CN115674053A - Compound frock of aeronautical material processing - Google Patents
Compound frock of aeronautical material processing Download PDFInfo
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- CN115674053A CN115674053A CN202211462369.5A CN202211462369A CN115674053A CN 115674053 A CN115674053 A CN 115674053A CN 202211462369 A CN202211462369 A CN 202211462369A CN 115674053 A CN115674053 A CN 115674053A
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Abstract
The invention discloses an aviation material processing composite tool, which belongs to the technical field of processing tools and comprises a workbench, wherein a positioning assembly is arranged at the center of the top of the workbench, a linkage assembly is connected to one side of the positioning assembly in a transmission manner, a cleaning assembly is fixedly connected to one side of the workbench, a first sliding groove is formed in the top of the workbench, a reciprocating lead screw is rotationally connected to the first sliding groove, and a first lead screw seat is in threaded connection with the outer surface of the reciprocating lead screw. According to the aviation material processing device, the positioning assembly and the linkage assembly are arranged, the two second screw rod seats drive the clamping blocks to be close to each other and clamp and limit aviation materials, so that the positioning assembly can be suitable for aviation materials with different lengths and specifications for limiting, the applicability of the positioning assembly is improved, the processing device can meet the processing requirements of aviation materials with different specifications, the linkage screw rod is rotated, the aviation materials are axially processed, and the processing effect is improved.
Description
Technical Field
The invention belongs to the technical field of machining tools, and particularly relates to a composite tool for machining an aviation material.
Background
With the continuous improvement of science and technology, the research field is continuously expanded, and the tourism in the universe is one of the greatest dreams of human beings since ancient times, at present, human beings have greatly improved in the aerospace field, and are not dreams when entering the universe, the spaceship realizes the dreams, the selection of materials is particularly important in the manufacturing of the spaceship, and composite tools are generally used for processing the aerospace materials in the processing process of the aerospace materials.
However, in the actual processing process, the adjustable angle range of the composite tool is small in the using process, the material processing process has certain angle limitation, part of aviation materials need to be processed in the axial direction, and the existing composite tool is difficult to meet.
Disclosure of Invention
The invention aims to: the composite tool for machining the aviation materials is provided for solving the problem that the composite tool is difficult to axially machine part of aviation materials.
In order to achieve the purpose, the invention adopts the following technical scheme:
the aviation material processing composite tool comprises a workbench, wherein a positioning assembly is arranged at the center of the top of the workbench, a linkage assembly is in transmission connection with one side of the positioning assembly, a cleaning assembly is fixedly connected with one side of the workbench, a first chute is formed in the top of the workbench, a reciprocating lead screw is rotationally connected in the first chute, a first lead screw seat is in threaded connection with the outer surface of the reciprocating lead screw, the first lead screw seat is in sliding connection with the first chute, an installation assembly is fixedly connected to the top of the first lead screw seat, a protection plate is fixedly connected to one side of the top of the workbench, a motor is fixedly installed on one side of the workbench through an installation plate, and one end of an output shaft of the motor is fixedly connected with one end of the reciprocating lead screw through a rotating shaft;
locating component includes the dwang, the second spout has been seted up at the workstation top, second spout inner wall both sides all inlay and are equipped with the bearing, the equal fixedly connected with pivot in dwang both ends, and the pivot rotates to be connected in the bearing, dwang surface sliding connection has two spliced poles, spliced pole sliding connection is in the second spout, two the equal fixedly connected with third lead screw seat in spliced pole bottom, and the inside equal threaded connection of two third lead screw seats has the removal lead screw, and two remove fixed connection between the lead screw, and two remove lead screw one end and rotate with second spout inner wall one side and be connected, the one end that third lead screw seat was kept away from to the spliced pole is rotated through first connecting axle and is connected with the connection pad, the third spout has been seted up to connection pad one side, the third spout is connected with two adjustment lead screws, and fixed connection between two adjustment lead screws, adjustment lead screw surface threaded connection has the second lead screw seat, second lead screw seat sliding connection is in the third spout, second lead screw seat one end fixedly connected with grip block.
As a further description of the above technical solution:
the spliced pole is inside to have seted up the second cavity, fixedly connected with mounting bracket in the second cavity, the embedded bearing that is equipped with of mounting bracket, and the bearing internal rotation is connected with the connection pivot, connection pivot one end fixedly connected with third bevel gear, third bevel gear bottom meshing has fourth bevel gear, the inside joint of fourth bevel gear has the sleeve, the sleeve dwang cup joints mutually, the one end fixedly connected with second bevel gear of third bevel gear is kept away from in the connection pivot, second bevel gear top one side meshing has first bevel gear, first bevel gear and first connecting axle surface looks joint.
As a further description of the above technical solution:
the two adjusting screw rods and the moving screw rods are symmetrically distributed along the central position, and the thread directions of the two adjusting screw rods and the moving screw rods are opposite.
As a further description of the above technical solution:
first cavity has been seted up to workstation one side, be connected with drive gear through the pivot in the first cavity, and pivot one end and dwang fixed connection, the spacing rack of drive gear top meshing, spacing rack top threaded connection has elevating screw, elevating screw one end extends to first cavity outside and fixedly connected with knob through the pivot.
As a further description of the above technical solution:
the linkage assembly comprises a mounting plate, the bottom of the mounting plate is connected with a linkage screw rod through a rotating shaft in a rotating mode, the outer surface of the linkage screw rod is in threaded connection with a fourth screw rod seat, one side of the fourth screw rod seat is attached to one side of the workbench, a connecting piece is fixedly connected to the bottom of the fourth screw rod seat, and a second gear is connected to the connecting piece in a rotating mode.
As a further description of the above technical solution:
one side of the second gear is meshed with a first gear, one side of the first gear is fixedly connected with the transmission gear through a rotating shaft, one side of the second gear, far away from the first gear, is meshed with a third gear, and one side of the third gear is fixedly connected with one end of a reciprocating screw rod through a rotating shaft.
As a further description of the above technical solution:
clean the subassembly and include the connecting box, connecting box one side and workstation one side fixed connection, connecting box inner wall both sides all inlay and are equipped with the bearing, and rotate between two bearings and be connected with the second connecting axle, second connecting axle surface joint has the cam, the laminating of cam one side has the stripper plate, a plurality of gasbags of one side fixedly connected with of cam are kept away from to the stripper plate, one side and connecting box inner wall one side fixed connection that the stripper plate was kept away from to the gasbag, gasbag one end fixedly connected with connecting pipe, the connecting pipe runs through the connecting box and inlays to locate in the guard plate, connecting pipe other end fixedly connected with one-way air outlet valve.
As a further description of the above technical solution:
the utility model discloses a spring, including stripper plate, connecting box inner wall, telescopic link, spring both ends respectively with stripper plate one side and connecting box inner wall one side fixed connection, a plurality of telescopic links of equal fixedly connected with in stripper plate both sides, connecting box inner wall one side fixed connection is kept away from to the telescopic link, telescopic link surface cover is equipped with the spring, the spring both ends respectively with stripper plate one side and connecting box inner wall one side fixed connection.
As a further description of the above technical solution:
second connecting axle one end extends to the connecting box outside and fixedly connected with from the driving wheel, motor output shaft one end is through pivot fixedly connected with action wheel, the transmission is connected with the drive belt between action wheel and the driven.
As a further description of the above technical solution:
the mounting assembly comprises a connecting block, a groove is formed in the top of the connecting block, a transmission lead screw is connected in the groove in a rotating mode, a transmission lead screw seat is connected to the outer surface of the transmission lead screw in a threaded mode, the transmission lead screw is fixedly connected with an assembling plate at the top, and a plurality of assembling holes are formed in the top of the assembling plate.
In summary, due to the adoption of the technical scheme, the invention has the beneficial effects that:
1. according to the invention, by arranging the positioning assembly and the linkage assembly, the movable screw rod moves through the third screw rod to drive the two connecting columns to be close to each other, the connecting columns drive the connecting discs to be close to each other, when the clutch is in due time, a worker rotates the adjusting screw rod, the adjusting screw rod drives the second screw rod seats to move in the third chute, the two second screw rod seats drive the clamping blocks to be close to each other and clamp and limit the aviation materials, so that the positioning assembly can be suitable for aviation materials with different lengths and different specifications to limit, the applicability of the positioning assembly is improved, the processing device can meet the processing requirements of aviation materials with different specifications, the linkage screw rod drives the fourth screw rod seat to move in the vertical direction by rotating the linkage screw rod, the second gear, the first gear and the third gear are controlled to be meshed with and separated from each other, the rotation of the connecting discs can be controlled by a series of transmission, the axial processing of the aviation materials is realized, and the processing effect is improved.
2. According to the invention, the cleaning assembly is arranged, the driving wheel drives the driven wheel to rotate, the driven wheel drives the cam to rotate through the second connecting shaft, the cam is matched with the spring to drive the extrusion plate to do reciprocating motion, the extrusion plate drives the air bag to contract and expand in a reciprocating mode, so that air in the air bag is discharged through the connecting pipe and the one-way air outlet valve and sweeps impurities generated in processing, the workbench can be cleaned, the cleanness of the workbench is ensured, the impurities are prevented from blocking the operation of the processing tool, and the smoothness of the operation of the processing tool is improved.
3. According to the aviation material processing device, the installation assembly is arranged, so that a worker can fixedly install the processing tool and the assembly plate, then the distance between the processing tool and the aviation material is adjusted according to the processing requirement, the aviation material is conveniently processed, on one hand, the worker can conveniently replace different processing tools, the flexibility of aviation material processing is improved, on the other hand, the distance between the assembly plate and the material is adjusted by rotating the transmission lead screw, therefore, different processing requirements are met, and the applicability of aviation material processing is improved.
Drawings
Fig. 1 is a schematic perspective structure view of an aerospace material processing composite tool provided by the invention;
fig. 2 is an enlarged structural schematic diagram of a part a of the composite tooling for processing the aircraft material, provided by the invention;
fig. 3 is a schematic front sectional structure view of an aircraft material processing composite tool provided by the invention;
fig. 4 is an enlarged structural schematic diagram of a part B of the composite tooling for processing the aviation material, which is provided by the invention;
FIG. 5 is an enlarged schematic structural view of a part C of the composite tooling for processing the aviation material, which is provided by the invention;
FIG. 6 is a schematic side view of a cross-sectional structure of an aircraft material processing composite tool according to the present invention;
fig. 7 is an enlarged structural schematic diagram of a part D of the composite tooling for machining an aircraft material according to the present invention. Illustration of the drawings: 1. a work table; 2. mounting the component; 201. connecting blocks; 202. a drive screw base; 203. assembling a plate; 204. a drive screw; 205. a groove; 206. an assembly hole; 3. a positioning assembly; 301. connecting columns; 302. connecting the rotating shaft; 303. a mounting frame; 304. a second chute; 305. a second lead screw base 306 and a connecting disc; 307. a first bevel gear; 308. a first connecting shaft; 309. a second bevel gear; 310. a third chute; 311. adjusting a lead screw; 312. a clamping block; 313. a third bevel gear; 314. rotating the rod; 315. a knob; 316. lifting a screw rod; 317. a limit rack; 318. a transmission gear; 319. a first cavity; 320. moving the lead screw; 321. a third lead screw seat; 322. a fourth bevel gear; 323. a sleeve; 324. a second cavity; 4. a protection plate; 5. a sweeping assembly; 501. a driving wheel; 502. a transmission belt; 503. a connecting box; 504. a driven wheel; 505. a one-way air outlet valve; 506. a connecting pipe; 507. a second connecting shaft; 508. a cam; 509. a compression plate; 510. an air bag; 511. a spring; 512. a telescopic rod; 6. a first lead screw base; 7. a reciprocating screw; 8. a first chute; 9. a linkage assembly; 901. a first gear; 902. a connecting member; 903. a second gear; 904. a third gear; 905. a fourth screw base; 906. a linkage lead screw; 907. mounting a plate; 10. an electric motor.
Detailed Description
Referring to fig. 1-7, the present invention provides a technical solution:
the utility model provides a compound frock of aeronautical material processing, including workstation 1, 1 top central point of workstation puts and is provided with locating component 3, the transmission of 3 one sides of locating component is connected with linkage subassembly 9, 1 one side fixedly connected with of workstation cleans subassembly 5, first spout 8 has been seted up at 1 top of workstation, 8 internal rotations of first spout are connected with reciprocal lead screw 7, 7 surface threaded connection of reciprocal lead screw have first lead screw seat 6, 6 sliding connection of first lead screw seat in first spout 8, 6 top fixedly connected with installation component 2 of first lead screw seat, 1 top one side fixedly connected with guard plate 4 of workstation, 1 one side of workstation has motor 10 through mounting panel fixed mounting, motor 10 output shaft one end is through pivot and 7 one end fixed connection of reciprocal lead screw.
The mounting assembly 2 comprises a connecting block 201, a groove 205 is formed in the top of the connecting block 201, a transmission lead screw 204 is connected to the inner side of the groove 205 in a rotating mode, a transmission lead screw seat 202 is connected to the outer surface of the transmission lead screw 204 in a threaded mode, the transmission lead screw 204 is fixedly connected with an assembling plate 203 on the top portion, and a plurality of assembling holes 206 are formed in the top portion of the assembling plate 203
The implementation mode specifically comprises the following steps: through setting up installation component 2, the staff carries out fixed mounting with machining tool and assembly plate 203, later, requires to adjust machining tool and aviation material distance according to the processing, and the convenience is to the processing of aviation material, and on the one hand, makes things convenient for the staff to the change of different machining tools, has improved the flexibility to aviation material processing.
The positioning component 3 comprises a rotating rod 314, a second chute 304 is arranged at the top of the workbench 1, bearings are embedded at two sides of the inner wall of the second chute 304, rotating shafts are fixedly connected at two ends of the rotating rod 314 and are rotatably connected in the bearings, two connecting columns 301 are slidably connected on the outer surface of the rotating rod 314, the connecting columns 301 are slidably connected in the second chute 304, third screw bases 321 are fixedly connected at the bottoms of the two connecting columns 301, a movable screw 320 is respectively and internally and spirally connected in the two third screw bases 321, two movable screws 320 are fixedly connected between the two movable screws, one end of each movable screw 320 is rotatably connected with one side of the inner wall of the second chute 304, one end of each connecting column 301 far away from the third screw base 321 is rotatably connected with a connecting disk 306 through a first connecting shaft 308, a third chute 310 is arranged at one side of the connecting disk 306, two adjusting screws 311 are rotatably connected in the third chute 310, two adjusting screws are fixedly connected between the two adjusting screws 311, a second screw base 305 is rotatably connected on the outer surface of the adjusting screws 311, the second screw base 305 is slidably connected in the third chute 310, one end of the second screw base 305 is fixedly connected with a clamping block 312, a second bevel gear holder 309, a third bevel gear 302 is fixedly connected in the top of the rotating shaft, a fourth bevel gear 302, a fourth bevel gear clamp connected with a third bevel gear 313 fixedly connected in the top of a third bevel gear holder 313, a fourth bevel gear clamp connected with a third bevel gear 302, a third bevel gear clamp connected in the top of a third bevel gear clamp connected in the bearing 313, a third bevel gear clamp connected with a fourth bevel gear 313, two adjustment lead screws 311 and removal lead screw 320 all are the symmetric distribution along central point, and two adjustment lead screws 311 and the opposite direction of removal lead screw 320 screw thread, first cavity 319 has been seted up to workstation 1 one side, be connected with drive gear 318 through the pivot in the first cavity 319, and pivot one end and dwang 314 fixed connection, drive gear 318 top meshing limit rack 317, limit rack 317 top threaded connection has lifting screw 316, lifting screw 316 one end extends to first cavity 319 outside and fixedly connected with knob 315 through the pivot.
The implementation mode is specifically as follows: through setting up locating component 3 and linkage subassembly 9, it removes through third lead screw seat 321 to remove lead screw 320, drive two spliced poles 301 and be close to each other, spliced pole 301 drives connection pad 306 and is close to each other, it is in good time apart from the separation and reunion, the staff rotates adjustment lead screw 311, adjustment lead screw 311 drives second lead screw seat 305 and removes in third spout 310, two second lead screw seats 305 drive grip block 312 and are close to each other and carry out the centre gripping to the aeronautical material and prescribe a limit to, thereby make locating component 3 can be applicable to different length, aeronautical material of different specifications carries on spacingly, locating component 3's suitability has been improved, through rotating linkage lead screw 906, linkage lead screw 906 drives fourth lead screw seat 905 and removes in vertical direction, control second gear 903 and first gear 901 and third gear 904 intermeshing and separation, and can control connection pad 306's rotation through a series of transmissions.
Cleaning assembly 5 includes connecting box 503, connecting box 503 one side and workstation 1 one side fixed connection, the bearing has all been inlayed to connecting box 503 inner wall both sides, and rotate between two bearings and be connected with second connecting axle 507, second connecting axle 507 outer surface joint has cam 508, cam 508 one side laminating has stripper plate 509, stripper plate 509 keeps away from a plurality of gasbags 510 of one side fixedly connected with of cam 508, one side and connecting box 503 inner wall one side fixed connection that stripper plate 509 was kept away from to gasbag 510, gasbag 510 one end fixedly connected with connecting pipe 506, connecting pipe 506 runs through connecting box 503 and inlays and locates in guard plate 4, connecting pipe 506 other end fixedly connected with one-way air outlet valve 505, a plurality of telescopic links 512 of the equal fixedly connected with in stripper plate 509 both sides, telescopic link 512 keeps away from connecting box 503 inner wall one side fixed connection, telescopic link 512 outer surface cover is equipped with spring 511, the spring 511 both ends respectively with stripper plate 509 one side and connecting box 503 inner wall one side fixed connection, second 507 one end extends to connecting box 503 outside and fixedly connected with driven wheel 504, motor 10 output shaft fixedly connected with action wheel 501 through pivot, transmission belt 502 between action wheel 501 and the driven wheel.
The implementation mode is specifically as follows: through setting up and cleaning subassembly 5, action wheel 501 drives from driving wheel 504 and rotates, from driving wheel 504 drives cam 508 through second connecting axle 507 and rotates, cam 508 cooperation spring 511 drives stripper plate 509 and is reciprocating motion, stripper plate 509 drives gasbag 510 reciprocal contraction and expansion, make the air in the gasbag 510 discharge and sweep the impurity that produces in the processing through connecting pipe 506 and one-way air outlet valve 505, can clean workstation 1, guaranteed the clean and tidy of workstation 1.
The working principle is as follows: during the use, the staff rotates removal lead screw 320, remove lead screw 320 and drive the third lead screw and slide in second spout 304, third lead screw seat 321 drives two spliced poles 301 and is close to each other, spliced pole 301 drives connection pad 306 and is close to each other, when the separation and reunion is in good time, the staff rotates adjustment lead screw 311, adjustment lead screw 311 drives second lead screw seat 305 and removes in third spout 310, two second lead screw seats 305 drive grip block 312 and are close to each other and carry out the centre gripping to aeronautical materials and prescribe a limit.
Accomplish the centre gripping to the aeronautical material spacing back, the staff carries out fixed mounting with machining tool (like spray gun or processing cutter etc.) and assembly plate 203, later, adjusts machining tool and aeronautical material distance according to the processing requirement, and the convenience is to the processing of aeronautical material.
After the installation of the machining tool is completed, the worker rotates the lifting screw 316, the lifting screw 316 drives the limiting rack 317 to move upwards, the limiting rack 317 relieves the limitation on the transmission gear 318, meanwhile, the worker rotates the linkage screw 906, the linkage screw 906 drives the fourth screw seat 905 to move downwards, so that the second gear 903 is meshed with the first gear 901 and the third gear 904, at the moment, the worker starts the motor 10, the motor 10 drives the reciprocating screw 7 to rotate, the reciprocating screw 7 drives the first screw seat 6 to reciprocate in the first chute 8, the first screw seat 6 drives the connecting block 201 to reciprocate, the connecting block 201 drives the machining tool to machine the aviation material through the assembling plate 203, at the moment, the third gear drives the second gear 903 to rotate, the second gear 903 drives the first gear 901 to rotate, the first gear 901 drives the rotating rod 314 to rotate, the rotating rod 314 drives the sleeve 323 to rotate, the sleeve 323 drives the fourth bevel gear 322 to rotate, the fourth bevel gear 322 drives the third bevel gear 313 to drive the connecting rotating shaft 302 to rotate, the connecting rotating shaft 302 drives the second bevel gear 309 to rotate, the second bevel gear 309 drives the first bevel gear 307 to rotate, the first bevel gear 307 drives the first connecting shaft 308 to rotate, the first connecting shaft 308 drives the aviation material to rotate through the connecting disc 306, so that the machining tool performs axial machining on the aviation material, when axial machining is not needed, the linkage screw 906 is rotated to enable the second gear 903 to release the meshing state of the first gear 901 and the third gear 904, meanwhile, the lifting screw 316 is rotated to enable the limiting rack 317 to limit the transmission gear 318, and the position of the rotating disc is fixed.
Meanwhile, the motor 10 drives the driving wheel 501 to rotate, the driving wheel 501 drives the driven wheel 504 to rotate through the transmission belt 502, the driven wheel 504 drives the second connecting shaft 507 to rotate, the second connecting shaft 507 drives the cam 508 to rotate, the cam 508 drives the extrusion plate 509 to move, meanwhile, the telescopic rod 512 and the spring 511 drive the extrusion plate 509 to perform reset motion, the cam 508 drives the extrusion plate 509 to perform reciprocating motion by matching with the spring 511, the extrusion plate 509 drives the air bag 510 to perform reciprocating contraction and relaxation, so that air in the air bag 510 is discharged through the connecting pipe 506 and the one-way air outlet valve 505 and sweeps impurities generated in processing.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (10)
1. The composite tooling for processing the aviation materials comprises a workbench (1) and is characterized in that a positioning component (3) is arranged at the center of the top of the workbench (1), a linkage component (9) is in transmission connection with one side of the positioning component (3), a cleaning component (5) is fixedly connected with one side of the workbench (1), a first sliding chute (8) is formed in the top of the workbench (1), a reciprocating lead screw (7) is rotationally connected with the first sliding chute (8), a first lead screw seat (6) is in threaded connection with the outer surface of the reciprocating lead screw (7), the first lead screw seat (6) is in sliding connection with the first sliding chute (8), an installation component (2) is fixedly connected with the top of the first lead screw seat (6), a protection plate (4) is fixedly connected with one side of the top of the workbench (1), a motor (10) is fixedly installed on one side of the workbench (1) through an installation plate, and one end of an output shaft of the motor (10) is fixedly connected with one end of the reciprocating lead screw (7) through a rotating shaft;
the positioning component (3) comprises a rotating rod (314), a second sliding groove (304) is formed in the top of the workbench (1), bearings are embedded in two sides of the inner wall of the second sliding groove (304), rotating shafts are fixedly connected to two ends of the rotating rod (314) and rotatably connected to the bearings, two connecting columns (301) are slidably connected to the outer surface of the rotating rod (314), the two connecting columns (301) are slidably connected to the second sliding groove (304) in two ways, a third screw seat (321) is fixedly connected to the bottom of each connecting column (301), a connecting disc (306) is rotatably connected to the inner wall of the second sliding groove (304) through a first connecting shaft (308), a third sliding groove (310) is formed in one side of the connecting disc (306), two adjusting screws (311) are rotatably connected to the third sliding groove (310), two adjusting screws (311) are rotatably connected to the connecting disc (306) through two adjusting screws (308), the outer surface of each adjusting screw seat (305) is rotatably connected to the second screw seat (311), and the outer surface of each second screw seat (311) is rotatably connected to the second sliding groove (310), one end of the second lead screw seat (305) is fixedly connected with a clamping block (312).
2. The composite tooling for processing the aviation materials as claimed in claim 1, wherein a second cavity (324) is formed inside the connecting column (301), a mounting frame (303) is fixedly connected inside the second cavity (324), a bearing is embedded in the mounting frame (303), a connecting rotating shaft (302) is rotationally connected in the bearing, a third bevel gear (313) is fixedly connected to one end of the connecting rotating shaft (302), a fourth bevel gear (322) is meshed at the bottom of the third bevel gear (313), a sleeve (323) is clamped inside the fourth bevel gear (322), a rotating rod (314) of the sleeve (323) is sleeved, a second bevel gear (309) is fixedly connected to one end, far away from the third bevel gear (313), of the connecting rotating shaft (302), a first bevel gear (307) is meshed on one side of the top of the second bevel gear (309), and the first bevel gear (307) is clamped to the outer surface of the first connecting shaft (308).
3. The composite tooling for machining the aeronautical material according to claim 1, wherein the two adjusting lead screws (311) and the two moving lead screws (320) are symmetrically distributed along the center position, and the thread directions of the two adjusting lead screws (311) and the two moving lead screws (320) are opposite.
4. The composite tooling for processing the aviation material according to claim 1, wherein a first cavity (319) is formed in one side of the workbench (1), a transmission gear (318) is connected into the first cavity (319) through a rotating shaft, one end of the rotating shaft is fixedly connected with the rotating rod (314), the top of the transmission gear (318) is meshed with a limit rack (317), the top of the limit rack (317) is in threaded connection with a lifting screw rod (316), and one end of the lifting screw rod (316) extends to the outside of the first cavity (319) through the rotating shaft and is fixedly connected with a knob (315).
5. The composite tooling for processing the aviation materials according to claim 1, wherein the linkage assembly (9) comprises a mounting plate (907), the bottom of the mounting plate (907) is rotatably connected with a linkage lead screw (906) through a rotating shaft, a fourth lead screw seat (905) is in threaded connection with the outer surface of the linkage lead screw (906), one side of the fourth lead screw seat (905) is attached to one side of the workbench (1), a connecting piece (902) is fixedly connected to the bottom of the fourth lead screw seat (905), and a second gear (903) is rotatably connected to the connecting piece (902).
6. The composite tooling for processing the aviation materials as claimed in claim 5, wherein a first gear (901) is meshed with one side of the second gear (903), one side of the first gear (901) is fixedly connected with the transmission gear (318) through a rotating shaft, a third gear (904) is meshed with one side, far away from the first gear (901), of the second gear (903), and one side of the third gear (904) is fixedly connected with one end of the reciprocating screw rod (7) through a rotating shaft.
7. The composite tooling for processing the aviation materials is characterized in that the cleaning assembly (5) comprises a connecting box (503), one side of the connecting box (503) is fixedly connected with one side of the workbench (1), bearings are embedded in two sides of the inner wall of the connecting box (503), a second connecting shaft (507) is rotatably connected between the two bearings, a cam (508) is clamped on the outer surface of the second connecting shaft (507), an extrusion plate (509) is attached to one side of the cam (508), a plurality of air bags (510) are fixedly connected to one side of the extrusion plate (509) far away from the cam (508), one side of the air bags (510) far away from the extrusion plate (509) is fixedly connected to one side of the inner wall of the connecting box (503), one end of each air bag (510) is fixedly connected with the connecting pipe (506), the connecting pipe (506) penetrates through the connecting box (503) and is embedded in the protection plate (4), and one-way air outlet valves (505) are fixedly connected to the other end of the connecting pipe (506).
8. The composite tooling for processing the aviation materials as claimed in claim 7, wherein a plurality of telescopic rods (512) are fixedly connected to both sides of the extrusion plate (509), one side of the telescopic rods (512) far away from the inner wall of the connecting box (503) is fixedly connected, a spring (511) is sleeved on the outer surface of each telescopic rod (512), and both ends of the spring (511) are respectively fixedly connected to one side of the extrusion plate (509) and one side of the inner wall of the connecting box (503).
9. The composite tooling for processing the aviation materials as claimed in claim 7, wherein one end of the second connecting shaft (507) extends to the outside of the connecting box (503) and is fixedly connected with a driven wheel (504), one end of an output shaft of the motor (10) is fixedly connected with a driving wheel (501) through a rotating shaft, and a transmission belt (502) is connected between the driving wheel (501) and the driven wheel in a transmission manner.
10. The composite tooling for machining the aviation material according to claim 9, wherein the mounting assembly (2) comprises a connecting block (201), a groove (205) is formed in the top of the connecting block (201), a transmission lead screw (204) is rotationally connected in the groove (205), a transmission lead screw seat (202) is in threaded connection with the outer surface of the transmission lead screw (204), the transmission lead screw (204) is fixedly connected with an assembly plate (203) at the top, and a plurality of assembly holes (206) are formed in the top of the assembly plate (203).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211462369.5A CN115674053A (en) | 2022-11-22 | 2022-11-22 | Compound frock of aeronautical material processing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211462369.5A CN115674053A (en) | 2022-11-22 | 2022-11-22 | Compound frock of aeronautical material processing |
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| Publication Number | Publication Date |
|---|---|
| CN115674053A true CN115674053A (en) | 2023-02-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202211462369.5A Withdrawn CN115674053A (en) | 2022-11-22 | 2022-11-22 | Compound frock of aeronautical material processing |
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| CN (1) | CN115674053A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116499337A (en) * | 2023-06-28 | 2023-07-28 | 西安航锦机械制造有限责任公司 | Frock is used in measurement of aviation auxiliary material product |
| CN117047587A (en) * | 2023-10-12 | 2023-11-14 | 四川英创力电子科技股份有限公司 | Six-axis forming machine for circuit board processing and using method thereof |
-
2022
- 2022-11-22 CN CN202211462369.5A patent/CN115674053A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116499337A (en) * | 2023-06-28 | 2023-07-28 | 西安航锦机械制造有限责任公司 | Frock is used in measurement of aviation auxiliary material product |
| CN116499337B (en) * | 2023-06-28 | 2023-09-08 | 西安航锦机械制造有限责任公司 | Frock is used in measurement of aviation auxiliary material product |
| CN117047587A (en) * | 2023-10-12 | 2023-11-14 | 四川英创力电子科技股份有限公司 | Six-axis forming machine for circuit board processing and using method thereof |
| CN117047587B (en) * | 2023-10-12 | 2023-12-19 | 四川英创力电子科技股份有限公司 | Six-axis forming machine for circuit board processing and using method thereof |
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Application publication date: 20230203 |