plotted against the volume flow rate generated by each exhaust fan where measures of the efficiency of the fan and the flow rate were determined at 2000 rpm, 3000 rpm, 3250 rpm and 4000 rpm. As a result of utilisation of the rotor according to the first embodiment, the efficiency of the fan was increased significantly and the flow rate generated from the fan also increased dramatically. B. In addition, a fan blade according to the first embodiment was utilised in an automotive cooling fan marketed under the name "Davies, Craig" by a company named Davies, Craig {model DCSL 10) as a result the following figures were determined. A second embodiment of the invention comprises a rotor of a similar form to that of the first embodiment where the other edge (17) comprises the leading edge of the rotor which is caused to rotate in the opposite direction to the rotor of the first embodiment. A third embodiment of the invention comprises a rotor of a similar form to^that of the first embodiment which is used as a propeller for use with watercraft. It is envisaged that the use of the third embodiment will enable the elimination or at least a reduction in the need for a surrounding shroud or duct which is often required with conventional propellers to improve their performance. According to a fourth embodiment of the invention a rotor of a similar form to that of the first embodiment is used as the impeller of a fluid mixer. According to a fifth embodiment of the invention a rotor of a similar form to that of the first embodiment is used as the impeller of a fluid pump. According to a sixth embodiment of the invention a rotor of a similar form to that of the first embodiment is used as the impeller of a compressor. According to a seventh embodiment of the invention a rotor of a similar form to that of the first embodiment is used as the turbine blade of a turbine. As a result of testing of rotors according to at least some of the embodiments described above It appears that the blades of the rotor uniquely replicates and match the lines of vorticity of a singular vortex. As a result the rotor creates a homogeneous fluid flow structure which is then aided In its stability by the inertia of the resultant fluid field (i.e. the rotor creates a single vortex)- Once rotating this singular vortex is both gyroscopic in nature and has a high rotating Inertia. Conventional propellers do not achieve this and if they are suddenly stopped the propeller interferes with the fluid flow pattern It has created In the body of fluid. In comparison testing has shown that rotors according to the embodiment do not demonstrate such interference with the fluid flow when they are stopped and that the fluid follow will continue until the angular momentum induced in the fluid fades. Throughout this specification (including the claims if present), unless the context requires othenwise, the word "comprise", or vartstrons such as "comprises" or "comprising", will be understood to imply the inclusion of a stated integer or group of integers but not the exclusion of any other integer or group of integers. It should be appreciated that the scope of the present Invention need not be limited to the particular scope of the embodiment described atiove. I CLAIM: 1. A single or multi-bladed rotor for use with a fluid flow generator or reactor, said rotor comprising a central portion (12) which is adapted to be mounted to a rotatable shaft, the rotor comprising at least one radial blade (11) mounted at one end to the central portion (12), each blade (11) having a leading edge (16) and a trailing edge (17) between its one end and its radially outer most extremity, said at least one blade having a fluid reactive face (14) which has the configuration of at least one logarithmic curve conforming to the Golden Section, the at least one blade having a remote face (15) which is remote from the reactive face (14), characterized in that said remote face (15) also has the configuration of at least one logarithmic curve conforming to the Golden Section and said trailing (17) or leading edge (16) of the rotor has a curvature corresponding to at least one logarithmic curve conforming to the Golden Section. 2. The single bladed rotor as claimed in claim 1 wherein the one blade is mounted to the central portion (12) and the central portion (12) supports a counterweight positioned to balance the rotor in use. 3. The muhi-bladed rotor as claimed in claim 1 wherein at least two blades (11) are mounted to the central portion (12) said blades (11) being spaced angularly equidistant around the central portion (12). 4. The single or multi-bladed rotor as claimed in claim I or 2 wherein the curvature of the reactive face (14) is uni-dimensional. 5. The single or multi-bladed rotor as claimed in claim 4 wherein the curvature of the reactive face (14) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is radial to the axis. 6. The single or multi-bladed rotor as claimed in claim 4 wherein the curvature of the reactive face (14) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is tangential to the rotation path about said axis. 7. The single or multi-bladed rotor as claimed in claim 4 wherein the curvature of the reactive face (14) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is coaxial with or parallel with said axis. 8. The single or multi-bladed rotor as claimed in claim 1 or 2 wherein the curvature of the reactive face (14) is bi- dimensional. 9. The single or multi-bladed rotor as claimed in claim 8 wherein the curvature of the reactive face (14) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is radial to the rotation path of the blade (11) about said axis and an axis which is tangential to the rotation path about said axis. 10. The single or multi-bladed rotor as claimed in claim 8 wherein the curvature of the reactive face (14) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is radial to the axis and an axis which is coaxial with or parallel with said axis. 11. The single or multi-bladed rotor as claimed in claim 8 wherein the curvature of the reactive face (14) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is tangential to the rotation path about said axis and an axis which is coaxial with or parallel with said axis. 12. The single or multi-bladed rotor as claimed in claim 1 or 2 wherein the curvature of the reactive face (14) is three-dimensional. 13. The single or multi-bladed rotor as claimed m claim 12 wherein the curvature of the reactive face (14) accordmg to the at least one logarithmic curve conforming to the Golden Section is about an axis which is radial to the rotation path, an axis which is tangential to the rotation path about said axis and an axis which is coaxial with or parallel with said axis. 14. The single or multi-bladed rotor as claimed in any one of claims I, 2, 4 to 13 wherein the trailing edge (17) of the rotor has a curvature corresponding to at least one logarithmic curve conforming to the Golden Section. 15. The single or multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 14 wherein the leading edge (16) of the rotor has a curvature corresponding to at least one logarithmic curve conforming to the Golden Section. 16. The multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 15, wherein the rotor comprises a three bladed rotor. 17. The single or multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 16 wherein the rotor comprises a fan blade which is intended to induce or react to a gaseous flow past the rotor. 18. The single or multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 16 wherein the rotor comprises an aircraft propeller. 19. The single or multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 16 wherein the rotor comprises a watercraft propeller. 20. The single or multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 16 wherein the rotor comprises a pump rotor. 21. The single or multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 16 wherein the rotor comprises a turbine rotor. 22. The single or multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 16 wherein the rotor comprises a mixer rotor. 23. The single or multi-bladed rotor as claimed in any one of claims 1, 2, 4 to 22 wherein the ctirvature of reactive face (14) and remote face (15) are of a equivalent form. 24. The single or multi-bladed rotor as claimed in any one of claims 1 , 2, 4 to 22 wherein the curvature of the remote face (15) is uni-dimensional. 25. The single or multi-bladed rotor as claimed in claim 24 wherein the curvature of the remote face (15) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is radial to the axis. 26. The single or multi-bladed rotor as claimed in claim 24 wherein the curvature of the remote face (15) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is tangential to the rotation path about said axis. 27. The single or multi-bladed rotor as claimed in claim 24 wherein the curvature of the remote face (15) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is coaxial with or parallel with said axis. 28. The single or multi-bladed rotor as claimed in any one of claims I, 2, 4 to 22 wherein the curvature of the remote face (15) is bi-dimensional. 29. The single or multi-bladed rotor as claimed in claim 28 wherein the curvature of the remote face (15) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is radial to the rotation path of the blade (11) about said axis and an axis which is tangential to the rotation path about said axis. 30. The single or muhi-bladed rotor as claimed in claim 28 wherein the curvature of the remote face (15) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is radial to the axis and an axis which is coaxial with or parallel with said axis. 31. The single or multi-bladed rotor as claimed in claim 28 wherein the curvature of the remote face (15) according to the at least one logarithmic curve conforming to the Golden Section is about an axis which is tangential to the rotation path about said axis and an axis which is coaxial with or parallel with said axis. 32. The single or multi-bladed rotor as claimed in any one of claims I, 2, 4 to 22 wherein the curvature of the remote face (15) is three dimensional. 33. The single or multi-bladed rotor as claimed in claim 32 wherein the curvature of the blades (11) accordmg to the at least one logarithmic curve conforming to the Golden Section is about an axis an axis which is radial to the rotation path, an axis which is tangential to the rotation path about said axis and an axis which is coaxial with or parallel with

Documents:

in-pct-2002-0969-che abstract.pdf

in-pct-2002-0969-che claims-duplicate.pdf

in-pct-2002-0969-che claims.pdf

in-pct-2002-0969-che correspondence-others.pdf

in-pct-2002-0969-che correspondence-po.pdf

in-pct-2002-0969-che description(complete)-duplicate.pdf

in-pct-2002-0969-che description(complete).pdf

in-pct-2002-0969-che drawings.pdf

in-pct-2002-0969-che form-1.pdf

in-pct-2002-0969-che form-19.pdf

in-pct-2002-0969-che form-26.pdf

in-pct-2002-0969-che form-3.pdf

in-pct-2002-0969-che form-5.pdf

in-pct-2002-0969-che others.pdf

in-pct-2002-0969-che pct.pdf

in-pct-2002-0969-che petition.pdf