Underneath type high-speed air jet loom carbon fiber heald frame and processing method thereof

Abstract

The invention provides an underneath type high-speed air jet loom carbon fiber heald frame and a processing method thereof.The underneath type high-speed air jet loom carbon fiber heald frame comprises two side baffles and carbon fiber cross beam plates, the two side baffles are arranged in a mirror image mode, the carbon fiber cross beam plates are arranged between the two side baffles, the two carbon fiber cross beam plates are arranged in a mirror image mode relative to the vertical center lines of the side baffles, and one sides of the side baffles are connected with corner joint assemblies; one side of each corner joint assembly is inserted into the corresponding carbon fiber cross beam plate, the two corner joint assemblies are arranged in a mirroring mode relative to the vertical center line of the side baffle, the transverse partition assemblies are arranged on the outer walls of the two carbon fiber cross beam plates, and the two sides of the transverse partition assemblies are fixedly connected with the two corner joint assemblies correspondingly; s1, processing a carbon fiber preassembled part; s2, a side frame preassembled part is machined; s3, positioning and pre-assembling are carried out; and S4, corner mounting and fixing. The side baffles and the corner joint assemblies are connected with the carbon fiber cross beam plates, meanwhile, the transverse partition assemblies and the corner joint assemblies are connected to form a rectangular peripheral structure, connection of the carbon fiber cross beam plates is reinforced, and the structural strength is further improved on the whole.

Description

Technical Field

[0001] The invention relates to the technical field of air jet looms, and in particular to a carbon fiber heald frame of a bottom-mounted high-speed air jet loom and a processing method thereof. Background Art

[0002] The heald frame is a key component in the air jet loom, which is mainly responsible for guiding and controlling the movement of the warp yarn to ensure the structure and quality of the fabric. The heald frame accurately guides each warp yarn to pass through, ensuring that the warp yarn is arranged according to the predetermined path to form a stable warp yarn layer. The increasing use of carbon fiber heald frames in high-speed air jet looms is mainly reflected in its unique performance advantages. Among them, the carbon fiber heald frame has extremely high strength and modulus, and can withstand huge mechanical stress during high-speed operation, ensuring the stability and reliability of the loom. In addition, its lightweight characteristics significantly reduce the overall weight of the loom, thereby reducing energy consumption and improving production efficiency. In addition, the carbon fiber heald frame also exhibits excellent corrosion resistance and thermal stability, and can maintain a good working condition for a long time in harsh working environments, extending the service life of the loom. These characteristics make the carbon fiber heald frame an indispensable key component of high-speed air jet looms, greatly improving the quality and efficiency of textile production.

[0003] At present, the carbon fiber heald frame mainly uses two carbon fiber cross beams as the supporting structure to connect the structure of guiding the warp yarn, and then uses the side blocks to fix it on the sides of the two carbon fiber cross beams. In order to ensure the structural strength, the side blocks of aluminum alloy materials are used, thereby ensuring the stability of the heald frame in reciprocating lifting to a certain extent. However, this kind of carbon fiber heald frame has the following problems:

[0004] 1. During the movement of the overall heald frame structure, the side guard is mainly subjected to force, but the carbon fiber cross beam plate is also subjected to the shear force of the side guard. As a result, after long-term use, the carbon fiber cross beam plate may break, resulting in structural instability, or even direct damage that affects processing;

[0005] 2. After long-term use, the side guards may be deformed and the connection with the carbon fiber cross beam plate may be offset, causing the overall structure to become loose and affecting the processing quality.

[0006] In summary, there is a need for a carbon fiber heald frame with high structural strength and stability. Summary of the invention

[0007] In view of the deficiencies in the prior art, the present invention provides a bottom-mounted high-speed air jet loom carbon fiber heald frame and a processing method thereof, which solves the problems mentioned in the background technology.

[0008] To achieve the above objectives, the present invention is implemented through the following technical solutions:

[0009] A carbon fiber heald frame of a bottom-mounted high-speed jet loom comprises a side fence and a carbon fiber cross beam plate, wherein two side fences are mirror-imaged, a carbon fiber cross beam plate is arranged between the two side fences, two carbon fiber cross beam plates are mirror-imaged about the vertical center line of the side fences, one side of the side fence is connected with an angle joint component, one side of the angle joint component is plugged into the inside of the carbon fiber cross beam plate, two groups of angle joint components are mirror-imaged about the vertical center line of the side fence, the outer walls of the two carbon fiber cross beam plates are both provided with a transverse partition component, the two sides of the transverse partition component are respectively fixedly connected to the two groups of angle joint components, the two side fences and the two groups of transverse partition components are fixedly connected through the angle joint components to form a rectangular peripheral structure, a plurality of docking blocks are fixedly provided on the inner wall of the carbon fiber cross beam plate, the carbon fiber cross beam plate is connected with a hanging component through the plurality of docking blocks, and one side of the hanging component is fixedly connected to the inner wall of the side fence;

[0010] The corner joint assembly includes a sleeve block, which is fixed to the side wall of the side guard, one side of the carbon fiber cross beam plate is inserted into the sleeve block, a second inner plug-in block is fixed inside the sleeve block, a first docking groove and a second docking groove are provided through the carbon fiber cross beam plate, the second inner plug-in block is inserted into the second docking groove, the first inner plug-in blocks are fixed to the inner walls on both sides of the side guard, the first baffles are fixed on both sides of the first inner plug-in block, the first inner plug-in block is inserted into the first docking groove, and the first baffles are attached to the side wall of the carbon fiber cross beam plate;

[0011] The corner joint assembly also includes a card top block, a first fixing plate, a second fixing plate, an inner top component and a reinforcement plate, the first fixing plate is fixed to the outer wall of the sleeve block, the second fixing plate is fixed to the side wall of the first fixing plate, the inner top component is penetrated inside the second fixing plate, a reinforcement plate is fixed to one side of the second fixing plate, a first slot is opened on the outer wall on one side of the side guard, the reinforcement plate is inserted into the first slot, a second slot of a T-shaped structure is opened between the sleeve block and the second inner plug-in block, openings on both sides of the second slot respectively penetrate through the two side walls of the second inner plug-in block, two card top blocks are mirrored inside the second slot, a pressure sensor is embedded in the side wall of the card top block, one side of the inner top component is inserted into the second slot, two card slots are opened on the inner wall of the second docking groove, the card top block is pushed out and extended through the inner top component to be inserted into the card slot, and one side of the pressure sensor is attached to the inner wall of the card slot.

[0012] Furthermore, the inner top component includes an adjusting bolt, a first spring, a first push plate and an inserting top plate, the adjusting bolt is threadedly connected to the inside of the second fixed plate, the first spring is sleeved on the outer wall of the adjusting bolt, one end of the adjusting bolt is rotatably connected to the first push plate, the side wall of the first push plate is fixed with an inserting top plate, the inserting top plate is inserted into the inside of the second slot, and the side of the inserting top plate away from the first push plate is a V-shaped structure, the V-shaped structure of the inserting top plate is used to push and separate the two top blocks, and the adjacent sides of the two top blocks are provided with an inclined surface structure.

[0013] Furthermore, the transverse partition assembly includes a heat conducting plate, a wear plate, a conduit, an axial connection block and a clamping plate. The heat conducting plate is fixed to the outer wall of the carbon fiber beam plate, and multiple heat conducting plates are arranged at intervals. Wear plates are fixed on both sides of the heat conducting plate, and the wear plates are fixed to the side walls of the carbon fiber beam plate. The conduit penetrates and is connected to the interior of multiple heat conducting plates. The outer walls at both ends of the conduit are sleeved with axial connection blocks, and a clamping plate with an inverted concave structure is fixed to the bottom surface of the axial connection block. The clamping plate is sleeved on the sleeve block and the outer wall of the side block. The outer wall of the side block is provided with a first protrusion, and one side of the clamping plate is fitted to the side wall of the first protrusion.

[0014] Furthermore, a heat dissipation groove is opened inside the heat conduction plate, a conduit is connected to the inside of the heat dissipation groove, a plurality of first air outlet holes are opened on the outer wall of the conduit close to the carbon fiber cross beam plate, and second air outlet holes are opened on the outer wall of the conduit that pass through the upper and lower parts, and the second air outlet holes are arranged inside the heat dissipation groove.

[0015] Furthermore, the hanging assembly includes a hanging plate, a corner block and a first limit block. The corner block is an L-shaped structure. Two corner blocks are mirrored. The two sides of the hanging plate are respectively inserted into the two corner blocks. One side of the corner block is right-angled to the inner wall of the carbon fiber beam plate, and the other side of the corner block is right-angled to the inner wall of the side block. The outer wall of the hanging plate is slidably sleeved with the first limit block. A second protrusion is provided on one side of the first limit block. The second protrusion is translated and inserted into the docking block through the first limit block.

[0016] A method for processing a carbon fiber heald frame of a bottom-mounted high-speed air jet loom, according to the above-mentioned carbon fiber heald frame of the bottom-mounted high-speed air jet loom, the processing method comprises the following steps:

[0017] S1, carbon fiber pre-assembled parts processing;

[0018] The carbon fiber cloth and carbon fiber filaments are impregnated with glue, and the carbon fiber cross beam plate is formed by heating the mold, cut and punched according to the product length, a plurality of docking blocks are fixed on the carbon fiber cross beam plate, the heat conduction plate is bonded to the outer wall of the carbon fiber cross beam plate, the grinding plate is bonded to both sides of the heat conduction plate and the carbon fiber cross beam plate, and the conduit is inserted into the interior of the heat conduction plate to obtain the carbon fiber preassembled part;

[0019] S2, side frame pre-assembled parts processing;

[0020] Cut and drill the aluminum alloy side guard, weld two sets of blocks to both sides of the side guard, grind and remove burrs, and obtain the side frame pre-assembled parts;

[0021] S3, positioning pre-assembly;

[0022] Positioning and placing two sets of carbon fiber pre-assembled parts on the assembly equipment, placing two sets of side frame pre-assembled parts and two sets of hanging components on the assembly equipment at the same time, starting the assembly equipment to simultaneously assemble the two sets of side frame pre-assembled parts and the two sets of hanging components and dock with the two sets of carbon fiber pre-assembled parts, and initially forming a frame structure;

[0023] The assembly equipment includes a bottom plate, a pushing component, a pushing component and a lifting and positioning component. The top surface of the bottom plate is provided with four groups of lifting and positioning components in a rectangular distribution. A pushing component is provided on the top surface of one side of the bottom plate. Two groups of pushing components are provided with a mirror image of the vertical center line of the bottom plate. A pushing component is connected between the two groups of pushing components. Two groups of pushing components are provided with a mirror image of the vertical center line of the pushing component. The lifting and positioning component is used to position and clamp the carbon fiber pre-assembled parts. The pushing component is used to position and assemble the side frame pre-assembled parts. The pushing component is pushed horizontally by the pushing component to clamp the hanging component.

[0024] S4, corner fixing;

[0025] Assemble the complete corner joint assembly and the cross partition assembly, and fix the hanging assembly between the carbon fiber cross beam plate and the side guard.

[0026] Furthermore, the pushing assembly includes a support seat, a first pneumatic rod, a second push plate, a tooth plate and a pushing and rotating component. The support seat is fixed to the top surface of the base plate, a slide groove is arranged on the top surface of the support seat, a first pneumatic rod is arranged on the side wall of the support seat, the telescopic end of the first pneumatic rod is connected to the inside of the slide groove, the telescopic end of the first pneumatic rod is connected to the second push plate, the second push plate is used to push the translational assembly of the side frame pre-assembled parts, the top of the second push plate slides and fits against the top surface of the support seat, the first connecting plates are fixed on both sides of the second push plate, the side walls of the first connecting plates are connected to the tooth plate, the tooth plate is slidably connected to the inside of the support seat, the side walls of the support seat are provided with a pushing and rotating component, two groups of pushing and rotating components are arranged in a mirror image about the vertical center line of the support seat, one side of the pushing and rotating component is connected to the pushing assembly, one side of the tooth plate is connected to the inside of the pushing and rotating component, and the pushing and rotating component is pushed by the tooth plate to translate the pushing assembly.

[0027] Furthermore, the pushing and rotating component includes a bracket, a first gear, a bracket seat, a push block and a screw rod. The bracket is fixed to the side wall of the support seat, and a screw rod is rotatably connected inside the bracket. The outer wall of one end of the screw rod is sleeved with a first gear, and the top of the first gear is meshingly connected with the bottom surface of the toothed plate. The outer wall of the screw rod is threadedly sleeved with a push block, and one side of the push block is slidably fitted with the side wall of the support seat. A bracket seat is fixed to the top surface of the push block, and the top surface of the bracket seat is provided with a groove structure for cooperating with the insertion of the corner block.

[0028] Further, the push assembly includes a first support plate, a motor, a second gear, a third push plate and a push card component, the first support plate is fixed to the side wall of the push block, a plurality of second limit blocks are fixed to the top surface of the first support plate, the third push plate is connected through the plurality of second limit blocks, a motor is arranged on the top surface of the first support plate, a second gear is connected to the rotating end of the motor, the bottom of the second gear is meshedly connected to the top surface of one side of the third push plate, a plurality of groups of push card components are arranged on the top surface of the third push plate, and the push card components are used to push the first limit block horizontally to be inserted into the docking block;

[0029] The pushing card component includes a fixed block, a second support plate, a positioning block, a fourth push plate, a guide rod, a second spring and a third limit block. The fixed block is fixed to the top surface of the third push plate, the second support plate is fixed on the top surface of the fixed block, the positioning block is fixed on the top surface of one side of the second support plate, the third limit block is fixed on the top surface of the other side of the second support plate, a guide rod is inserted into the inside of the third limit block, the second spring is sleeved on the outer wall of the guide rod, the fourth push plate is connected to one end of the guide rod close to the positioning block, and the distance between the fourth push plate and the positioning block is greater than the width of the first limit block.

[0030] Furthermore, the lifting and positioning assembly includes a second connecting plate, a second baffle, a third baffle, a second pneumatic rod and a lifting plate. The second baffle and the third baffle are respectively fixed on both sides of the second connecting plate. The second baffle and the third baffle are both fixed to the top surface of the bottom plate. The second pneumatic rod is arranged on the bottom surface of the second connecting plate. The telescopic top end of the second pneumatic rod passes through the top of the second connecting plate. The telescopic top end of the second pneumatic rod is connected to the lifting plate, and the lifting plate is fitted between the second baffle and the third baffle.

[0031] The present invention provides a carbon fiber heald frame of a bottom-mounted high-speed air jet loom and a processing method thereof. Compared with the prior art, the present invention has the following beneficial effects:

[0032] 1. By connecting the side guards and corner joint components with the carbon fiber cross beam plate, and connecting the cross partition components with the corner joint components to form a rectangular peripheral structure, the connection to the carbon fiber cross beam plate is strengthened, and the overall structural strength is further improved, ensuring the overall working stability of the heald frame;

[0033] 2. Connect between the carbon fiber cross beam plate and the side guard through the corner joint assembly, insert the second inner plug-in block into the carbon fiber cross beam plate for reinforcement, and then push the card top block with the pressure sensor into the carbon fiber cross beam plate through the inner top component, which not only further strengthens the fixing strength of the carbon fiber cross beam plate, but also uses the pressure sensor to monitor the internal fixing pressure. When the pressure changes after long-term work, the card top block can be quickly adjusted by adjusting the inner top component. The adjustment operation is simple and efficient, which further ensures the stability of the fixation of the carbon fiber cross beam plate;

[0034] 3. The top block is clamped inside the carbon fiber beam plate to ensure the stability of the fixed structure. When the pressure sensor does not reach the pressure standard, it is only necessary to turn the adjustment bolt to push the top plate to further push the top block out to ensure the stability of the internal fixed structure and facilitate the adjustment operation;

[0035] 4. Connect the pipes through multiple heat-conducting plates, and then further fix them through shaft blocks and clamping plates to ensure the stability of the structure;

[0036] 5. By adopting the heat conduction plate and the wear plate structure, the wear plate can be used to fit and limit the wear plate on other heald frames to ensure the stability of the heald frame lifting and lowering. The wear-resistant wear plate is used for fitting and friction to reduce friction loss and ensure the stability of the structure. The heat generated by the friction of the wear-resistant plate is conducted to the heat conduction plate so that the heat can be dissipated, further ensuring the stability of the heald frame operation. BRIEF DESCRIPTION OF THE DRAWINGS

[0037] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0038] Figure 1 A schematic diagram of the structure of a carbon fiber heald frame of a bottom-mounted high-speed air jet loom of the present invention is shown;

[0039] Figure 2 An exploded view of the overall structure of the present invention is shown;

[0040] Figure 3 A schematic diagram of the connection structure between the corner joint assembly and the side guard of the present invention is shown;

[0041] Figure 4 An exploded view of the corner joint assembly structure of the present invention is shown;

[0042] Figure 5 A cross-sectional view of the internal connection structure of the corner joint assembly, the side guard and the carbon fiber cross beam plate of the present invention is shown;

[0043] Figure 6 The schematic diagram of the internal structure of the sleeve block of the present invention is shown;

[0044] Figure 7 Shows Figure 1 A local enlarged structural schematic diagram;

[0045] Figure 8 A cross-sectional view of the internal connection structure of the conduit and the heat conducting plate of the present invention is shown;

[0046] Fig. 9 A schematic diagram of the structure of the hook assembly of the present invention is shown;

[0047] Fig.10 A schematic diagram of the structure of the assembling device of the present invention is shown;

[0048] Fig.11 A schematic diagram of the structure of the push component of the present invention is shown;

[0049] Fig.12A schematic diagram of the internal structure of the push component of the present invention is shown;

[0050] Fig.13 A schematic diagram of the push-on assembly structure of the present invention is shown;

[0051] Fig.14 A schematic diagram of the structure of the lifting and positioning assembly of the present invention is shown;

[0052] Fig.15 It shows a schematic structural diagram of the state in which the pre-assembled parts of the present invention are placed on an assembling device;

[0053] Fig.16 It shows a schematic structural diagram of the pre-assembly state of the heald frame of the assembling equipment of the present invention;

[0054] As shown in the figure: 1, side guard; 11, first protrusion; 12, first baffle; 13, first slot; 14, first insert block; 2, carbon fiber cross beam plate; 21, docking block; 22, first docking slot; 221, card slot; 23, second docking slot; 3, partition assembly; 31, heat conduction plate; 311, heat dissipation slot; 32, wear plate; 33, duct; 331, first air outlet; 332, second air outlet; 34, shaft Connecting block; 35, clamping plate; 4, corner joint assembly; 41, sleeve block; 411, second slot; 412, second inner plug-in block; 42, top block; 421, pressure sensor; 43, first fixing plate; 44, second fixing plate; 45, inner top component; 451, adjustment bolt; 452, first spring; 453, first push plate; 454, plug-in top plate; 46, reinforcement plate; 5, hanging assembly; 51, hanging plate; 52, corner block ; 53, first limit block; 531, second protrusion; 6, bottom plate; 7, push assembly; 71, support seat; 711, slide groove; 72, first pneumatic rod; 73, second push plate; 731, first connecting plate; 74, tooth plate; 75, push-transfer component; 751, bracket; 752, first gear; 753, bracket seat; 754, push block; 755, screw; 8, push assembly; 81, first support plate; 811, first The second limit block; 82, the motor; 83, the second gear; 84, the third push plate; 85, the push-card component; 851, the fixing block; 852, the second support plate; 853, the positioning block; 854, the fourth push plate; 855, the guide rod; 856, the second spring; 857, the third limit block; 9, the lifting and positioning assembly; 91, the second connecting plate; 92, the second baffle plate; 93, the third baffle plate; 94, the second pneumatic rod; 95, the lifting plate. DETAILED DESCRIPTION

[0055] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention are clearly and completely described. Obviously, the described embodiments are part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0056] Embodiment 1

[0057] In order to solve the technical problems in the background technology, the following bottom-mounted high-speed air jet loom carbon fiber heald frame is provided:

[0058] Combination Figure 1-Figure 9 As shown, the carbon fiber heald frame of the bottom-mounted high-speed air jet loom provided by the present invention comprises a side fence 1 and a carbon fiber cross beam plate 2, wherein two side fences 1 are arranged in a mirror image, a carbon fiber cross beam plate 2 is arranged between the two side fences 1, and two carbon fiber cross beam plates 2 are arranged in a mirror image with respect to the vertical center line of the side fence 1, one side of the side fence 1 is connected with an angle joint component 4, one side of the angle joint component 4 is plugged into the inside of the carbon fiber cross beam plate 2, and two groups of angle joint components 4 are arranged in a mirror image with respect to the vertical center line of the side fence 1, and the outer walls of the two carbon fiber cross beam plates 2 are both provided with a transverse partition component 3, and the two sides of the transverse partition component 3 are respectively fixedly connected to the two groups of angle joint components 4, and the two side fences 1 and the two groups of transverse partition components 3 are fixedly connected through the angle joint component 4 to form a rectangular peripheral structure, and a plurality of docking blocks 21 are fixed to the inner wall of the carbon fiber cross beam plate 2, and the carbon fiber cross beam plate 2 is connected to a hanging component 5 through a plurality of docking blocks 21, and one side of the hanging component 5 is fixedly connected to the inner wall of the side fence 1;

[0059] The corner joint assembly 4 includes a sleeve block 41, which is fixed to the side wall of the side guard 1, one side of the carbon fiber cross beam plate 2 is inserted into the sleeve block 41, a second inner plug-in block 412 is fixed inside the sleeve block 41, a first docking groove 22 and a second docking groove 23 are provided through the carbon fiber cross beam plate 2, the second inner plug-in block 412 is inserted into the second docking groove 23, first inner plug-in blocks 14 are fixed to the inner walls on both sides of the side guard 1, first baffles 12 are fixed to both sides of the first inner plug-in block 14, the first inner plug-in block 14 is inserted into the first docking groove 22, and the first baffle 12 is attached to the side wall of the carbon fiber cross beam plate 2;

[0060] The corner joint assembly 4 also includes a card top block 42, a first fixing plate 43, a second fixing plate 44, an inner top component 45 and a reinforcing plate 46. The first fixing plate 43 is fixed to the outer wall of the sleeve block 41, the second fixing plate 44 is fixed to the side wall of the first fixing plate 43, the inner top component 45 is penetrated inside the second fixing plate 44, and a reinforcing plate 46 is fixed to one side of the second fixing plate 44. A first slot 13 is opened on the outer wall of one side of the side guard 1, and the reinforcing plate 46 is inserted into the first slot 13. A slot 13 is opened between the sleeve block 41 and the second inner insert block 412. The second slot 411 has a T-shaped structure, and openings on both sides of the second slot 411 are respectively connected to the two side walls of the second inserted block 412. Two card top blocks 42 are mirror-imaged inside the second slot 411, and a pressure sensor 421 is embedded in the side wall of the card top block 42. One side of the inner top component 45 is inserted into the second slot 411. Two card slots 221 are provided on the inner wall of the second docking groove 23. The card top block 42 is pushed outward by the inner top component 45 and inserted into the card slot 221. One side of the pressure sensor 421 is attached to the inner wall of the card slot 221.

[0061] According to the above structure, the following effects can be achieved:

[0062] 1. By connecting the side guard 1 and the corner joint assembly 4 with the carbon fiber cross beam plate 2, and connecting the cross partition assembly 3 with the corner joint assembly 4 to form a rectangular peripheral structure, not only the connection to the carbon fiber cross beam plate 2 is strengthened, but also the structural strength is further improved as a whole, ensuring the overall working stability of the heald frame;

[0063] 2. Connect the carbon fiber cross beam plate 2 and the side guard 1 through the corner joint component 4, insert the second inner plug-in block 412 into the carbon fiber cross beam plate 2 for reinforcement, and then push the card top block 42 with the pressure sensor 421 into the carbon fiber cross beam plate 2 through the inner top component 45, which not only further strengthens the fixing strength of the carbon fiber cross beam plate 2, but also uses the pressure sensor 421 to monitor the internal fixing pressure. When the pressure changes after long-term work, the card top block 42 can be quickly adjusted by adjusting the inner top component 45. The adjustment operation is simple and efficient, which further ensures the stability of the fixation of the carbon fiber cross beam plate 2.

[0064] In this embodiment, the inner top component 45 includes an adjusting bolt 451, a first spring 452, a first push plate 453 and an inserting top plate 454. The adjusting bolt 451 is threadedly connected to the inside of the second fixed plate 44. The outer wall of the adjusting bolt 451 is sleeved with the first spring 452. One end of the adjusting bolt 451 is rotatably connected to the first push plate 453. The side wall of the first push plate 453 is fixed with an inserting top plate 454. The inserting top plate 454 is inserted into the inside of the second slot 411. The side of the inserting top plate 454 away from the first push plate 453 is a V-shaped structure. The V-shaped structure of the inserting top plate 454 is used to push and separate the two card top blocks 42. The adjacent sides of the two card top blocks 42 are both provided with an inclined surface structure.

[0065] The top block 42 is clamped inside the carbon fiber cross beam plate 2 to ensure the stability of the fixed structure. When the pressure sensor 421 does not reach the pressure standard, it is only necessary to rotate the adjustment bolt 451 to push the top plate 454 to further push the top block 42 out to ensure the stability of the internal fixed structure and facilitate the adjustment operation.

[0066] In this embodiment, the diaphragm assembly 3 includes a heat conducting plate 31, a wear plate 32, a conduit 33, an axis connecting block 34 and a clamping plate 35. The heat conducting plate 31 is fixed to the outer wall of the carbon fiber cross beam plate 2. A plurality of heat conducting plates 31 are arranged at intervals. Wear plates 32 are fixed on both sides of the heat conducting plate 31. The wear plates 32 are fixed to the side walls of the carbon fiber cross beam plate 2. The conduit 33 penetrates and connects to the interior of the plurality of heat conducting plates 31. The outer walls at both ends of the conduit 33 are sleeved with axis connecting blocks 34. The bottom surface of the axis connecting block 34 is fixed with a clamping plate 35 with an inverted concave structure. The clamping plate 35 is sleeved on the sleeve block 41 and the outer wall of the side guard 1. The outer wall of the side guard 1 is provided with a first protrusion 11. One side of the clamping plate 35 is fitted to the side wall of the first protrusion 11.

[0067] The conduit 33 is connected to the inside of the plurality of heat conducting plates 31 and then further fixedly connected by the shaft connection block 34 and the clamping plate 35 to ensure the stability of the structure;

[0068] By adopting the structure of the heat conducting plate 31 and the wearing plate 32, the wearing plate 32 can be used to fit and limit the position of the wearing plate 32 on other heald frames to ensure the stability of the lifting and lowering of the heald frames. The wear-resistant wearing plate 32 is used for fitting and friction to reduce friction loss and ensure the stability of the structure. The heat generated by the friction of the wear-resistant plate is conducted to the heat conducting plate 31 so that the heat can be dissipated, thereby further ensuring the stability of the operation of the heald frames.

[0069] In this embodiment, a heat dissipation slot 311 is provided inside the heat conducting plate 31, and a conduit 33 is connected to the inside of the heat dissipation slot 311. A plurality of first air outlet holes 331 are provided on the outer wall of the conduit 33 close to the carbon fiber cross beam plate 2, and a second air outlet hole 332 is provided on the outer wall of the conduit 33 that passes through from top to bottom. The second air outlet hole 332 is provided inside the heat dissipation slot 311.

[0070] By arranging the first air outlet hole 331 and the second air outlet hole 332 on the conduit 33, when the external air pump is connected to the inside of the conduit 33 and inflated, the first air outlet hole 331 can blow air to clean the carbon fiber beam plate 2 to ensure the stability of the structure of the carbon fiber beam plate 2, and at the same time, the second air outlet hole 332 blows air inside the heat dissipation groove 311 to improve the heat dissipation efficiency of the heat conducting plate 31.

[0071] In this embodiment, the hanging assembly 5 includes a hanging plate 51, an angle block 52 and a first limit block 53. The angle block 52 is an L-shaped structure. Two angle blocks 52 are mirror-imaged. The two sides of the hanging plate 51 are respectively inserted into the two angle blocks 52. One side of the angle block 52 is right-angled to the inner wall of the carbon fiber cross beam plate 2, and the other side of the angle block 52 is right-angled to the inner wall of the side block 1. The outer wall of the hanging plate 51 is slidably sleeved with the first limit block 53. A second protrusion 531 is provided on one side of the first limit block 53. The second protrusion 531 is translated and inserted into the docking block 21 through the first limit block 53.

[0072] The hanging plate 51 for hanging the heald pieces is fixed with two corner blocks 52, and one right-angled side of the corner block 52 is clamped on the carbon fiber cross beam plate 2, while the other side of the corner block 52 is fixed on the side guard 1, thereby further improving the overall structural strength inside the heald frame.

[0073] Embodiment 2

[0074] In order to solve the technical problems in the background technology, the following processing method of a carbon fiber heald frame of a bottom-mounted high-speed air jet loom is provided:

[0075] Combination Figure 1-Figure 16 As shown, the present invention provides a method for processing a carbon fiber heald frame of a bottom-mounted high-speed air jet loom. According to the above-mentioned carbon fiber heald frame of the bottom-mounted high-speed air jet loom, the processing method comprises the following steps:

[0076] S1, carbon fiber pre-assembled parts processing;

[0077] The carbon fiber cloth and carbon fiber filaments are impregnated with glue, and heated in a mold to form a carbon fiber cross beam plate 2, which is cut and punched according to the product length, and a plurality of docking blocks 21 are fixed on the carbon fiber cross beam plate 2, and a heat conducting plate 31 is bonded to the outer wall of the carbon fiber cross beam plate 2, and a grinding plate 32 is bonded to both sides of the heat conducting plate 31 and the carbon fiber cross beam plate 2, and a conduit 33 is inserted into the interior of the heat conducting plate 31 to obtain a carbon fiber preassembled part;

[0078] S2, side frame pre-assembly processing;

[0079] The aluminum alloy side guard 1 is cut and drilled, two sleeve blocks 41 are welded to both sides of the side guard 1, and the burrs are removed by grinding to obtain a side frame pre-assembled part;

[0080] S3, positioning pre-assembly;

[0081] Positioning and placing two sets of carbon fiber pre-assembled parts on the assembly equipment, placing two sets of side frame pre-assembled parts and two sets of hanging components 5 on the assembly equipment at the same time, starting the assembly equipment to simultaneously assemble the two sets of side frame pre-assembled parts and the two sets of hanging components 5 and the two sets of carbon fiber pre-assembled parts to initially form a frame structure;

[0082] The assembly equipment includes a bottom plate 6, a pushing component 7, a pushing component 8 and a lifting and positioning component 9. Four groups of lifting and positioning components 9 are arranged on the top surface of the bottom plate 6 in a rectangular distribution. A pushing component 7 is arranged on the top surface of one side of the bottom plate 6. Two groups of pushing components 7 are arranged in a mirror image with respect to the vertical center line of the bottom plate 6. A pushing component 8 is connected between the two groups of pushing components 7. Two groups of pushing components 8 are arranged in a mirror image with respect to the vertical center line of the pushing component 7. The lifting and positioning component 9 is used to position and clamp the carbon fiber pre-assembled parts. The pushing component 7 is used to position and assemble the side frame pre-assembled parts. The pushing component 8 is pushed horizontally by the pushing component 7 to clamp the hanging component 5.

[0083] The above steps are specifically as follows: two groups of carbon fiber pre-assembled parts are positioned and placed on the lifting plate 95, and the carbon fiber cross beam plate 2 is fit and limited by the second baffle plate 92 and the third baffle plate 93, and two groups of side frame pre-assembled parts are placed on the support seat 71 at the same time, and fit with the top surface of the support seat 71, and the two first protrusions 11 on the side gear 1 are respectively fit and limited on the top surfaces of both sides of the support seat 71, and the second push plate 73 is fit with the side gear 1, and then the two groups of hanging components 5 are respectively placed on the two groups of pushing components 8, so that the multiple first limiting blocks 53 are respectively fit on the second supporting plate 852 of the multiple groups of pushing components 85, so that the first limiting block 53 is between the fourth push plate 854 and the positioning block 853, and at the same time, the two sides of the hanging plate 51 and the connected corner blocks 52 are matched and inserted on the top surface of the plug-in seat 753;

[0084] After positioning and placing the above-mentioned main components, the two first pneumatic rods 72 are started to pull the second push plate 73, and the second push plate 73 pushes the side frame pre-assembled parts on the top surface of the support seat 71 to translate toward the sides of the two carbon fiber cross beam plates 2, so that the sleeve block 41 is inserted into the outside of the side of the carbon fiber cross beam plate 2, and the second insert block 412 is inserted into the second docking groove 23, and at the same time, the first insert block 14 is inserted into the first docking groove 22, and the first baffle plate 12 is attached to the outer wall of the carbon fiber cross beam plate 2;

[0085] At the same time, the second push plate 73 drives the tooth plate 74 to move, the tooth plate 74 drives the first gear 752 to rotate, the screw rod 755 drives the push block 754 to translate, and the push block 754 drives the push assembly 8 to translate toward the carbon fiber beam plate 2 as a whole, so that the hanging assembly 5 translates toward the carbon fiber beam plate 2, and one side of the corner block 52 is clamped on the inner wall of the carbon fiber beam plate 2. At the same time, the second protrusions 531 on the multiple first limit blocks 53 are aligned with the sockets on the docking block 21, and then the motor 82 is started to drive the second gear 83 to rotate, and the second gear 83 drives the third push plate 84 to translate, and synchronously pushes the multiple fourth push plates 854 to translate to synchronously insert the second protrusions 531 of the multiple first limit blocks 53 into the docking block 21, thereby initially forming a frame structure;

[0086] S4, corner mounting and fixing;

[0087] Assemble the complete corner joint assembly 4 and the cross partition assembly 3, and fix the hanging assembly 5 between the carbon fiber cross beam plate 2 and the side guard 1;

[0088] The above steps are specifically as follows: fit the two card top blocks 42 of the magnetic material together, so that the inclined surface structures of the card top blocks 42 are assembled together, and inserted into the second slot 411 of the sleeve block 41, so that the inclined surface structure faces the outside of the opening of the second slot 411, and then insert the top plate 454 into the second slot 411, and the top plate 454 pushes the two card top blocks 42 into the second inner insert block 412 until the two card top blocks 42 reach the other two openings of the second slot 411, and the top plate 454 pushes the two card top blocks 42 to separate, and the card top block 42 extends out of the second inner insert block 412 and is inserted into the carbon The pressure sensor 421 is attached to the inner wall of the slot 221 inside the fiber beam plate 2, and the first fixing plate 43 is attached to the outer wall of the sleeve block 41. The reinforcement plate 46 is inserted into the first slot 13. The first fixing plate 43, the sleeve block 41 and the carbon fiber beam plate 2 are fixedly connected by fixing bolts, the reinforcement plate 46 and the side guard 1 are fixedly connected by fixing bolts, the second fixing plate 44 and the sleeve block 41 are fixedly connected by fixing bolts, and the first push plate 453 is set between the sleeve block 41 and the second fixing plate 44, and a space for the first push plate 453 to move in translation is reserved;

[0089] The corner block 52 and the side guard 1 are fixed together by fixing bolts, the clamping plate 35 is translated and clamped on the outer wall of the sleeve block 41, one side of the clamping plate 35 is fitted with the first protrusion 11, and the shaft connection block 34 on the clamping plate 35 is translated, and the guide tube 33 is passed through the shaft connection block 34 and fixed to the outer wall of the guide tube 33 protruding outward by nuts, and the clamping plate 35 is fixed to the side guard 1 by fixing bolts, so as to complete the assembly of a right angle position of the heald frame, and the other three right angle positions are assembled in the same way, so that the overall assembly of the heald frame is completed;

[0090] Then, the adjusting bolts 451 at the four corners of the heald frame are rotated respectively, and the adjusting bolts 451 push the first push plate 453 to move so that the top plate 454 is further inserted into the second slot 411, and the top plate 454 pushes the top card block 42 to further separate, so that the pressure sensor 421 is pressed tightly against the inside of the card slot 221 until the pressure of the pressure sensor 421 reaches the required fixed pressure value, thereby ensuring the internal fixing strength of the four corners of the heald frame, and monitoring the fixing pressure in the later use, and only need to rotate the adjusting bolt 451 to adjust to ensure the fixing strength;

[0091] Finally, the second pneumatic rod 94 is started to push the lifting plate 95 upward, so that the assembled and debugged heald frame is lifted as a whole for easy removal.

[0092] In this embodiment, the pushing assembly 7 includes a support seat 71, a first pneumatic rod 72, a second push plate 73, a tooth plate 74 and a push-turning component 75. The support seat 71 is fixed to the top surface of the bottom plate 6. The top surface of the support seat 71 is provided with a slide groove 711. The side wall of the support seat 71 is provided with a first pneumatic rod 72. The telescopic end of the first pneumatic rod 72 is connected to the inside of the slide groove 711. The telescopic end of the first pneumatic rod 72 is connected to the second push plate 73. The second push plate 73 is used to push the translational assembly of the side frame preassembled parts. The second push plate 73 is The first connecting plate 731 is fixed on both sides of the second push plate 73, and the side wall of the first connecting plate 731 is connected with a tooth plate 74, and the tooth plate 74 is slidably connected to the inside of the support seat 71. The side wall of the support seat 71 is provided with a push-pushing component 75, and the push-pushing component 75 is mirrored with two groups about the vertical center line of the support seat 71. One side of the push-pushing component 75 is connected with a push-installation assembly 8, and one side of the tooth plate 74 is connected to the inside of the push-pushing component 75. The push-pushing component 75 is pushed by the tooth plate 74 to make the push-installation assembly 8 translate.

[0093] The first pneumatic rod 72 pulls the second push plate 73 to assemble the side frame pre-assembled parts, and at the same time drives the tooth plate 74 to move, so as to drive the push component 75 to drive the push assembly 8 to move horizontally, thereby realizing synchronous operation, which can improve the efficiency and convenience of the pre-assembly of the whole heald frame.

[0094] In this embodiment, the push-turning component 75 includes a bracket 751, a first gear 752, a socket 753, a push block 754 and a screw 755. The bracket 751 is fixed to the side wall of the support seat 71. The bracket 751 is rotatably connected with the screw 755 inside. The outer wall of one end of the screw 755 is sleeved with the first gear 752. The top of the first gear 752 is meshed with the bottom surface of the toothed plate 74. The outer wall of the screw 755 is threadedly sleeved with the push block 754. One side of the push block 754 is slidably fitted with the side wall of the support seat 71. The top surface of the push block 754 is fixed with the socket 753. The top surface of the socket 753 is provided with a groove structure for matching the insertion of the corner block 52.

[0095] After positioning the corner block 52 of the hanging assembly 5 on the top surface of the socket 753, while assembling the side frame pre-assembled parts, the toothed plate 74 drives the first gear 752 to rotate, so that the screw rod 755 drives the push block 754 to move, thereby translating the hanging assembly 5 to approach the carbon fiber cross beam plate 2, and the assembly operation is simple and stable.

[0096] In this embodiment, the push assembly 8 includes a first support plate 81, a motor 82, a second gear 83, a third push plate 84 and a push card component 85. The first support plate 81 is fixed to the side wall of the push block 754. A plurality of second limit blocks 811 are fixed to the top surface of the first support plate 81. The third push plate 84 is connected to the inside of the plurality of second limit blocks 811 through the third push plate 84. A motor 82 is provided on the top surface of the first support plate 81. The rotating end of the motor 82 is connected to the second gear 83. The bottom of the second gear 83 is meshedly connected to the top surface of one side of the third push plate 84. A plurality of push card components 85 are provided on the top surface of the third push plate 84. The push card components 85 are used to push the first limit block 53 horizontally to be inserted into the docking block 21.

[0097] The push card component 85 includes a fixed block 851, a second support plate 852, a positioning block 853, a fourth push plate 854, a guide rod 855, a second spring 856 and a third limit block 857. The fixed block 851 is fixed to the top surface of the third push plate 84, the second support plate 852 is fixed to the top surface of the fixed block 851, the positioning block 853 is fixed to the top surface of one side of the second support plate 852, and the third limit block 857 is fixed to the top surface of the other side of the second support plate 852. The guide rod 855 is inserted into the third limit block 857, and the second spring 856 is sleeved on the outer wall of the guide rod 855. The fourth push plate 854 is connected to the end of the guide rod 855 close to the positioning block 853, and the distance between the fourth push plate 854 and the positioning block 853 is greater than the width of the first limit block 53.

[0098] By setting a larger distance between the fourth push plate 854 and the positioning block 853, it is convenient to insert the first limit block 53 therebetween, so that the first limit block 53 can be inserted between the fourth push plate 854 and the positioning block 853 by roughly adjusting the positions of the multiple first limit blocks 53 on the hanging plate 51, and then the motor 82 only needs to be driven to enable the third push plate 84 to drive multiple groups of push-card components 85 to translate, so that the multiple fourth push plates 854 are used to elastically push the first limit block 53 to be inserted into the docking block 21 at the same time, thereby improving the stability and safety of the assembly of the hanging component 5.

[0099] In this embodiment, the lifting and positioning assembly 9 includes a second connecting plate 91, a second baffle 92, a third baffle 93, a second pneumatic rod 94 and a lifting plate 95. The second baffle 92 and the third baffle 93 are fixed on both sides of the second connecting plate 91, respectively. The second baffle 92 and the third baffle 93 are both fixed to the top surface of the bottom plate 6. The second pneumatic rod 94 is provided on the bottom surface of the second connecting plate 91. The telescopic top end of the second pneumatic rod 94 passes through the top of the second connecting plate 91. The telescopic top end of the second pneumatic rod 94 is connected to the lifting plate 95. The lifting plate 95 is arranged between the second baffle 92 and the third baffle 93.

[0100] By positioning the carbon fiber cross beam plate 2 between the second baffle plate 92 and the third baffle plate 93, after the heald frame is assembled, the assembled heald frame can be easily taken out by simply starting the second pneumatic rod 94 to push the lifting plate 95 upward.

[0101] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the sentence "comprise a ..." do not exclude the existence of other identical elements in the process, method, article or device including the elements.

[0102] The above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit the same. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that the technical solutions described in the aforementioned embodiments may still be modified, or some of the technical features may be replaced by equivalents. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A carbon fiber heald frame for a bottom-mounted high-speed air jet loom, characterized in that: It includes side guards and carbon fiber cross beam plates, wherein two side guards are mirror-imaged, a carbon fiber cross beam plate is arranged between the two side guards, two carbon fiber cross beam plates are mirror-imaged about the vertical center line of the side guards, one side of the side guard is connected with an angle joint component, one side of the angle joint component is plugged into the inside of the carbon fiber cross beam plate, two groups of angle joint components are mirror-imaged about the vertical center line of the side guards, the outer walls of the two carbon fiber cross beam plates are both provided with a transverse partition component, the two sides of the transverse partition component are respectively fixedly connected with the two groups of angle joint components, the two side guards and the two groups of transverse partition components are fixedly connected through the angle joint components to form a rectangular peripheral structure, the inner wall of the carbon fiber cross beam plate is fixed with a plurality of docking blocks, the carbon fiber cross beam plate is connected with a hanging component through a plurality of docking blocks, and one side of the hanging component is fixedly connected with the inner wall of the side guard; The corner joint assembly includes a sleeve block, which is fixed to the side wall of the side guard, one side of the carbon fiber cross beam plate is inserted into the sleeve block, a second inner plug-in block is fixed inside the sleeve block, a first docking groove and a second docking groove are provided through the carbon fiber cross beam plate, the second inner plug-in block is inserted into the second docking groove, the first inner plug-in blocks are fixed to the inner walls on both sides of the side guard, the first baffles are fixed on both sides of the first inner plug-in block, the first inner plug-in block is inserted into the first docking groove, and the first baffles are attached to the side wall of the carbon fiber cross beam plate; The corner joint assembly also includes a card top block, a first fixing plate, a second fixing plate, an inner top component and a reinforcement plate, the first fixing plate is fixed to the outer wall of the sleeve block, the second fixing plate is fixed to the side wall of the first fixing plate, the inner top component is penetrated inside the second fixing plate, a reinforcement plate is fixed to one side of the second fixing plate, a first slot is opened on the outer wall on one side of the side guard, the reinforcement plate is inserted into the first slot, a second slot of a T-shaped structure is opened between the sleeve block and the second inner plug-in block, openings on both sides of the second slot respectively penetrate through the two side walls of the second inner plug-in block, two card top blocks are mirrored inside the second slot, a pressure sensor is embedded in the side wall of the card top block, one side of the inner top component is inserted into the second slot, two card slots are opened on the inner wall of the second docking groove, the card top block is pushed out and extended through the inner top component to be inserted into the card slot, and one side of the pressure sensor is attached to the inner wall of the card slot.

2. The carbon fiber heald frame of the bottom-mounted high-speed air jet loom according to claim 1, characterized in that: The inner top component includes an adjusting bolt, a first spring, a first push plate and an inserting plate. The adjusting bolt is threadedly connected to the inside of the second fixed plate. The first spring is sleeved on the outer wall of the adjusting bolt. One end of the adjusting bolt is rotatably connected to the first push plate. The side wall of the first push plate is fixed with an inserting plate. The inserting plate is inserted into the inside of the second slot. The side of the inserting plate away from the first push plate is a V-shaped structure. The V-shaped structure of the inserting plate is used to push and separate the two top blocks. The adjacent sides of the two top blocks are provided with an inclined surface structure.

3. The carbon fiber heald frame of the bottom-mounted high-speed air jet loom according to claim 2, characterized in that: The partition assembly includes a heat conducting plate, a wear plate, a conduit, an axial connection block and a clamping plate. The heat conducting plate is fixed to the outer wall of the carbon fiber cross beam plate. A plurality of heat conducting plates are arranged at intervals. Wear plates are fixed on both sides of the heat conducting plate. The wear plates are fixed to the side walls of the carbon fiber cross beam plate. The conduit penetrates and connects to the interior of the plurality of heat conducting plates. The outer walls at both ends of the conduit are sleeved with axial connection blocks. A clamping plate with an inverted concave structure is fixed to the bottom surface of the axial connection block. The clamping plate is sleeved on the sleeve block and the outer wall of the side block. The outer wall of the side block is provided with a first protrusion, and one side of the clamping plate is fitted to the side wall of the first protrusion.

4. The carbon fiber heald frame of the bottom-mounted high-speed air jet loom according to claim 3, characterized in that: A heat dissipation groove is provided inside the heat conduction plate, a conduit is connected to the inside of the heat dissipation groove, a plurality of first air outlet holes are provided on the outer wall of the conduit close to the carbon fiber cross beam plate, and second air outlet holes are provided on the outer wall of the conduit that pass through from top to bottom, and the second air outlet holes are arranged inside the heat dissipation groove.

5. The carbon fiber heald frame of the bottom-mounted high-speed air jet loom according to claim 4, characterized in that: The hanging assembly includes a hanging plate, a corner block and a first limit block. The corner block is an L-shaped structure. Two corner blocks are mirrored. The two sides of the hanging plate are respectively inserted into the two corner blocks. One side of the corner block is right-angled to the inner wall of the carbon fiber beam plate, and the other side of the corner block is right-angled to the inner wall of the side block. The first limit block is slidably sleeved on the outer wall of the hanging plate. A second protrusion is set on one side of the first limit block. The second protrusion is translated and inserted into the docking block through the first limit block.

6. The method for processing a carbon fiber heald frame of a bottom-mounted high-speed air jet loom according to claim 5, characterized in that: The processing method comprises the following steps: S1, carbon fiber pre-assembled parts processing; The carbon fiber cloth and carbon fiber filaments are impregnated with glue, and the carbon fiber cross beam plate is formed by heating the mold, cut and punched according to the product length, a plurality of docking blocks are fixed on the carbon fiber cross beam plate, the heat conduction plate is bonded to the outer wall of the carbon fiber cross beam plate, the grinding plate is bonded to both sides of the heat conduction plate and the carbon fiber cross beam plate, and the conduit is inserted into the interior of the heat conduction plate to obtain the carbon fiber preassembled part; S2, side frame pre-assembled parts processing; Cut and drill the aluminum alloy side guard, weld two sets of blocks to both sides of the side guard, grind and remove burrs, and obtain the side frame pre-assembled parts; S3, positioning pre-assembly; Positioning and placing two sets of carbon fiber pre-assembled parts on the assembly equipment, placing two sets of side frame pre-assembled parts and two sets of hanging components on the assembly equipment at the same time, starting the assembly equipment to simultaneously assemble the two sets of side frame pre-assembled parts and the two sets of hanging components and dock with the two sets of carbon fiber pre-assembled parts, and initially forming a frame structure; The assembly equipment includes a bottom plate, a pushing component, a pushing component and a lifting and positioning component. The top surface of the bottom plate is provided with four groups of lifting and positioning components in a rectangular distribution. A pushing component is provided on the top surface of one side of the bottom plate. Two groups of pushing components are provided with a mirror image of the vertical center line of the bottom plate. A pushing component is connected between the two groups of pushing components. Two groups of pushing components are provided with a mirror image of the vertical center line of the pushing component. The lifting and positioning component is used to position and clamp the carbon fiber pre-assembled parts. The pushing component is used to position and assemble the side frame pre-assembled parts. The pushing component is pushed horizontally by the pushing component to clamp the hanging component. S4, corner mounting and fixing; Assemble the complete corner joint assembly and the cross partition assembly, and fix the hanging assembly between the carbon fiber cross beam plate and the side guard.

7. The method for processing a carbon fiber heald frame of a bottom-mounted high-speed air jet loom according to claim 6, characterized in that: The pushing assembly includes a support seat, a first pneumatic rod, a second push plate, a tooth plate and a pushing and rotating component. The support seat is fixed to the top surface of the base plate, a slide groove is arranged on the top surface of the support seat, a first pneumatic rod is arranged on the side wall of the support seat, the telescopic end of the first pneumatic rod is connected to the inside of the slide groove, the telescopic end of the first pneumatic rod is connected to the second push plate, the second push plate is used to push the translational assembly of the side frame pre-assembled parts, the top of the second push plate slides and fits against the top surface of the support seat, the first connecting plates are fixed on both sides of the second push plate, the side walls of the first connecting plates are connected to the tooth plate, the tooth plate is slidably connected to the inside of the support seat, the side walls of the support seat are provided with a pushing and rotating component, two groups of pushing and rotating components are arranged in a mirror image about the vertical center line of the support seat, one side of the pushing and rotating component is connected to the pushing assembly, one side of the tooth plate is connected to the inside of the pushing and rotating component, and the pushing and rotating component is pushed by the tooth plate to translate the pushing assembly.

8. The method for processing a carbon fiber heald frame of a bottom-mounted high-speed air jet loom according to claim 7, characterized in that: The pushing and turning component includes a bracket, a first gear, a bracket seat, a push block and a screw rod. The bracket is fixed to the side wall of the support seat, and a screw rod is rotatably connected inside the bracket. The outer wall of one end of the screw rod is sleeved with the first gear, and the top of the first gear is meshingly connected with the bottom surface of the toothed plate. The outer wall of the screw rod is threadedly sleeved with a push block, and one side of the push block is slidably fitted with the side wall of the support seat. A bracket seat is fixed to the top surface of the push block, and a groove structure is provided on the top surface of the bracket seat to cooperate with the insertion of the corner block.

9. The method for processing a carbon fiber heald frame of a bottom-mounted high-speed air jet loom according to claim 8, characterized in that: The push assembly includes a first support plate, a motor, a second gear, a third push plate and a push card component, the first support plate is fixed to the side wall of the push block, a plurality of second limit blocks are fixed to the top surface of the first support plate, the third push plate is connected through the plurality of second limit blocks, a motor is arranged on the top surface of the first support plate, a second gear is connected to the rotating end of the motor, the bottom of the second gear is meshedly connected to the top surface of one side of the third push plate, a plurality of groups of push card components are arranged on the top surface of the third push plate, and the push card components are used to push the first limit block horizontally to be inserted into the docking block; The pushing card component includes a fixed block, a second support plate, a positioning block, a fourth push plate, a guide rod, a second spring and a third limit block. The fixed block is fixed to the top surface of the third push plate, the second support plate is fixed on the top surface of the fixed block, the positioning block is fixed on the top surface of one side of the second support plate, the third limit block is fixed on the top surface of the other side of the second support plate, a guide rod is inserted into the inside of the third limit block, the second spring is sleeved on the outer wall of the guide rod, the fourth push plate is connected to one end of the guide rod close to the positioning block, and the distance between the fourth push plate and the positioning block is greater than the width of the first limit block.

10. The method for processing a carbon fiber heald frame of a bottom-mounted high-speed air jet loom according to claim 6, characterized in that: The lifting and positioning assembly includes a second connecting plate, a second baffle, a third baffle, a second pneumatic rod and a lifting plate. The second baffle and the third baffle are respectively fixed on both sides of the second connecting plate. The second baffle and the third baffle are both fixed to the top surface of the bottom plate. The second pneumatic rod is arranged on the bottom surface of the second connecting plate. The telescopic top end of the second pneumatic rod passes through the top of the second connecting plate. The telescopic top end of the second pneumatic rod is connected with the lifting plate. The lifting plate is fitted between the second baffle and the third baffle.

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