Method and weaving machine for manufacturing in-plane multiaxial thick woven fabrics

Abstract: This invention describes a method of manufacturing in-plane multiaxial thick woven fabrics using a weaving machine comprising healds through which warps are passed, a shuttle reciprocating so as to insert wefts in a warp shedding portion formed by said heald, a reed, and a woven fabric removing device. The method comprises the steps of providing a large number of healds in parallel in the direction of woven fabric removal; forming a shedding portion by passing warps of the number such that predetermined thickness and width of woven fabric are formed through the healds and by widely reciprocating the healds in the width direction; moving the shedding position sequentially from one side to the other side; inserting a weft sequentially in the shedding portion and arranging it by shifting the weft position in the width direction; forming a texture of the first row of predetermined width and thickness by fixing warps; and manufacturing in-plane multiaxial thick woven fabric of a continuous length by performing shedding, weft insertion, and beating sequentially, wherein when the shedding position shifts from the travel passage of the shuttle, the woven fabric removing device is moved vertically by an up-and-down motion rack so as to agree with the travel passage of the shuttle.

Description: 2. FIELD OF THE INVENTION AND RELATED ART STATEMENT The present invention relates to a weaving method and a weaving machine for in-plane multiaxial thick woven fabrics which are effectively used for interior and exterior materials of aircraft and the like. Conventionally, glass fiber woven fabrics which are impregnated with thermosetting resin, reinforced resin parts which are formed by laminating carbon fiber woven fabrics in multiple layers and by heating and curing, and composite material parts have been used for interior and exterior materials of aircraft and in other various industrial fields because they are light in weight and have high mechanical strength. In the case where this material is used for the external surface of aircraft shell or the like, there is a problem in that separation occurs when a stone or the like strikes the external surface when the aircraft runs on the ground. To solve this problem, a three-dimensional woven fabric for reinforcing a structure, in which layers of woven fabric are integrally connected by using knotting thread, has been disclosed in Japanese Patent Publication No.13060/1990. The three-dimensional woven fabric disclosed in Japanese Patent Publication No.13060/1990 will be described with reference to Figs.17 and 18. In these figures, reference numerals 50, 50a to 50c denote warps, 51, 51a to 51d denote wefts, and 52a and 52b denote knotting threads. This three-dimensional woven fabric is woven with a weaving machine. As shown in Fig.17, wefts 51a to 51d are laminated in parallel, warps 50a to 50c are laminated in perpendicular to the wefts, and knotting threads 52a and 52b fix internal warps 50a to 50c and wefts 51b and 51c by turning at the outside wefts 51a and 51d. As described above, conventional composite material parts in which woven fabric impregnated with thermosetting resin is laminated and heated for formation has a disadvantage that the laminated woven fabric is separated by a shock due to collision from the outside. With the three-dimensional woven fabric shown in Figs.17 and 18, in which laminated warp layer and weft layer are connected by knotting threads 52a and 52b, separation occurring in composite material parts, in which woven fabric impregnated with thermosetting resin is laminated and heated for curing, does not occur. In this woven fabric, however, fibers cannot be arranged in a multiaxial mode in a plane, there being a problem in that fiber arrangement for lightweight and optimized mechanical strength cannot be set. To solve the above problem, Japanese Patent Application No.157513/1988 discloses a method in which triaxial or quadaxial woven fabric with simple structure can be formed by a weft insertion device and a beating-up device by crossing a diagonal warp supplied from a creel for diagonal warp and a diagonal warp of opposite direction alternately in the reverse inclined direction and then by appropriately shedding after transforming to substantially right angles. however, this method can weave only thin in-plane multiaxial woven fabrics. In this case, as described in the prior art, a problem of separation is posed because a laminating operation is required. Also, there is a problem in that the prior art cannot obtain in-plane multiaxial thick woven fabrics. The US-Patent 5.024.874 describes a three dimensional fabric that has a base formed from a multiplicity of woven strings. The strings are arranged and woven to form a fabrik having a multiplicity of warps arranged in a plurality of rows and columns, a plurality of first wefts crossing the warp columns in the interstitial spaces between adjacent warp rows, and a plurality of second wefts crossing said warps and said first wefts in the interstitial spaces between adjacent warp columns. The three dimensional fabric also has a solid linkage mechanism incorporated into the fabric's body by a plurality of the strings that are wound about ist periphery. 3. OBJECT AND SUMMARY OF THE INVENTION The object of the present invention is to provide a weaving method and a weaving apparatus for manufacturing threedimensional woven fabric of arranging warps (supplied from bobbins) multiaxially in the inward direction of a plane of weaving and also arranging wefts (supplied from shuttles in the direction of thickness of weaving) in the direction at right angels to said plane. To achieve the above object, the present invention provides a method of manufacturing in-plane multiaxial thick woven fabrics using a weaving machine comprising healds through which warps are passed, a shuttle reciprocating so as to insert wefts in a warp shedding portion formed by the heald, a reed, and a woven fabric removing device, comprising the steps of providing a large number of healds in parallel in the direction of woven fabric removal; forming a shedding portion by passing warps of the number such that predetermined thickness and width of woven fabric are formed through the healds and by widely reciprocating the healds in the thickness direction; moving the shedding position sequentially from one side to the other side in the woven fabric thickness direction; inserting a weft sequentially in the shedding portion and arranging it by shifting the weft position in the thickness direction; forming a texture of the first row of predetermined width and thickness by fixing warps; and manufacturing an in-plane multiaxial thick woven fabric of a continuous length by performing shedding, weft insertion, and beating sequentially, wherein when the shedding position shifts from the travel passage of the shuttle, the woven fabric removing device is moved vertically so as to agree with the travel passage of the shuttle. Also, the present invention provides a method of manufacturing in-plane multiaxial thick woven fabrics wherein the thickness between selvedges formed by the warp at each end in the direction of the thickness of woven fabric to be manufactured is kept constant, by which the shrinkage of woven fabric in the thickness direction due to the tension of warp is prevented. Further, the present invention provides a weaving machine for manufacturing in-plane multiaxial thick woven fabrics having healds through which warps are passed, a shuttle reciprocating so as to insert wefts in a warp shedding portion formed by said heald, a reed, and a woven fabric removing device, wherein warps of the number such that predetermined thickness and width of woven fabric are formed are passed, and the weaving machine is provided with a reciprocating mechanism for widely reciprocating the heald in the woven fabric thickness direction, a mechanism for reciprocating the woven fabric removing device so as to agree with the travel passage of the shuttle, and a fixing mechanism for fixing the thickness of a selvedge in a constant manner by engaging the selvedge formed by warp at each end in the woven fabric thickness direction. The operation of the present invention is as follows: The warps pulled out from the group of bobbins 2 are allowed to pass through the respective healds and further pass through the reed, and then fixed to the woven fabric removing portion. At this time, an up-and-down motion rack is lowered down to a position where the shed centerline of the heald agrees with the shedding portion of woven fabric. The shedding procedure is performed as shown in Fig.14. In addition to the shedding procedure, the operation sequence of each part is inputted in a computer beforehand. In the operation of the present invention, the operation is basically performed in the order of shedding, weft insertion, beating, winding, and vertical movement. Only when the warp forming a selvedge appears, the operation is performed in the order of shedding, weft insertion, selvedge holding, beating, winding, and vertical movement. The winding amount of woven fabric for each step is set so that the woven fabric is advanced by division in such a manner that a desired pitch in the weft length direction is obtained when the weft advances from the uppermost (lowermost) weft position to the lowermost (uppermost) weft position, or, as necessary, the woven fabric is advanced by a desired pitch in the weft length direction at a time when the weft advances from the uppermost (lowermost) weft position to the lowermost (uppermost) weft position. In this case, the weaving machine is operated in the order of shedding, weft insertion, beating, and vertical movement. Only when the warp forming a selvedge appears, the operation is performed in the order of shedding, weft insertion, selvedge holding, beating, winding (by a pitch in the weft length direction. When the warp forming a selvedge appears two times continuously, the latter need not be wound.), and vertical movement. The amount of vertical movement is allowed to coincide with a desired vertical pitch, or determined empirically on the basis of the desired vertical pitch. According to the present invention described above, in-plane multiaxial thick three-dimensional woven fabrics can be manufactured automatically with high efficiency by using a weaving machine. Since a selvedge formed by a warp loop is formed at each end in the thickness direction, there is no disadvantage that the warp comes off, or frays at each end. Also, since many healds are used and moved for a large thickness, the weft can be arranged at intervals vertically in the first row, thick woven fabrics in which warp is fixed by weft can be manufactured, and three-dimensional woven fabrics in which no cut end of warp and weft is present in the thickness direction can be manufactured. The invention and further features thereof are claimed in claims 1-3. 4. BRIEF DESCRIPTION OF THE DRAWINGS In the drawings, Fig.1 is a perspective view of a weaving machine for manufacturing in-plane multiaxial thick woven fabrics in accordance with an embodiment of the present invention, Fig.2 is an expanded side view of the main portion of Fig.1, Fig.3 is an expanded front view of the main portion of Fig.1, Fig.4 is an expanded perspective view of a rail portion in a selvedge holding mechanism, Fig.5 is a front view of a selvedge holding member mounted on the rail of Fig.4, Fig.6 is a side view of Fig.5, Fig.7 is a perspective view of a selvedge holding mechanism of an embodiment different from that of Fig.5, Fig.8 is a perspective view of a selvedge holding mechanism of an embodiment different from that of Fig.7, Fig.9 is a perspective view of one embodiment of an auxiliary shedding device, Fig.10 is a schematic view illustrating one embodiment of the weaving method of the present invention, Fig.11 is a schematic view showing an operating condition different from that of Fig.10, Fig.12 is a sectional view of a woven fabric manufactured by the method shown in Figs.10 and 11, Fig.13 is a view illustrating the operation sequence of one embodiment of the weaving method of the present invention, Fig.14 is a chart showing the raising and lowering of heald for each step in relation to the warp in the weaving method of the present invention, Fig.15 is a view illustrating a weaving method in the direction of the thickness of woven fabric (1 to 4 stage) in the present invention, Fig.16 is a timing chart in the weaving method of the present invention, Fig.17 is a perspective view of one example of a conventional three-dimensional woven fabric, and Fig.18 is a sectional view of the woven fabric of Fig.17. 5. DETAILED DESCRIPTION OF PREFERRED EMBODIMENT An embodiment of the present invention will be described below with reference to Figs.1 through 15. First, a weaving machine for manufacturing in-plane multiaxial thick woven fabrics in accordance with one embodiment of the present invention will be described with reference to Figs.1 through 9. Many warps 1 are unwound from bobbins 2 and arranged in a flat plane form, and then are allowed to pass through healds 3. The heald 3 is installed in large numbers in parallel in the front and rear direction. Warps 1 of the number such that a predetermined width is formed are allowed to pass through the mail of each heald. Each of the heald moves vertically to form a shed 4, and a weft 6 is allowed to pass through the shed 4 by a shuttle 5. The weft 6 is turned and inserted into the shed 4 of the next warp 1 to form a selvedge at each side in the width direction. The shed 4 of the warp 1 moves vertically in the direction of the thickness of woven fabric, and an up-and-down motion rack 7 vertically moves the woven fabric 8. Therefore, the weft 6 inserted in each shed 4 is also arranged in the thickness direction at a predetermined position in the woven fabric between the warps 1 and fixed. Thus, the thickness dimension of the woven fabric is formed. A reed 9 beats up the weft 6 to the cloth fell after the weft 6 is inserted into the shed 4 by the shuttle 5, thereby the crossing of warp and weft being completed. Reference numeral 10 denotes a woven fabric removing portion which pulls out the woven fabric manufactured by vertical movement by means of the up-and-down motion rack, and 11 denotes a selvedge holding mechanism for fixing a selvedge 8a of warp 1 formed at each end in the thickness direction of the woven fabric 8. This selvedge holding mechanism has a woven fabric holding bar 11b which engages with a hook 11a (Fig.5). The bar 11b hooks the selvedge 8a to prevent the shrinkage of the thickness of woven fabric 8 due to the tension of warp, thereby the thickness of woven fabric being held constant. The hook 11a slides in rails 12, 12, 13, 13 fixed at the upper and lower portions of the selvedge holding mechanism 11 via a roller 14 or the like. When the woven fabric 8 moves from the position of the selvedge holding mechanism 11 toward the woven fabric removing portion 10, the hook 11a comes off from the rails 12 and 13. Afterward, the woven fabric holding bar 11b is removed manually or automatically. The bar 11b is installed to the selvedge of woven fabric 8 manually or automatically. The selvedge holding mechanism 11, unlike the embodiment of Fig.5, may be provided with a wire 16 sequentially wound around a endless wire 15 installed over and under the woven fabric 8 as shown in Fig.7 so that the wire 16 engages with the selvedge 8a of the woven fabric 8 and the wire 15 alternately to keep the thickness of the woven fabric 8 constant. Further, a device shown in Fig.8 may be used, in which a block 18 with a bar which is allowed to pass through the selvedge 8a of woven fabric is inserted into a rail 17 installed over and under the woven fabric 8. An auxiliary shedding device 19 is installed to insert the weft 6 smoothly by increasing the shedding angle because the shedding angle of the warp 1 1 is decreased as the group of healds increases, thereby the warp 1 is rubbed when the shuttle 5 moves. Fig.9 is a detailed view of the auxiliary shedding device 19. The auxiliary shedding device opens by moving into the shed 4 as shown by a solid line, as necessary, from the withdrawal position shown by a two-dot chain line by means of a guide device 20. The reed 9 is installed over the arm 21 of the beating device, and the arm 21 is constructed so as to move back and forth with its lower end being a fulcrum by the action of a beating air cylinder 22 connected at the middle portion to perform beating. The air cylinder 22 is connected to a frame 23. The frame 23 has cylinders 24, 24, 25, 25 for raising/lowering the healds as shown in Fig.3. The rod end of the air cylinder 24, 24 is connected to one end of a bell crank 31, 31, and the other end of the bell crank 31, 31 is connected to a wire 32, 32. The wire 32, 32 is connected to the heald 3 via a grooved wheel 33, 33 and a wire 26, 26 for driving the heald to raise the heald 3. At the other end of the bell crank 31, the rod end of the cylinder 25, 25 for raising/lowering the heald is connected, and the cylinder 25, 25 is also connected to the wire 26, 26 for driving the heald. At one end of the bell crank 31, 31, a wire 34, 34 is connected to a wire 36 for pulling down the heald 3 via a grooved wheel 35, 35. An air cylinder 27 for activating the shuttle has rods 28, 28 extending to the right and the left. The rod 28, 28 is connected to a wire 37, 37. The wire 37, 37 is connected to each end of a rack 38, so that when one of the rods 28, 28 stretches, one wire 37 stretches, thereby the rack 38 being moved in one direction. Therefore, the shuttle 5 is constructed so as to run in the shed 4 from one side to the other by the rotation of a pinion 39 engaging with the rack 38. The shuttle 5 also has a rack engaging with the pinion 39 on its lower surface. When the other of the rods 28 stretches, the shuttle runs in the reverse direction. With the above drive mechanism, the operation by an air cylinder is preferable because the movement of the heald 3, the reed 9, the shuttle 5, and the auxiliary shedding device 19 is constant. For the up-and-down motion rack 7 and the woven fabric removing portion 10, a servomotor is preferably used because the moving amount must be changed depending on the thickness of warp 1 and weft 6 and the structure of woven fabric. Since all controls of aforesaid drive mechanisms are performed by a computer, the drive sequence can be changed and the drive amount for up-and-down motion rack 7 and the woven fabric removing portion 10 can be easily changed. Further, it is preferable that the group of bobbins 2 have a mechanism such that the tension of each warp can be controlled because the feed amount of each warp 1 set up to each heald differs. In Fig.2, reference numeral 29 denotes a servomotor for raising/lowering the woven fabric, and 30 denotes a servomotor for pulling out the woven fabric. In the above embodiment, the healds 3 are installed in parallel in the front and rear direction and moved vertically to form a shed 4 for the warp 1. However, a construction may be used in which the healds 3 are arranged vertically to run the warps from up to down and the healds are moved back and forth, so that the woven fabric is removed downward. Next, the operation will be described with reference to Figs.10 and 11. The warps la to lq pulled out from the group of bobbins 2 (not shown) are allowed to pass through the respective healds 3a to 3q and further pass through the reed 9, and then fixed to the woven fabric removing portion 10. It is preferable that the position of warp generally coincide with the arrangement sequence on the weaving start side as shown by a black circle (weft) in Fig.12. At this time, the up-and-down motion rack 7 is lowered down to a position where the shed centerline of the heald agrees with the shedding portion of woven fabric (first, the position of black circle). The shed centre line between the healds is aligned with the shed apex at the woven fabric fell. The shedding procedure is performed as shown in Fig.14. In addition to this shedding procedure, the operation sequence of each part is inputted in a computer beforehand. With a conventional weaving machine, the operation of each part is performed in the order of shedding, weft insertion, beating, and winding. When weaving is performed with the weaving machine of the present invention, the operation is basically performed in the order of shedding, weft insertion, beating, winding, and vertical movement. Only when the warp forming a selvedge appears, the operation is performed in the order of shedding, weft insertion, selvedge holding, beating, winding, and vertical movement. Fig.10 shows the state in which the beating of the 33rd step shown in Fig.14 has been completed (which differs slightly from the actual warp condition). In this state, the up-and-down motion rack 7 is adjusted in such a manner that the opening portion of the fabric may align with the height of passage of the shuttle supplying wefts. Fig.11 schematically shows the state in which the insertion of weft of the 35th step shown in Fig.14 has been completed. In this state, the warp In forming a selvedge appears at the lowermost position. Therefore, the holding of the selvedge 8a is then performed by the selvedge holding mechanism 11. After beating is performed, winding is carried out to proceed to the 36th step. Next, a weaving method for the in-plane multiaxial thick woven fabric 8 [Fig.13(i)] will be described with reference to Fig.13(a) through (h). In this embodiment, 12 warps 1A to 1E 3 and four stages of weft 6 are inserted. In this figure, the warp 1A, moving in a zigzag direction, composes the thickness direction of the woven fabric, and forms a loop 8a at each end. The warps 1B, 1C, 1D, 1F, 1G, 1H, 1J, and 1K compose the diagonal direction of the woven fabric, and the warps 1E 1 , 1E 2 , and 1E 3 compose the lengthwise direction of the woven fabric. Fig.13(a) shows the state in which the beating of second row has been completed just before the beating of third row starts. In this state, all healds for all warps are raised. Fig.13(b) shows the state in which the heald for the warp 1A lowers to the lowermost end, the heald for the warp 1F also lowers, and the weft 6a is inserted into the shedding portion formed between the warps 1H and 1F. In Fig.13(c), the healds for the warps 1H, 1E 3 , and 1B lower, and a shed is formed between the warp 1J and them. Fig.13(d) shows the state in which the weft 6b is inserted in the shed in Fig.13(c), the healds for the warps 1J, 1E 2 , and 1C lower so that the weft 6b is put between and wound by the warps 1J and 1B on the upper side of the weft 6a, and a shedding portion is formed between the warps 1C and 1K. Fig.13(e) shows the state in which the weft 6c is inserted in the shedding portion between the warps 1C and 1K, the healds for the warps 1K, 1E 1 , and 1D lower, the weft 6c is put between and wound by the warps 1C and 1K on the upper side of the weft 6b, and a shedding portion is formed between the warps 1D and 1G. Fig.13(f) shows the state in which the weft 6d is inserted in the shedding portion between the warps 1D and 1G, and the heald for the warp 1G lowers. In this state, the healds for all warps lower. In the state shown in Fig.13(g), the heald for the warp 1A rises from the lowermost end to the uppermost end, and the warp 1A wraps the wefts 6a to 6d. Fig.13(h) shows the state in which the healds for all warps rise, and the third row is formed. Although the embodiment of Fig.13 shows only one plane in the width direction of woven fabric 8, a woven fabric of a predetermined width is integrally manufactured in the direction of weft 6 at the same time. This state will be described with reference to Fig.15. A, B, C, and D in Fig.15 show respective warps 1a to 1q of one texture at the first stage 8A, the second stage 8B, the third stage 8C, and the fourth stage 8D in the width direction of the woven fabric 8. Fig.15 shows the state in which these warps pass the healds 3a to 3q to manufacture the woven fabric 8. In Fig.15, a, b, c, d show the mail of the first through fourth stages, respectively. Fig.13(i) is an expanded sectional view of a plane of the woven fabric 8. Although not shown in the above description of operation, just before the formation of selvedge due to the upper end warp 1A in Fig.13(a), the formation of selvedge due to the lower end warp 1A in Fig.13(b), the formation of selvedge due to the warp 1D in Fig.13(c), (d), and (e), the formation of selvedge of upper and lower portions due to warp 1G and 1A in Fig.13(f), and the formation of selvedge of lower end due to the warp 1F in Fig.13(g), the hook 11a of the selvedge holding mechanism 11 in Fig.5 is engaged with the selvedge forming portion due to these warps, by which the selvedge 8a of the woven fabric 8 is automatically fixed by the hook or the like with ease. Next, an example of time chart in accordanoe with the present invention will be described with reference to Fig.16. A winding roller is raised or lowered by the up-and-down motion rack driven by a servomotor in response to the shedding position; its operation is not particularly described. For the operation of the reed, the reed advances from the retracted position for the time period from 0 to 1 second to perform beating and weaving of the first row. For the time period from 1 to 6 seconds, the reed is at the retracted position. For the time period from 6 to 7 seconds, the reed performs the beating of the second row. Afterward, the same operation is repeated. The shedding of warp due to heald changes from #1 to #2 one second after the beating is completed. Afterward, the shedding remains in the condition of #2 until 7 seconds. When 7 seconds elapses, the shedding changes from #2 to #1, and afterward it remains in the condition of #1. The auxiliary shedding bar is at the retracted position until 2 seconds. It advances for the time period from 2 to 3 seconds, remains at the advanced position for the time period from 3 to 5 seconds, retracts for the time period from 5 to 6 seconds, and remains at the retracted position afterward. The auxiliary shed, which moves in association with the auxiliary shedding bar, closes for the time period from 0 to 3 seconds, opens for the time period from 3 to 3.5 seconds, remains open until 4.5 seconds, closes by 5 seconds, and afterward remains closed. The shuttle is at the retracted position until 3,5 seconds when beating, shedding of warp due to heald, and auxiliary shedding due to the auxiliary bar are performed. For the time period from 3.5 to 4.5 seconds, the shuttle advances to insert a weft into the shed of warp. This inserting condition continues to 8 seconds and afterward. In Figs.10 through 12, the weaving method in which wefts are piled vertically at five stages has been described, while in Fig.13, the weaving method in which wefts are piled vertically at four stages has been described. If the number of healds is increased, a vertically wide woven fabric can be manufactured. In this case, however, a sufficient shedding angle to pass the shuttle cannot sometimes be obtained. At this time, the auxiliary shedding device is used. After the auxiliary shedding device moves to between the warps after opening, it turns 90 degrees to forcedly open the warps , and provides a sufficient warp shedding angle to pass the shuttle. After the shuttle is passed, the auxiliary shedding device is returned to the original position to perform beating. The above embodiment has shown only one example; the present invention is not limited to this range.

Claims: A method of manufacturing in-plane multiaxial thick woven fabrics using a weaving machine comprising healds (3) through which warps (1) are passed, a shuttle (5) reciprocating so as to insert wefts (6) in a warp shedding portion formed by said healds (3), a reed (9), and a woven fabric take-up device (10), comprising the steps of: providing a large number of healds (3) arranged in rows both across the thickness of the fabric and parallel to the direction of woven fabric removal, forming a shed by passing warps (1) through said healds (3) of the number such that a predetermined thickness and width of woven fabric is formed and by widely reciprocating said healds (3) in the thickness direction, moving the shedding position sequentially from one side to the other side in the woven fabric thickness direction, inserting a weft (6) sequentially in subsequent shedding portions and arranging it by shifting the weft (6) position in the width direction, forming a first row of predetermined width and thickness by fixing warps (1), and manufacturing an in-plane multiaxial thick woven fabric of a continuous length by performing shedding, weft insertion, and beating sequentially, wherein when said subsequent shedding position shifts from the travel passage of said shuttle (5), said woven fabric take-up device (10) is moved vertically so that the horizontal centre-line between the healds (3) is aligned with the shed apex at the woven fabric fell. A method of manufacturing in-plane multiaxial thick woven fabric according to claim 1 wherein the thickness between selvedges (8a) formed by the warp at each end in the direction of the thickness of woven fabric to be manufactured is kept constant, by which the shrinkage of woven fabric in the thickness direction due to the tension of warp is prevented. A weaving machine for manufacturing in-plane multiaxial thick woven fabrics by the method according to claim 1, wherein warps (1) of the number such that predetermined thickness and width of woven fabric are formed through said healds (3) and said weaving machine is provided with a reciprocating mechanism for widely reciprocating said heald (3) in the woven fabric thickness direction, a mechanism for reciprocating said woven fabric take-up device (10) so that the horizontal centre-line between the healds (3) is aligned with the shed apex at the woven fabric fell, and a fixing mechanism for fixing the thickness of a selvedge (8a) in a constant manner by engaging said selvedge (8a) formed by warp at each end in the woven fabric thickness direction.

Inventors: NISHIYAMA SHIGERU, YAMAMOTO TETSUYA, NISHIYAMA, SHIGERU, YAMAMOTO, TETSUYA, Nishiyama, Shigeru, c/o Mitsubishi Jukogyo K.K., Yamamoto, Tetsuya, c/o Mitsubishi Jukogyo K.K.
Applicants: MITSUBISHI HEAVY IND LTD, MITSUBISHI JUKOGYO KABUSHIKI KAISHA
Application year: 1993
Main classification: D03D41
IPC codes: B32B5, D03D1, D03D25, D03D41, D03D11