Title of Invention	"AN IMPROVED APPARATUS FOR CHARGING A SHAFT SECTION OF A FURNACE IN PARTICULAR A BLAST FURNACE
Abstract	This invention relates to an apparatus for charging a shaft furnace, in which each of plane faces of a second segment of a guiding member of a unit for distributing a burden over a cross section of the furnace is formed so that its first line of intersection with the first vertical plane passing through its geometric center and tangentially to a circle lying in a horizontal plane and having the center on the axis of the furnace and the radius equal to the distance from the furnace axis to the geometric center, the inclined angle " " to the horizontal plane, the intersection line© of all plane faces forming a polygonal line, exact subsequent length of the polygonal line, in a burden flow direction, making a greater angle of inclination with the horizontal plane than the preceding one, and a second line of intersection of each plane face with a second vertical plane passing through its geomettic center and the furnace axis is inclined at angle "beta" to the horizontal plane. With angle "beta" increasing with the burden flow.

Title of Invention

"AN IMPROVED APPARATUS FOR CHARGING A SHAFT SECTION OF A FURNACE IN PARTICULAR A BLAST FURNACE

Abstract

This invention relates to an apparatus for charging a shaft furnace, in which each of plane faces of a second segment of a guiding member of a unit for distributing a burden over a cross section of the furnace is formed so that its first line of intersection with the first vertical plane passing through its geometric center and tangentially to a circle lying in a horizontal plane and having the center on the axis of the furnace and the radius equal to the distance from the furnace axis to the geometric center, the inclined angle " " to the horizontal plane, the intersection line© of all plane faces forming a polygonal line, exact subsequent length of the polygonal line, in a burden flow direction, making a greater angle of inclination with the horizontal plane than the preceding one, and a second line of intersection of each plane face with a second vertical plane passing through its geomettic center and the furnace axis is inclined at angle "beta" to the horizontal plane. With angle "beta" increasing with the burden flow.

Full Text	1A The present invention relates to ferrous metallurgy, and more particularly, to an apparatus for charging a shaft furnace. The invention may be most successfully used in blast furnaces. As of now, in the quest to intensify the iron-making process the efforts are directed to improving the blast-furnace process through optimum distribution of a gas flow over the blast furnace shaft section, which determines the quality of iron produced, the specific fuel consumption for its production and the blast furnace output as a whole. The uniform distribution of the gas flow over the furnace section is attained by controlling the rate of blowing and changing the layer contours of ore and coke components of the burden which is fed into a throat zone by a charging device installed on the furnace cone. Therefore, the requirements that are placed upon the charging device are to provide a desired contour of the burden layer over the furnace cross section with minimum nonuniformity in the circumferential grain-size distribution of the burden in the throat zone, and, essentially, a controlled thickness of the burden layer charged. Conventional blast furnace charging apparatuses include a double-cone charging apparatus equipped with movable throat plates, which is disclosed in DE A 2125062. The above apparatus for charging a shaft furnace comprises a bin having an inlet and an outlet, the bin being connected through flanges with a top portion of the furnace. The bin outlet is located in the furnace chamber, within its throat zone, and closed by a cone-shaped locking member. The locking member is adapted to move vertically. The furnace throat zone is provided with movable plates which carry distributing plates with a reflecting surface facing the bin outlet. The plates are uniformly circumferentially 2 disposed and adapted to radially move along the guides which are rigidly fixed to the furnace shell. In operation of the apparatus, the locking member is displaced towards the furnace chamber, and a burden is admitted through an annular gap formed to the peripheral region of the throat zone. If the blast-furnace process is disturbed, it is required to change the contour of the charged burden layer. To this end, the plates are radially displaced towards the furnace axis until they reach a position in which the path of the falling burden intersects the surface of the distributing plates, which results in altering the burden flow direction so that the burden moves towards the furnace axis. The above prior art apparatus, however, changes the contour of the burden layer charged only in the peripheral annular region due to the restricted displacement of the movable plate, which reduces the potentials of the apparatus, limiting the burden laying control only to 1/3 the furnace radius. Most closely approaching the present invention by the combination of technical features and the achieved result is an apparatus for charging a shaft furnace, comprising a bin for a burden having an inlet and an outlet, a unit for distributing the burden over a cross section of the furnace, said unit being mounted in a throat zone beneath the bin outlet and adapted to rotate about the furnace axis. The burden distributing unit comprises a horizontal member having at least two guiding members disposed around its periphery, each of the guiding members being connected with the horizontal member and consisting of two segments which are arranged sequentially in the direction of the burden flow. A first segment is located in the immediate vicinity to the horizontal member, and a second segment is defined by at least two plane faces and has a burden shoot edge facing the furnace throat zone (WO Application No. 92/19776, C21B 7/20). 3 Owing to the design of the distributing unit, the burden body leaving the bin outlet is divided into at least two flows which form a charge layer in the throat zone with approximately even circumferential grain-size distribution. This is attained due to laying the burden pellets of the same size symmetrically about the furnace axis, thereby significantly reducing the nonuniformity of the circumferential burden weight distribution in the furnace. The uniform arrangement of the guiding members around the periphery with the first segment being disposed in the immediate vicinity to the horizontal member, makes it possible to change the radial direction of the burden flow to the circumferential one. On the guiding member second segments, the circumferential direction of the burden flow changes to a tangential one, or towards the furnace axis, under the effect of the resultant of frictional, centrifugal and Coriolis forces. This enables the burden to be charged to any throat region and provides the possibility to form a required stockline contour in the throat zone. This is attained by a single type of motion, in particular, by rotation of the burden distributing unit about the furnace axis. The above structural features of the charging unit provide the improvement in the blast-furnace process parameters and the reduction in energy losses. The rotary drive of the unit has a simpler structure. In operation, a burden portion is charged from the burden bin on the horizontal member of the burden distributing unit and further along the guiding members into the furnace chamber. A burden layer is formed in the furnace throat zone by virtue of rotation of the burden distributing unit. Owing to the possibility to change the rotational speed of said unit, the apparatus provides a desired stockline contour in the shaft furnace. This improves the blast-furnace process characteristics. However, a required stockline contour is not provided when laying the burden by the above apparatus in the region adjacent to the furnace axis, since the non-optimal 4 spatial orientation of the plane faces of the guiding member second segment hinders the admission of a sufficient amount of material to the furnace axial region. As a consequence, the optimum gas distribution over the furnace cross section is not provided, resulting in the increased coke consumption and some reduction in the output. In addition, in the prior art apparatus the position of plane faces of the guiding members fails to be unambiguously defined which makes the manufacture of the apparatus as such problematic, and further hampers the attainment of a desired stockline contour in the furnace throat zone. Summary of the Invention It is an object of the present invention to provide an apparatus for charging a shaft furnace, having a unit for distributing a burden over the furnace cross section, designed so that to provide a required stockline contour in the furnace throat zone with a highly uniform circumferential grain-size and weight distribution of the burden. The foregoing and other objects of the present invention are achieved in an apparatus for charging a shaft furnace, comprising a bin for a burden, having an inlet and an outlet, said bin being connected with a unit for distributing the burden over the furnace cross section, said unit being adapted to be mounted in the throat zone and rotate about the furnace axis beneath the bin outlet along a burden flow which is formed by a horizontal member having at least two uniformly circumferentially disposed guiding members, each of the guiding members being connected to the horizontal member and including two segments which are arranged sequentially in the burden flow direction, a first of the segments being disposed in the immediate vicinity to the horizontal member, while a second segment is defined by at least two plane faces and has a burden shoot edge which faces the furnace throat zone, wherein in accordance with the invention each 5 of the plane faces of the second segment is formed so that its first line of intersection with a first vertical plane passing through its geometric centre and tangentially to a circle lying in a horizontal plane and having the centre on the furnace axis and the radius equal to the distance from the furnace axis to the geometric centre is inclined at angle "a" to the horizontal plane, the intersection lines of all plane faces (25, 25a, 25b) forming a polygonal line, each sequential length of which in the burden flow direction has greater inclination angle "a" than the preceding one, and a second line of intersection of each plane face with a second vertical plane passing through its geometric centre and the furnace axis is inclined at angle "p" to a horizontal plane, with angle "p" increasing with the burden flow. The increase in inclination angle "a" of the plane faces in the burden flow direction provides the reduction in bonding forces between each subsequent plane face and the burden flow, promoting the burden descent from the guiding members. As a consequence, the material falls closer to the furnace axial region at a minimum rotational speed of the unit, providing the charging of the middle region of the throat zone. The design of the guiding member, with plane faces of the second segment simultaneously changing angles "p" of inclination to the furnace axis, changes the burden flow direction towards the furnace axis at low rotational speeds of the unit, providing the charging of the throat zone centre. The above design of the burden distributing unit allows the attainment of a required stockline contour by changing the rotational speed of the unit. This enables the peripheral region of the throat zone to be charged at a maximum rotational speed, the axial region to be charged at a minimum rotational speed and the middle region to be charged at intermediate values of the unit rotational speed. With the rotational speed of the distributing unit 6 being unchanged, the burden will be laid in the throat zone in the form of an annular ridge with a distinct apex. When the rotational speed of the distributing unit changes during the discharge from high to low, the burden is laid in the throat zone in a spiral, so that a layer with a smoothened surface is formed. Preferably the first segment of each guiding member comprises a trough with side wails having a height which is equal to 1/2 the segment width at the beginning of the segment and 1/5 the segment width at the end thereof. The trough-like configuration of the first segment results in forming a burden flow entering the second segment as a directed jet, which ensures the provision of a required weight ratio of coke and ore components in the vertical stock column over the entire furnace volume Preferably a bottom of the first segment trough at the connection with the surface of the second segment is deeper than the latter. This deepening amounts to 20 to 60mm which is about one-half an average diameter of burden particles charged into the shaft surface. Consequently, the lower plane of the guiding member trough portion will be lined with small charge fractions and have an optimally rough surface on which the burden flow will be formed. Owing to such configuration of the first segment, the trough bottom surface is afforded the protection against abrasive wear due to forming a burden layer on the first segment surface, which extends the life of the burden distributing unit. Moreover, the burden flow motion over the burden layer formed on the first segment of the guiding member results in a blended grain-size distribution of the burden charged into the throat zone of the furnace. With the unit being rotated, the above circumstance ensures that 7 the burden layer formed in the above region has a minimum nonuniformity in the circumferential burden grain-size distribution in the furnace throat zone. These and other objects and advantages of the invention will be best appreciated from the following detailed description of a preferred embodiment, taken in conjunction with the accompanying drawings in which: Fig. 1 is a schematic perspective view of an apparatus for charging a shaft furnace, with a partial cutout; Fig.2 is an enlarged perspective view of a unit for distributing burden over the furnace cross section, in accordance with the present invention; Fig.3 is a perspective view of a guiding member; Fig.4 is a view developed through section IV-IV of Fig.3 formed by first vertical planes; Fig.5 is a view developed through section V-V of Fig.3 formed by second vertical planes; , Fig.6 is a stockline contour in the furnace throat zone at a forward rotation direction of the charging unit; Fig.7 is a stockline contour in the furnace throat zone at a reverse rotation direction of the charging unit. An apparatus for charging a shaft furnace, such as a blast furnace, in accordance with the invention includes a burden bin 1 (Fig.1) connected with the furnace 2 via a casing 3 which is coaxial with the bin 1 and the furnace 2. The casing 3 accommodates a rotary drive of a unit 4 for distributing burden over the cross section of the furnace 2 and has a ring 5 for connection with the latter. The bin 1 has a burden inlet 6 closed by a cone-shaped locking member 7 and an outlet 8 closed by a cone-shaped locking member 9. The inlet 6 and the outlet 8 are concentric with the axis of symmetry of the bin 1. The cone-shaped locking members 7 and 9 are connected to vertical displacement drives (not shown in Fig.1) via bars 10 8 and 11, respectively. Burden is charged into the bin 1 through a hopper 12 which is mounted on the bin 1 and serves to accumulate a burden portion which is loaded, for instance, by a conveyor (not shown in Fig. 1). The unit 4 is connected with the top portion of the furnace 2 and disposed in its chamber in a throat zone 13 beneath the outlet 8 of the bin 1. The geometric axis of rotation of the unit 4 is coaxial with the outlet 8 which communicates with the casing 3 cavity connected with the throat zone 13 of the furnace 2. The unit 4 (Fig.2) comprises a horizontal member 14 in the form of a hub 15 which serves to divide the burden axial flow into radial flows and has an opening 15a for mounting on a shaft (not shown). The hub is defined by a polyhedron having, for instance, five uniformly circumferentially disposed guiding members 16 around its periphery. Each of the members 16 is comprised of a first and second segments 17 and 18, respectively, which are disposed sequentially in the burden flow direction. The first segment 17 of each of the guiding members 16 serves to change the radial burden flow to the circumferential one, while the second segment 18 deflects the circumferential direction, depending on the rotational speed and direction of the unit 4. Rigidity of the unit 4 is increased by stiffening ribs 19, 20, for instance, in the trapezium form. In order to reduce the weight of the unit 4, the hub 15 is provided with blind holes 21. The first segment 17 of the guiding member 16 is made in the form of a trough with walls 22, while the second segment 18 is defined, for instance, by three plane faces 25, 25a and 25b and has a burden shoot edge 24. The trough bottom of the first segment 17 is 20 to 60 mm deeper than the plane faces 25, 25a, 25b of the second segment 18, i.e. a step is formed in the connection region between the first segment 17 and the second segment 18. A height of the trough walls 22 decreases with the burden flow, making up 1/2 the segment width at beginning of the first segment 17 and 1/5 the segment width at the end 9 thereof. Each guiding member 16, being a part of the unit 4, makes an angle with a horizontal plane so that its burden shoot edge 24 faces the throat zone 13 of the furnace 2 (Fig.1), and the vectors of circumferential velocity components of the burden motion over all guiding members 16 have the same direction. Inclination angles "a" of the plane faces 25, 25a and 26b of the second segment 18 increase with the burden flow so as to meet inequality 25 vertical plane passing through geometric centre O25 of this plane face and tangentially to the circle lying in the horizontal plane and having the centre on axis A-A of the furnace 2 and the radius equal to the distance from the furnace axis to geometric centre O25 is inclined at angle " 25" to the horizontal plane. First line m25 of intersection of the plane face 25a with a first vertical plane passing through its geometric centre O25 and tangentially to the circle lying in the horizontal plane and having the centre on axis A-A of the furnace 2 and the radius equal to the distance of the furnace axis to geometric centre O25a is inclined at angle 25 to the horizontal plane, with 25a > 25 The plane face 25b is made in a similar manner, in particular, its first line m25b of intersection with a first vertical plane passing through its geometric centre O25b and tangentially to the circle lying in a horizontal plane and having the centre on axis A-A of the furnace 2 and the radius equal to the distance from the furnace axis to geometric centre O25b is inclined at angle 25b to the horizontal plane, with 25b > 25a Consequently, the first lines of intersection of all plane faces 25, 25a and 25b form a polygonal line (Fig.4), each subsequent length of which has a greater inclination angle than 10 the preceding one, i.e. the inclination angles increase with the burden flow so as to meet inequality 25 The limit of the variation in the inclination angle of the plane faces 25, 25a and 25b is defined experimentally. The plane faces 25, 25a and 25b are also inclined to axis A-A of the furnace 2, making angles "p" with a horizontal plane. For this purpose the plane face 25 of the second segment 18 is made so that its second line n25 (Fig.5) of intersection with a second vertical plane passing through geometric centre O25 and axis A-A of the furnace 2 is inclined at angle p2S to a horizontal plane. Second line n25a of intersection of the plane face 25a with a second vertical plane passing through geometric centre O25a and axis A-A of the furnace 2 is inclined at angle 25a to a horizontal plane, with 25a > 25. The plane face 25b is made in a similar manner, in particular, its second line n25b of intersection with a second vertical plane passing through geometric centre O25b and axis A-A of the furnace 2 is inclined at angle 25b to a horizontal plane, with 25a > 25a-Therefore, each subsequent line of intersection of the plane face, in the burden flow direction, is inclined at greater angle p so as to meet inequality 25 An apparatus for charging a shaft furnace operates in the following manner. The inlet 6 of the bin 1 is closed by a cone-shaped locking member 7 (Fig.1), and the hopper 12 is filled by a burden portion supplied thereto by a conveyor (not shown). Further, a drive (not shown) displaces, via the bar 10, the cone-shaped locking member 7, the latter descends and opens the inlet 6, and the burden is admitted through an annular gap into the bin 1. Here, the burden grain-size composition and weight are distributed over the cross section of the bin 1 by any conventional method, the burden being 11 accumulated since the cone-shaped member 9 closes the outlet 8. Once the hopper 12 has been emptied, the cone-shaped member 7 is displaced by a drive (not shown) via the bar 10 upwards to close the inlet 6. It is a common knowledge that in performing the blast-furnace process at increased gas pressure in the throat zone of the furnace 2, prior to discharging a burden portion from the bin 1 into the furnace 2 the gas pressure is equalized between the cavities of the bin 1 and furnace 2 using any conventional technique. After that a drive (not shown) displaces, via the bar 11, the cone-shaped locking member 9 downwards to form an annular gap through which the burden is admitted into the casing 3 cavity and further to holes 21 in the hub 15. Once the blind holes 21 have been filled with the burden, the latter forms on the surface of the hub 15 a pyramidal surface, the edges of which divide the burden into separate flows which are shot to the troughs of the guiding members 16 along the faces of the burden pyramidal surface. A charge layer is accumulating in each trough until the layer surface is even with the plane face 25. Then, the burden flow direction-on the burden layer surface in the trough changes from radial to circumferential. Generated in the trough is a jet flow of the burden which is actively stirred due to its motion over the burden layer surface, resulting in a blended grain-size distribution of the burden. The premature shooting of the burden from the trough is prevented by the trough side walls having a height of 1/2 the segment width at the beginning of the first segment 17, and 1/5 the segment width at the end thereof. The above relationships have been found experimentally in order to provide an optimum cross section of the charge flow formed. From every trough of the first segment 17, the burden flow passes to the second segment 18 of the guiding member 16, where, with the unit 4 rotating in the direction shown by arrow "a" (Fig. 1), the burden flows change their direction under the action of the resultant of frictional, 12 centrifugal and Coriolis forces. When the direction of the unit 4 rotation is the same as the direction of the burden flow over the guiding member 16 and the rotational speed of the unit 4 is, for example, 2 r.p.m., the burden moves along the dotted path (Fig.6), providing the charging of the middle portion of the throat zone 13. As the rotational speed of the unit 4 increases to 9,5 r.p.m., the burden flow changes its initial direction, and the burden drop path, shown by the dash-dot jine, displaces from the furnace middle region to its periphery. At a maximum rotational speed of the unit 4, for example, 17 r.p.m., the throat zone is charged at its periphery, in particular, the burden is laid immediately against the furnace 2 wall, as shown by the solid line in Fig.6. The axial region of the furnace 2 is charged when the unit 4 increases the speed and reverses the direction of rotation, as shown by arrow "b" (Fig.1). When the rotational speed of the unit 4 reaches, for instance, 5 r.p.m., the burden is charged directly to the furnace centre, as shown by the solid line in Fig.7. Thus, a required contour of the burden charged into the throat zone 13 of the furnace 2 is provided by changing-the rotation direction and speed of the unit 4, ensuring a minimum nonuniformity in the circumferential grain-size and weight distribution of the burden in the furnace 2. To compensate disturbances in the blast-furnace process, caused by a circumferentially asymmetric gas flow distribution in the furnace 2, the nonuniformity of the burden grain-size and weight distribution in the annular flow received at the unit 4 is increased in agreement with the gas flow asymmetry by any conventional method . When the unit 4 rotates in the direction of arrow "a" (Fig. 1) which is coincident with the burden flow over the guiding member 16, at the rotational speed of the unit 4 close to a minimum one, as the burden travels, from the surface 25 to the surface 25a, and from the surface 25a to the surface 25b (provided inequality 25 13 burden and the surfaces 25, 25a, 25b decreases, with the velocity of the burden descent from the final surface 25b being increased. The foregoing results in changing the initial conditions of the burden free fall from the guiding member 16, under which the burden flight range reduces, providing the charging of the furnace middle region which is located closer to its axis. Furthermore, the axial region of the furnace is charged at the rotational speed less than a maximum one. To enhance the efficiency of forming a required stockline contour of the charge closer to the central region of the furnace, components of the plane faces 25, 25a and 25b of the second segment 18 are further inclined to axis A-A of the furnace 2. If the inclination angle of line n25 of intersection of the plane face 25 with a second vertical plane is less than p2s, only the peripheral region 13 of the furnace 2 is charged due to the considerably increased action of the centrifugal force on the burden, which inhibits the burden from charging the axial region. With the inclination angle of line n25 of intersection of the plane face 25b with a second vertical plane being greater than 25b, only the axial region of the furnace 2 is charged due to an increase in the gravity component acting on the burden and directed along the slope line of the second portion 18 to the furnace axial region, as compared to the resultant of centrifugal, frictional and Coriolis forces. The mechanism of the effect of the plane face inclinations to the furnace axis is as follows: When the burden distributing unit 4 rotates in the direction of arrow "a" which is coincident with the direction of the burden motion over the guiding member 16, and the rotational speed of the unit 4 is close to a minimum one, as the burden travels from the surface 25 to the surface 25a and further from the surface 25a to the surface 25b, the frictional force between the burden and the surfaces 25, 25a and 25b 14 decreases, provided inequality 25 An apparatus for charging a shaft furnace in accordance with the invention, when installed at a blast furnace with a working volume of, for example, 2000 cu m, provides a high-quality circumferential distribution of every burden portion over the entire surface of the throat zone in a short time, such as 20, ... 30 s, thereby increasing furnace output up to 20% and enhancing the cost efficiency due the coke consumption reduced by 15%. 15 WE CLAIM: 1. An improved apparatus for charging a shaft section of a furnace (2) in particular blast furnaces comprising a bin for a burden, having an inlet (6) and an outlet (8), the bin (1) being connected to a unit (4) for distributing the burden over a cross section of the furnace (2), the unit (4) being adapted & be disposed in a threat zone (13) and rotate about an axis of said furnace (2) beneath the bin outlet (6) along a flow of the burden, characterized in that the unit comprising a horizontal member (14) having at least two guiding members uniformly ctrcumferentially disposed around its periphery, each of the guiding members (16) being connected with the horizontal member (14) and having two segments (17,18) which are configured sequentially In a biffden flow direction, a first (17) of the segments being located in the immediate vicinity of the horizontal member (14), while a second (18) segment is defined by at least two plane faces (25,25a, 25b) whereinanJntersection line (rns) formed when intersecting each plane face (25,25a25b) Mth a first vertical plane passing through ofihe plane face and tangentially to a circle lying in a horizontal plane and having the center on the axis (A-A) of said furnace (2) and the radius equal to the distance from the axis (A-A) of said furnace to the geometric center (02s), is inclined at angle tta* to the horizontal plane, the intersection lines (m^^^,. m^) of all plane faces (25,25a, 25b) forming a polygonal line, each successive length of which, in the burden flow direction, makes greater inclination angle a with the harizontai plane than the preceding one (o35 16 formed when intersecting each plane face (25) with a second vertical plane passing through the geometric center (0s) of the plane face and the axis (A-A) of the furnace (2), is inclined at angle "JJ^to the horizontal plane, with angle increasing with the burden flow 25a ajburden shoot edge (24) of the second segment (18) facing the throat zone (13) of said furnace (2). 2. The apparatus as claimed in claim 1, wherein said first segment (17) of each guiding member (14) comprises a trough with side walls (22) having a height decreasing with the burden flow; the height of the walls being equal to Vt the width of the segment at the beginning and 1/5 the width of the segment at the end thereof. 3. The apparatus as claimed in claim 2, wherein a bottom of the trough of the first segment is deeper than the plane faces (25,25a, 25b) of the second segment (18) by an amount equal to one-half the average size of particles of the burden charged. 4. An improved apparatus for charging a shaft section of a furnace in * particular blast furnaces substantially as described in the description and shown in drawings of Fig. I to 7. This invention relates to an apparatus for charging a shaft furnace, in which each of plane faces of a second segment of a guiding member of a unit for distributing a burden over a cross section of the furnace is formed so that its first line of intersection with the first vertical plane passing through its geometric center and tangentially to a circle lying in a horizontal plane and having the center on the axis of the furnace and the radius equal to the distance from the furnace axis to the geometric center, the inclined angle " " to the horizontal plane, the intersection line© of all plane faces forming a polygonal line, exact subsequent length of the polygonal line, in a burden flow direction, making a greater angle of inclination with the horizontal plane than the preceding one, and a second line of intersection of each plane face with a second vertical plane passing through its geomettic center and the furnace axis is inclined at angle "beta" to the horizontal plane. With angle "beta" increasing with the burden flow.

Full Text

1A

The present invention relates to ferrous metallurgy, and more particularly, to an apparatus for charging a shaft furnace.
The invention may be most successfully used in blast furnaces.
As of now, in the quest to intensify the iron-making process the efforts are directed to improving the blast-furnace process through optimum distribution of a gas flow over the blast furnace shaft section, which determines the quality of iron produced, the specific fuel consumption for its production and the blast furnace output as a whole. The uniform distribution of the gas flow over the furnace section is attained by controlling the rate of blowing and changing the layer contours of ore and coke components of the burden which is fed into a throat zone by a charging device installed on the furnace cone. Therefore, the requirements that are placed upon the charging device are to provide a desired contour of the burden layer over the furnace cross section with minimum nonuniformity in the circumferential grain-size distribution of the burden in the throat zone, and, essentially, a controlled thickness of the burden layer charged.
Conventional blast furnace charging apparatuses include a double-cone charging apparatus equipped with movable throat plates, which is disclosed in DE A 2125062.
The above apparatus for charging a shaft furnace comprises a bin having an inlet and an outlet, the bin being connected through flanges with a top portion of the furnace. The bin outlet is located in the furnace chamber, within its throat zone, and closed by a cone-shaped locking member. The locking member is adapted to move vertically. The furnace throat zone is provided with movable plates which carry distributing plates with a reflecting surface facing the bin outlet. The plates are uniformly circumferentially

2 disposed and adapted to radially move along the guides which are rigidly
fixed to the furnace shell.
In operation of the apparatus, the locking member is displaced towards the furnace chamber, and a burden is admitted through an annular gap formed to the peripheral region of the throat zone. If the blast-furnace process is disturbed, it is required to change the contour of the charged burden layer. To this end, the plates are radially displaced towards the furnace axis until they reach a position in which the path of the falling burden intersects the surface of the distributing plates, which results in altering the burden flow direction so that the burden moves towards the furnace axis. The above prior art apparatus, however, changes the contour of the burden layer charged only in the peripheral annular region due to the restricted displacement of the movable plate, which reduces the potentials of the apparatus, limiting the burden laying control only to 1/3 the furnace radius.
Most closely approaching the present invention by the combination of technical features and the achieved result is an apparatus for charging a shaft furnace, comprising a bin for a burden having an inlet and an outlet, a unit for distributing the burden over a cross section of the furnace, said unit being mounted in a throat zone beneath the bin outlet and adapted to rotate about the furnace axis. The burden distributing unit comprises a horizontal member having at least two guiding members disposed around its periphery, each of the guiding members being connected with the horizontal member and consisting of two segments which are arranged sequentially in the direction of the burden flow. A first segment is located in the immediate vicinity to the horizontal member, and a second segment is defined by at least two plane faces and has a burden shoot edge facing the furnace throat zone (WO Application No. 92/19776, C21B 7/20).

3 Owing to the design of the distributing unit, the burden body leaving
the bin outlet is divided into at least two flows which form a charge layer in the throat zone with approximately even circumferential grain-size distribution. This is attained due to laying the burden pellets of the same size symmetrically about the furnace axis, thereby significantly reducing the nonuniformity of the circumferential burden weight distribution in the furnace. The uniform arrangement of the guiding members around the periphery with the first segment being disposed in the immediate vicinity to the horizontal member, makes it possible to change the radial direction of the burden flow to the circumferential one. On the guiding member second segments, the circumferential direction of the burden flow changes to a tangential one, or towards the furnace axis, under the effect of the resultant of frictional, centrifugal and Coriolis forces. This enables the burden to be charged to any throat region and provides the possibility to form a required stockline contour in the throat zone. This is attained by a single type of motion, in particular, by rotation of the burden distributing unit about the furnace axis. The above structural features of the charging unit provide the improvement in the blast-furnace process parameters and the reduction in energy losses. The rotary drive of the unit has a simpler structure.
In operation, a burden portion is charged from the burden bin on the horizontal member of the burden distributing unit and further along the guiding members into the furnace chamber. A burden layer is formed in the furnace throat zone by virtue of rotation of the burden distributing unit. Owing to the possibility to change the rotational speed of said unit, the apparatus provides a desired stockline contour in the shaft furnace. This improves the blast-furnace process characteristics. However, a required stockline contour is not provided when laying the burden by the above apparatus in the region adjacent to the furnace axis, since the non-optimal

4 spatial orientation of the plane faces of the guiding member second segment
hinders the admission of a sufficient amount of material to the furnace axial region. As a consequence, the optimum gas distribution over the furnace cross section is not provided, resulting in the increased coke consumption and some reduction in the output. In addition, in the prior art apparatus the position of plane faces of the guiding members fails to be unambiguously defined which makes the manufacture of the apparatus as such problematic, and further hampers the attainment of a desired stockline contour in the furnace throat zone.
Summary of the Invention
It is an object of the present invention to provide an apparatus for charging a shaft furnace, having a unit for distributing a burden over the furnace cross section, designed so that to provide a required stockline contour in the furnace throat zone with a highly uniform circumferential grain-size and weight distribution of the burden.
The foregoing and other objects of the present invention are achieved in an apparatus for charging a shaft furnace, comprising a bin for a burden, having an inlet and an outlet, said bin being connected with a unit for distributing the burden over the furnace cross section, said unit being adapted to be mounted in the throat zone and rotate about the furnace axis beneath the bin outlet along a burden flow which is formed by a horizontal member having at least two uniformly circumferentially disposed guiding members, each of the guiding members being connected to the horizontal member and including two segments which are arranged sequentially in the burden flow direction, a first of the segments being disposed in the immediate vicinity to the horizontal member, while a second segment is defined by at least two plane faces and has a burden shoot edge which faces the furnace throat zone, wherein in accordance with the invention each

5 of the plane faces of the second segment is formed so that its first line of
intersection with a first vertical plane passing through its geometric centre and tangentially to a circle lying in a horizontal plane and having the centre on the furnace axis and the radius equal to the distance from the furnace axis to the geometric centre is inclined at angle "a" to the horizontal plane, the intersection lines of all plane faces (25, 25a, 25b) forming a polygonal line, each sequential length of which in the burden flow direction has greater inclination angle "a" than the preceding one, and a second line of intersection of each plane face with a second vertical plane passing through its geometric centre and the furnace axis is inclined at angle "p" to a horizontal plane, with angle "p" increasing with the burden flow.
The increase in inclination angle "a" of the plane faces in the burden flow direction provides the reduction in bonding forces between each subsequent plane face and the burden flow, promoting the burden descent from the guiding members. As a consequence, the material falls closer to the furnace axial region at a minimum rotational speed of the unit, providing the charging of the middle region of the throat zone.
The design of the guiding member, with plane faces of the second segment simultaneously changing angles "p" of inclination to the furnace axis, changes the burden flow direction towards the furnace axis at low rotational speeds of the unit, providing the charging of the throat zone centre.
The above design of the burden distributing unit allows the attainment of a required stockline contour by changing the rotational speed of the unit. This enables the peripheral region of the throat zone to be charged at a maximum rotational speed, the axial region to be charged at a minimum rotational speed and the middle region to be charged at intermediate values of the unit rotational speed. With the rotational speed of the distributing unit

6
being unchanged, the burden will be laid in the throat zone in the form of an annular ridge with a distinct apex. When the rotational speed of the distributing unit changes during the discharge from high to low, the burden is laid in the throat zone in a spiral, so that a layer with a smoothened surface is formed.
Preferably the first segment of each guiding member comprises a trough with side wails having a height which is equal to 1/2 the segment width at the beginning of the segment and 1/5 the segment width at the end thereof.
The trough-like configuration of the first segment results in forming a burden flow entering the second segment as a directed jet, which ensures the provision of a required weight ratio of coke and ore components in the vertical stock column over the entire furnace volume
Preferably a bottom of the first segment trough at the connection with the surface of the second segment is deeper than the latter. This deepening amounts to 20 to 60mm which is about one-half an average diameter of burden particles charged into the shaft surface. Consequently, the lower plane of the guiding member trough portion will be lined with small charge fractions and have an optimally rough surface on which the burden flow will be formed.
Owing to such configuration of the first segment, the trough bottom surface is afforded the protection against abrasive wear due to forming a burden layer on the first segment surface, which extends the life of the burden distributing unit. Moreover, the burden flow motion over the burden layer formed on the first segment of the guiding member results in a blended grain-size distribution of the burden charged into the throat zone of the furnace. With the unit being rotated, the above circumstance ensures that

7
the burden layer formed in the above region has a minimum nonuniformity in the circumferential burden grain-size distribution in the furnace throat zone.
These and other objects and advantages of the invention will be best appreciated from the following detailed description of a preferred embodiment, taken in conjunction with the accompanying drawings in which:
Fig. 1 is a schematic perspective view of an apparatus for charging a shaft furnace, with a partial cutout;
Fig.2 is an enlarged perspective view of a unit for distributing burden over the furnace cross section, in accordance with the present invention;
Fig.3 is a perspective view of a guiding member;
Fig.4 is a view developed through section IV-IV of Fig.3 formed by first vertical planes;
Fig.5 is a view developed through section V-V of Fig.3 formed by second vertical planes;
, Fig.6 is a stockline contour in the furnace throat zone at a forward rotation direction of the charging unit;
Fig.7 is a stockline contour in the furnace throat zone at a reverse rotation direction of the charging unit.
An apparatus for charging a shaft furnace, such as a blast furnace, in accordance with the invention includes a burden bin 1 (Fig.1) connected with the furnace 2 via a casing 3 which is coaxial with the bin 1 and the furnace 2. The casing 3 accommodates a rotary drive of a unit 4 for distributing burden over the cross section of the furnace 2 and has a ring 5 for connection with the latter. The bin 1 has a burden inlet 6 closed by a cone-shaped locking member 7 and an outlet 8 closed by a cone-shaped locking member 9. The inlet 6 and the outlet 8 are concentric with the axis of symmetry of the bin 1. The cone-shaped locking members 7 and 9 are connected to vertical displacement drives (not shown in Fig.1) via bars 10

8 and 11, respectively. Burden is charged into the bin 1 through a hopper 12
which is mounted on the bin 1 and serves to accumulate a burden portion which is loaded, for instance, by a conveyor (not shown in Fig. 1). The unit 4 is connected with the top portion of the furnace 2 and disposed in its chamber in a throat zone 13 beneath the outlet 8 of the bin 1. The geometric axis of rotation of the unit 4 is coaxial with the outlet 8 which communicates with the casing 3 cavity connected with the throat zone 13 of the furnace 2. The unit 4 (Fig.2) comprises a horizontal member 14 in the form of a hub 15 which serves to divide the burden axial flow into radial flows and has an opening 15a for mounting on a shaft (not shown). The hub is defined by a polyhedron having, for instance, five uniformly circumferentially disposed guiding members 16 around its periphery. Each of the members 16 is comprised of a first and second segments 17 and 18, respectively, which are disposed sequentially in the burden flow direction. The first segment 17 of each of the guiding members 16 serves to change the radial burden flow to the circumferential one, while the second segment 18 deflects the circumferential direction, depending on the rotational speed and direction of the unit 4. Rigidity of the unit 4 is increased by stiffening ribs 19, 20, for instance, in the trapezium form. In order to reduce the weight of the unit 4, the hub 15 is provided with blind holes 21. The first segment 17 of the guiding member 16 is made in the form of a trough with walls 22, while the second segment 18 is defined, for instance, by three plane faces 25, 25a and 25b and has a burden shoot edge 24. The trough bottom of the first segment 17 is 20 to 60 mm deeper than the plane faces 25, 25a, 25b of the second segment 18, i.e. a step is formed in the connection region between the first segment 17 and the second segment 18. A height of the trough walls 22 decreases with the burden flow, making up 1/2 the segment width at beginning of the first segment 17 and 1/5 the segment width at the end

9
thereof. Each guiding member 16, being a part of the unit 4, makes an angle with a horizontal plane so that its burden shoot edge 24 faces the throat zone 13 of the furnace 2 (Fig.1), and the vectors of circumferential velocity components of the burden motion over all guiding members 16 have the same direction. Inclination angles "a" of the plane faces 25, 25a and 26b of the second segment 18 increase with the burden flow so as to meet inequality 25 vertical plane passing through geometric centre O25 of this plane face and tangentially to the circle lying in the horizontal plane and having the centre on axis A-A of the furnace 2 and the radius equal to the distance from the furnace axis to geometric centre O25 is inclined at angle " 25" to the horizontal plane. First line m25 of intersection of the plane face 25a with a
first vertical plane passing through its geometric centre O25 and tangentially to the circle lying in the horizontal plane and having the centre on axis A-A of the furnace 2 and the radius equal to the distance of the furnace axis to geometric centre O25a is inclined at angle 25 to the horizontal plane, with
25a > 25
The plane face 25b is made in a similar manner, in particular, its first line m25b of intersection with a first vertical plane passing through its
geometric centre O25b and tangentially to the circle lying in a horizontal plane and having the centre on axis A-A of the furnace 2 and the radius equal to the distance from the furnace axis to geometric centre O25b is inclined at angle 25b to the horizontal plane, with 25b > 25a Consequently, the first lines of intersection of all plane faces 25, 25a and 25b form a polygonal line (Fig.4), each subsequent length of which has a greater inclination angle than

10 the preceding one, i.e. the inclination angles increase with the burden flow
so as to meet inequality 25 The limit of the variation in the inclination angle of the plane faces 25, 25a and 25b is defined experimentally. The plane faces 25, 25a and 25b are also inclined to axis A-A of the furnace 2, making angles "p" with a horizontal plane. For this purpose the plane face 25 of the second segment 18 is made so that its second line n25 (Fig.5) of intersection with a second vertical plane passing through geometric centre O25 and axis A-A of the furnace 2 is inclined at angle p2S to a horizontal plane. Second line n25a of
intersection of the plane face 25a with a second vertical plane passing through geometric centre O25a and axis A-A of the furnace 2 is inclined at angle 25a to a horizontal plane, with 25a > 25. The plane face 25b is made in a similar manner, in particular, its second line n25b of intersection with a second vertical plane passing through geometric centre O25b and axis A-A of the furnace 2 is inclined at angle 25b to a horizontal plane, with 25a > 25a-Therefore, each subsequent line of intersection of the plane face, in the burden flow direction, is inclined at greater angle p so as to meet inequality 25 An apparatus for charging a shaft furnace operates in the following manner. The inlet 6 of the bin 1 is closed by a cone-shaped locking member 7 (Fig.1), and the hopper 12 is filled by a burden portion supplied thereto by a conveyor (not shown). Further, a drive (not shown) displaces, via the bar 10, the cone-shaped locking member 7, the latter descends and opens the inlet 6, and the burden is admitted through an annular gap into the bin 1. Here, the burden grain-size composition and weight are distributed over the cross section of the bin 1 by any conventional method, the burden being

11 accumulated since the cone-shaped member 9 closes the outlet 8. Once the
hopper 12 has been emptied, the cone-shaped member 7 is displaced by a drive (not shown) via the bar 10 upwards to close the inlet 6. It is a common knowledge that in performing the blast-furnace process at increased gas pressure in the throat zone of the furnace 2, prior to discharging a burden portion from the bin 1 into the furnace 2 the gas pressure is equalized between the cavities of the bin 1 and furnace 2 using any conventional technique. After that a drive (not shown) displaces, via the bar 11, the cone-shaped locking member 9 downwards to form an annular gap through which the burden is admitted into the casing 3 cavity and further to holes 21 in the hub 15. Once the blind holes 21 have been filled with the burden, the latter forms on the surface of the hub 15 a pyramidal surface, the edges of which divide the burden into separate flows which are shot to the troughs of the guiding members 16 along the faces of the burden pyramidal surface. A charge layer is accumulating in each trough until the layer surface is even with the plane face 25. Then, the burden flow direction-on the burden layer surface in the trough changes from radial to circumferential. Generated in the trough is a jet flow of the burden which is actively stirred due to its motion over the burden layer surface, resulting in a blended grain-size distribution of the burden. The premature shooting of the burden from the trough is prevented by the trough side walls having a height of 1/2 the segment width at the beginning of the first segment 17, and 1/5 the segment width at the end thereof. The above relationships have been found experimentally in order to provide an optimum cross section of the charge flow formed. From every trough of the first segment 17, the burden flow passes to the second segment 18 of the guiding member 16, where, with the unit 4 rotating in the direction shown by arrow "a" (Fig. 1), the burden flows change their direction under the action of the resultant of frictional,

12
centrifugal and Coriolis forces. When the direction of the unit 4 rotation is the same as the direction of the burden flow over the guiding member 16 and the rotational speed of the unit 4 is, for example, 2 r.p.m., the burden moves along the dotted path (Fig.6), providing the charging of the middle portion of the throat zone 13. As the rotational speed of the unit 4 increases to 9,5 r.p.m., the burden flow changes its initial direction, and the burden drop path, shown by the dash-dot jine, displaces from the furnace middle region to its periphery. At a maximum rotational speed of the unit 4, for example, 17 r.p.m., the throat zone is charged at its periphery, in particular, the burden is laid immediately against the furnace 2 wall, as shown by the solid line in Fig.6. The axial region of the furnace 2 is charged when the unit 4 increases the speed and reverses the direction of rotation, as shown by arrow "b" (Fig.1). When the rotational speed of the unit 4 reaches, for instance, 5 r.p.m., the burden is charged directly to the furnace centre, as shown by the solid line in Fig.7. Thus, a required contour of the burden charged into the throat zone 13 of the furnace 2 is provided by changing-the rotation direction and speed of the unit 4, ensuring a minimum nonuniformity in the circumferential grain-size and weight distribution of the burden in the furnace 2. To compensate disturbances in the blast-furnace process, caused by a circumferentially asymmetric gas flow distribution in the furnace 2, the nonuniformity of the burden grain-size and weight distribution in the annular flow received at the unit 4 is increased in agreement with the gas flow asymmetry by any conventional method .
When the unit 4 rotates in the direction of arrow "a" (Fig. 1) which is coincident with the burden flow over the guiding member 16, at the rotational speed of the unit 4 close to a minimum one, as the burden travels, from the surface 25 to the surface 25a, and from the surface 25a to the surface 25b (provided inequality 25
13 burden and the surfaces 25, 25a, 25b decreases, with the velocity of the
burden descent from the final surface 25b being increased. The foregoing results in changing the initial conditions of the burden free fall from the guiding member 16, under which the burden flight range reduces, providing the charging of the furnace middle region which is located closer to its axis. Furthermore, the axial region of the furnace is charged at the rotational speed less than a maximum one.
To enhance the efficiency of forming a required stockline contour of the charge closer to the central region of the furnace, components of the plane faces 25, 25a and 25b of the second segment 18 are further inclined
to axis A-A of the furnace 2. If the inclination angle of line n25 of intersection
of the plane face 25 with a second vertical plane is less than p2s, only the peripheral region 13 of the furnace 2 is charged due to the considerably increased action of the centrifugal force on the burden, which inhibits the
burden from charging the axial region. With the inclination angle of line n25
of intersection of the plane face 25b with a second vertical plane being greater than 25b, only the axial region of the furnace 2 is charged due to an increase in the gravity component acting on the burden and directed along the slope line of the second portion 18 to the furnace axial region, as compared to the resultant of centrifugal, frictional and Coriolis forces.
The mechanism of the effect of the plane face inclinations to the furnace axis is as follows: When the burden distributing unit 4 rotates in the direction of arrow "a" which is coincident with the direction of the burden motion over the guiding member 16, and the rotational speed of the unit 4 is close to a minimum one, as the burden travels from the surface 25 to the surface 25a and further from the surface 25a to the surface 25b, the frictional force between the burden and the surfaces 25, 25a and 25b

14
decreases, provided inequality 25 An apparatus for charging a shaft furnace in accordance with the invention, when installed at a blast furnace with a working volume of, for example, 2000 cu m, provides a high-quality circumferential distribution of every burden portion over the entire surface of the throat zone in a short time, such as 20, ... 30 s, thereby increasing furnace output up to 20% and enhancing the cost efficiency due the coke consumption reduced by 15%.

15 WE CLAIM:
1. An improved apparatus for charging a shaft section of a furnace (2) in
particular blast furnaces comprising a bin for a burden, having an inlet (6) and an outlet (8), the bin (1) being connected to a unit (4) for distributing the burden over a cross section of the furnace (2), the unit (4) being adapted & be disposed in a threat zone (13) and rotate about an axis of said furnace (2) beneath the bin outlet (6) along a flow of the burden, characterized in that the unit comprising a horizontal member (14) having at least two guiding members uniformly ctrcumferentially disposed around its periphery, each of the guiding members (16) being connected with the horizontal member (14) and having two segments (17,18) which are configured sequentially In a biffden flow direction, a first (17) of the segments being located in the immediate vicinity of the horizontal member (14), while a second (18) segment is defined by at least two plane faces (25,25a, 25b) whereinanJntersection line (rns) formed when intersecting each plane face (25,25a25b) Mth a first vertical plane passing through ofihe plane face and tangentially to a circle lying in a horizontal plane and having the center on the axis (A-A) of said furnace (2) and the radius equal to the distance from the axis (A-A) of said furnace to the geometric center (02s), is inclined at angle tta* to the horizontal plane, the intersection lines (m^^^,. m^) of all plane faces (25,25a, 25b) forming a polygonal line, each successive length of which, in the burden flow direction, makes greater inclination angle *a* with the harizontai plane
than the preceding one (o35
16
formed when intersecting each plane face (25) with a second vertical plane passing through the geometric center (0s) of the plane face and the axis (A-A) of the furnace (2), is inclined at angle "JJ^to the horizontal plane, with angle increasing with the burden flow 25a ajburden shoot edge (24) of the second
segment (18) facing the throat zone (13) of said furnace (2).
2. The apparatus as claimed in claim 1, wherein said first segment (17) of
each guiding member (14) comprises a trough with side walls (22) having a
height decreasing with the burden flow; the height of the walls being equal
to Vt the width of the segment at the beginning and 1/5 the width of the
segment at the end thereof.
3. The apparatus as claimed in claim 2, wherein a bottom of the trough of the
first segment is deeper than the plane faces (25,25a, 25b) of the second
segment (18) by an amount equal to one-half the average size of particles
of the burden charged.
4. An improved apparatus for charging a shaft section of a furnace in
* particular blast furnaces substantially as described in the description and shown in drawings of Fig. I to 7.

This invention relates to an apparatus for charging a shaft furnace, in which each of plane faces of a second segment of a guiding member of a unit for distributing a burden over a cross section of the furnace is formed so that its first line of intersection with the first vertical plane passing through its geometric center and tangentially to a circle lying in a horizontal plane and having the center on the axis of the furnace and the radius equal to the distance from the furnace axis to the geometric center, the inclined angle " " to the horizontal plane, the intersection line© of all plane faces forming a polygonal line, exact subsequent length of the polygonal line, in a burden flow direction, making a greater angle of inclination with the horizontal plane than the preceding one, and a second line of intersection of each plane face with a second vertical plane passing through its geomettic center and the furnace axis is inclined at angle "beta" to the horizontal plane. With angle "beta" increasing with the burden flow.

Documents:

00234-cal-1999-abstract.pdf

00234-cal-1999-claims.pdf

00234-cal-1999-correspondence.pdf

00234-cal-1999-description(complete).pdf

00234-cal-1999-drawings.pdf

00234-cal-1999-form-1.pdf

00234-cal-1999-form-2.pdf

00234-cal-1999-form-3.pdf

00234-cal-1999-letters patent.pdf

00234-cal-1999-p.a.pdf

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Patent Number

207090

Indian Patent Application Number

234/CAL/1999

PG Journal Number

21/2007

Publication Date

25-May-2007

Grant Date

23-May-2007

Date of Filing

18-Mar-1999

Name of Patentee

ZAKRYTOE AKTSIONERNOE OBSCHESTVO"NAUCHNO-PROIZVODSTVENNY I KOMMERCHESKY TSENTR"TOTEM"

Applicant Address

RUSSIAN FEDERATION, MOSCOW, 3 MYTISCHINSKAYA ULITSA, D. 16, KORPUS 60

Inventors:

#	Inventor's Name	Inventor's Address
1	ABRAMIN GERMAN VASILIEVICH	RUSSIAN FEDERATION, NOVOKUZNETSK, ULITSA KLIMENKO, D. 29/3, KV.17
2	KOSHELNIKOV ANDREI VASILIEVICH	RUSSIAN FEDERATION, NOVOKUZNETSK, ULITSA AVIATOROV,D.91,KV 100

PCT International Classification Number

C 21B - 7/08

PCT International Application Number

N/A

PCT International Filing date

PCT Conventions:

#	PCT Application Number	Date of Convention	Priority Country
1	98105182	1998-03-20	Russia