Edge turning inner supporting tool for aerospace cylinder section product

By rotating the hand-wheel drive screw, the inner support plate supports the cylinder section product outward, solving the problem of insufficient power supply of electric telescopic rods in the prior art, and achieving the effect of powerless operation and adaptability enhancement.

CN222856752UActive Publication Date: 2025-05-13TIANJIN ZECHUAN IND & TRADE CO LTD
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Patent Information

Application Number
CN202421724931.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-07-22
Publication Date
2025-05-13
Estimated Expiration
2034-07-22

AI Technical Summary

Technical Problem

When the vehicle edge inner support tooling of existing aerospace tube section products is installed at the edge of the processing tube section, the electric telescopic rod is insufficient for power supply, resulting in discontinuous internal support and poor adaptability.

Method used

The handwheel drive screw in the front of the support cylinder rotates, so that the inner support frame moves, and the inner support plate on the upper part of the suspension seat supports the cylinder section product outward without power operation, thereby increasing equipment adaptability.

Benefits of technology

It realizes internal support of the cylinder section product without power, increases the adaptability of the equipment, and reduces the area occupied by the center part through handwheel disassembly, making it easier to process the edge.

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Abstract

An aerospace cylinder section product edge turning inner supporting tool comprises an equipment base, a guide rod, a supporting frame, a supporting cylinder, an inner supporting seat and a suspension seat, the side portion of the equipment base is provided with a lead screw shaft groove, the lead screw shaft groove is matched with a lead screw, the lead screw shaft groove is connected with the lead screw, the lead screw rotates in the lead screw shaft groove, and the front portion of the equipment base is fixedly connected with a lead screw motor. The lower portion of the machining table is fixedly connected with the threaded seat, the threaded seat is in threaded connection with the interior of the lead screw, the upper portion of the machining table is fixedly connected with the edging machining assembly, the rear portion of the equipment base is fixedly connected with the equipment vertical table, the front portion of the equipment vertical table is provided with an auxiliary frame, and the lower portion of the auxiliary frame is fixedly connected with the equipment base. The side portion of the equipment vertical table is fixedly connected with a guide rod, the interior of the equipment vertical table is fixedly connected with a lifting air cylinder, and the guide rod adapts to the supporting frame.
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Description

Technical Field

[0001] The utility model relates to the field of aviation, in particular to an inner support tool for the side of an aerospace cylinder segment product. Background Art

[0002] An existing patent (publication number: CN112112446A) proposes a tooling for internal support of aerospace tube segment products. The device comprises a support having a reserved slot defined in the middle of the support's inner cavity, a positioner fixedly connected to the top of the reserved slot, and a 4G communication module fixedly connected to the bottom of the reserved slot. The left end of the support's top is movably connected to a first electric telescopic rod via a rotating shaft. However, this device, which "movably connects the left end of the support's top to the first electric telescopic rod via a rotating shaft," relies on multiple sets of electric telescopic rods on the side of the support for internal support of the tube segment product. If the tube segment product requires rotational processing, the controller inside the support may be unable to continuously power multiple sets, presenting certain limitations. Summary of the Invention

[0003] In response to the above-mentioned deficiencies in the prior art, the present invention provides a device that drives the screw to rotate by a handwheel at the front of the support tube, so that the screw drives the inner support frame to move, thereby causing the inner support plate on the upper part of the suspension seat to support the tube section product outward. During this period, no electricity is required for operation, thereby increasing the adaptability of the equipment. The screw is driven to rotate by the handwheel at the front of the support tube, so that the inner support plate supports the tube section product outward. When processing the edge of the tube section, the handwheel can be removed to reduce the area occupied by the interior of the center part, making it convenient to process the edge of the tube section product, thereby further increasing the adaptability of the equipment to provide an aerospace tube section product side inner support tool.

[0004] The purpose of this utility model is achieved through the following technical solutions:

[0005] A tooling for internal support of an aerospace barrel section product, comprising an equipment base, a guide rod, a support frame, a support cylinder, an internal support seat, and a suspension seat. The side of the equipment base has a screw shaft groove, the screw shaft groove is adapted to the screw, the screw shaft groove is connected to the screw, and the screw rotates inside the screw shaft groove. The front of the equipment base is fixedly connected to the screw motor, the inside of the screw motor is fixedly connected to the screw, the lower part of the processing table is fixedly connected to the threaded seat, the threaded seat is threadedly connected inside the screw, the upper part of the processing table is fixedly connected to the lathing processing assembly, the rear part of the equipment base is fixedly connected to the equipment stand, the front part of the equipment stand has an auxiliary frame, the lower part of the auxiliary frame is fixedly connected to the equipment base, the side of the equipment stand is fixedly connected to the guide rod, the inside of the equipment stand is fixedly connected to the lifting cylinder, and the guide rod is adapted to the support frame.

[0006] The guide rod is connected to the support frame, the support frame slides inside the guide rod, the upper part of the lifting cylinder is fixedly connected to the support frame, the support frame is adapted to the central axis, the support frame is connected to the central axis, the central axis rotates inside the support frame, the rear part of the support frame is fixedly connected to the worm gear frame, the rear part of the central axis has a worm gear, the worm gear frame is adapted to the worm gear, the worm gear frame is connected to the worm gear, and the worm gear rotates inside the worm gear frame.

[0007] The lower part of the support frame is fixedly connected to the worm frame, a worm shaft is provided inside the worm, the worm frame is adapted to the worm shaft, the worm frame is connected to the worm shaft, the worm shaft rotates inside the worm frame, the worm is engaged with the lower part of the worm wheel, the side of the worm frame is fixedly connected to the worm motor, the inside of the worm motor is fixedly connected to the worm shaft, the front part of the central shaft is fixedly connected to the shaft disk, the front part of the shaft disk is provided with a support cylinder, and the inside of the support cylinder is provided with a screw shaft groove.

[0008] The screw shaft groove is adapted to the screw, the screw shaft groove is connected to the screw, the screw rotates inside the screw shaft groove, the front of the screw is fixedly connected to the handwheel disk, the rear of the handwheel is fixedly connected to the docking protrusion, the handwheel disk is adapted to the docking protrusion, the handwheel disk is connected to the docking protrusion, the docking protrusion is inserted into the handwheel disk, the support tube is adapted to the inner support seat, the support tube is connected to the inner support seat, the inner support seat slides inside the support tube, and the lower part of the inner support plate is fixedly connected to the suspension seat. Beneficial effects

[0009] 1. During the use of the aerospace product side inner support tooling of the utility model, the screw is driven to rotate by the handwheel at the front of the support tube, so that the screw drives the inner support frame to move, thereby causing the inner support plate on the upper part of the suspension seat to support the tube section product outward. During this period, no electricity is required for operation, thereby increasing the adaptability of the equipment.

[0010] 2. During the use of the edge support tooling of the utility model, the screw is driven to rotate by the handwheel on the front of the support barrel, so that the inner support plate supports the barrel section product outward. When processing the edge of the barrel section, the handwheel can be removed to reduce the area occupied by the center part, making it easier to process the edge of the barrel section product, thereby further increasing the adaptability of the equipment.

[0011] 3. During the use of the lathe inner support tooling of the utility model, the screw is driven to rotate by the screw motor on the side of the equipment base, so that the screw drives the lathe processing assembly on the upper part of the processing table to move, so that the equipment can adapt to the processing of aerospace materials of different lengths. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 This is a schematic diagram of the inner support tooling structure of the side of an aerospace cylinder segment product described in the utility model.

[0013] Figure 2This is a three-dimensional assembly diagram of the base structure of the side inner support tooling equipment for an aerospace barrel section product described in the utility model.

[0014] Figure 3 This is a three-dimensional assembly diagram of the vertical platform structure of the side inner support tooling equipment for aerospace cylinder segment products described in the utility model.

[0015] Figure 4 This is a three-dimensional assembly diagram of the inner support tooling support frame structure of the aerospace barrel section product described in the utility model.

[0016] Figure 5 This is a three-dimensional assembly diagram of the support tube structure of the side inner support tooling of an aerospace tube segment product described in the utility model. DETAILED DESCRIPTION

[0017] The present invention will be described in further detail below with reference to the accompanying drawings and embodiments:

[0018] Example 1:

[0019] A tool for internal support of the side of an aerospace tube segment product, comprising a device base 01, a guide rod 10, a support frame 12, a support tube 21, an internal support seat 27, and a suspension seat 29. The side of the device base 01 has a screw shaft groove 02, which is adapted to the screw shaft groove 02, which is connected to the screw 03, and the screw 03 rotates inside the screw shaft groove 02. The front of the device base 01 is fixedly connected to the screw motor 04, and the inside of the screw motor 04 is fixedly connected to the screw 03. During the use of the tool for internal support of the side of the product, the screw 03 is driven to rotate by the screw motor 04 on the side of the device base 01, so that the screw 03 drives the processing The lathe processing assembly 07 on the upper part of the platform 05 moves so that the equipment can adapt to processing raw materials of different lengths. The lower part of the processing platform 05 is fixedly connected to the threaded seat 06, and the threaded seat 06 is threadedly connected inside the screw 03. The upper part of the processing platform 05 is fixedly connected to the lathe processing assembly 07, and the rear part of the equipment base 01 is fixedly connected to the equipment stand 08. The front part of the equipment stand 08 has an auxiliary frame 09, and the lower part of the auxiliary frame 09 is fixedly connected to the equipment base 01. The side of the equipment stand 08 is fixedly connected to the guide rod 10, and the inside of the equipment stand 08 is fixedly connected to the lifting cylinder 11, and the guide rod 10 is adapted to the support frame 12.

[0020] Example 2:

[0021] The guide rod 10 of the present invention is connected to the support frame 12, the support frame 12 slides inside the guide rod 10, the upper part of the lifting cylinder 11 is fixedly connected to the support frame 12, the support frame 12 is adapted to the central axis 13, the support frame 12 is connected to the central axis 13, the central axis 13 rotates inside the support frame 12, the rear part of the support frame 12 is fixedly connected to the worm gear frame 14, the rear part of the central axis 13 has a worm gear 15, the worm gear frame 14 is adapted to the worm gear 15, the worm gear frame 14 is connected to the worm gear 15, and the worm gear 15 rotates inside the worm gear frame 14.

[0022] Example 3:

[0023] The lower part of the support frame 12 of the utility model is fixedly connected to the worm frame 16, and a worm shaft 18 is provided inside the worm 17. The worm frame 16 is adapted to the worm shaft 18, and the worm frame 16 is connected to the worm shaft 18, and the worm shaft 18 rotates inside the worm frame 16, and the worm 17 is meshed at the lower part of the worm wheel 15. The side of the worm frame 16 is fixedly connected to the worm motor 19, and the inside of the worm motor 19 is fixedly connected to the worm shaft 18. The front part of the center shaft 13 is fixedly connected to the shaft disk 20, and the front part of the shaft disk 20 has a support tube 21. During the use of the product edge support tooling, the screw 23 is driven to rotate by the handwheel 25 at the front of the support tube 21, so that the inner support plate 28 supports the barrel section product outward. When processing the edge of the barrel section, the handwheel 25 can be removed, thereby reducing the area occupied inside the center part, making it convenient to process the edge of the barrel section product, thereby further increasing the adaptability of the equipment. A screw shaft groove 22 is provided inside the support tube 21.

[0024] Example 4:

[0025] The screw shaft groove 22 of the present invention is adapted to the screw rod 23, the screw shaft groove 22 is connected to the screw rod 23, the screw rod 23 rotates inside the screw shaft groove 22, the front of the screw rod 23 is fixedly connected to the hand wheel disc 24, the rear of the hand wheel 25 is fixedly connected to the docking protrusion 26, the hand wheel disc 24 is adapted to the docking protrusion 26, the hand wheel disc 24 is connected to the docking protrusion 26, the docking protrusion 26 is inserted into the hand wheel disc 24, the support tube 21 is adapted to the inner support seat 27, the support tube 21 is connected to the inner support seat 27, the inner support seat 27 slides inside the support tube 21, and the lower part of the inner support plate 28 is fixedly connected to the suspension seat 29.

[0026] Example 5:

[0027] The inner support seat 27 and the suspension seat 29 of the present invention are both fixedly connected to the suspension shaft 30. The inner support seat 27 is threadedly connected to the screw rod 23. The suspension shaft 30 is adapted to the inner support frame 31. During the use of the product car side inner support tooling, the screw rod 23 is driven to rotate by the handwheel 25 at the front of the support tube 21, so that the screw 23 drives the inner support frame 31 to move, so that the inner support plate 28 on the upper part of the suspension seat 29 supports the barrel section product outward. No electricity is required for operation during this period, thereby increasing the adaptability of the equipment. The suspension shaft 30 is connected to the inner support frame 31, and the inner support frame 31 rotates inside the suspension shaft 30. The rear part of the inner support plate 28 has a positioning seat 32, and the side of the shaft disc 20 is fixedly connected to the positioning rod 33. The positioning rod 33 is adapted to the positioning seat 32. The positioning seat 32 is connected to the positioning rod 33, and the positioning rod 33 slides inside the positioning seat 32.

[0028] Example 6:

[0029] The installation steps of the utility model are as follows: rotate the screw 03 inside the screw shaft groove 02, fix the front of the equipment base 01 with the screw motor 04, fix the inside of the screw motor 04 with the screw 03, fix the lower part of the processing table 05 with the threaded seat 06, thread the threaded seat 06 inside the screw 03, fix the upper part of the processing table 05 with the lathe processing assembly 07, fix the rear part of the equipment base 01 with the equipment stand 08, fix the lower part of the auxiliary frame 09 with the equipment base 01, fix the side of the equipment stand 08 with the guide rod 10, fix the inside of the equipment stand 08 with the lifting cylinder 11, slide the support frame 12 inside the guide rod 10, fix the upper part of the lifting cylinder 11 with the support frame 12, rotate the central axis 13 inside the support frame 12, fix the rear part of the support frame 12 with the worm gear frame 14, rotate the worm gear 15 inside the worm gear frame 14, and fix the support frame 1 2 is fixedly connected to the worm frame 16 at the bottom, the worm shaft 18 is rotated inside the worm frame 16, the worm 17 is meshed with the lower part of the worm wheel 15, the side of the worm frame 16 is fixedly connected to the worm motor 19, the inside of the worm motor 19 is fixedly connected to the worm shaft 18, the front of the central shaft 13 is fixedly connected to the shaft disk 20, the screw 23 is rotated inside the screw shaft groove 22, the front of the screw 23 is fixedly connected to the hand wheel disk 24, and the rear of the hand wheel 25 is fixedly connected to the docking protrusion 26 is fixedly connected, the docking protrusion 26 is inserted into the handwheel disk 24, the inner support seat 27 is slid inside the support tube 21, the lower part of the inner support plate 28 is fixedly connected to the suspension seat 29, the inner support seat 27 and the inside of the suspension seat 29 are fixedly connected to the suspension shaft 30, the inner support seat 27 is threadedly connected to the inside of the screw rod 23, the inner support frame 31 is rotated inside the suspension shaft 30, the side of the shaft disk 20 is fixedly connected to the positioning rod 33, and the positioning rod 33 is slid inside the positioning seat 32.

[0030] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. It should be pointed out that ordinary technicians in this technical field can make several improvements and modifications without departing from the technical principles of the present invention. These improvements and modifications should also be regarded as within the scope of protection of the present invention.

Claims

1. An aerospace cylinder section product side support tooling, characterized by : It comprises an equipment base (01), a guide rod (10), a support frame (12), a support tube (21), an inner support seat (27), and a suspension seat (29). The side of the equipment base (01) has a screw shaft groove (02), the screw shaft groove (02) is adapted to the screw (03), the screw shaft groove (02) is connected to the screw (03), the screw (03) rotates inside the screw shaft groove (02), the front of the equipment base (01) is fixedly connected to the screw motor (04), the inside of the screw motor (04) is fixedly connected to the screw (03), the lower part of the processing table (05) is fixedly connected to the threaded seat (06), the threaded seat (06) is threadedly connected inside the screw (03), the upper part of the processing table (05) is fixedly connected to the lathe edge processing component (07), the rear part of the equipment base (01) is fixedly connected to the equipment vertical The equipment stand (08) is fixedly connected, the front part of the equipment stand (08) has an auxiliary frame (09), the lower part of the auxiliary frame (09) is fixedly connected to the equipment base (01), the side of the equipment stand (08) is fixedly connected to the guide rod (10), the interior of the equipment stand (08) is fixedly connected to the lifting cylinder (11), and the guide rod (10) is adapted to the support frame (12); the guide rod (10) is connected to the support frame (12), the support frame (12) slides inside the guide rod (10), the upper part of the lifting cylinder (11) is fixedly connected to the support frame (12), the support frame (12) is adapted to the central axis (13), the support frame (12) is connected to the central axis (13), the central axis (13) rotates inside the support frame (12), and the rear part of the support frame (12) is fixedly connected to the worm gear frame (14).

2. The aerospace cylinder section product side bracing tooling according to claim 1 is characterized by: A worm gear (15) is provided at the rear of the central shaft (13), a worm gear frame (14) is adapted to the worm gear (15), the worm gear frame (14) is connected to the worm gear (15), and the worm gear (15) rotates inside the worm gear frame (14).

3. The aerospace cylinder section product side bracing tooling according to claim 2 is characterized by: The lower part of the support frame (12) is fixedly connected to the worm frame (16), the worm (17) has a worm shaft (18), the worm frame (16) is adapted to the worm shaft (18), the worm frame (16) is connected to the worm shaft (18), the worm shaft (18) rotates inside the worm frame (16), the worm (17) is meshed with the lower part of the worm wheel (15), the side of the worm frame (16) is fixedly connected to the worm motor (19), the inside of the worm motor (19) is fixedly connected to the worm shaft (18), the front part of the central shaft (13) is fixedly connected to the shaft disc (20), the front part of the shaft disc (20) has a support tube (21), and the inside of the support tube (21) has a screw shaft groove (22).

4. The aerospace cylinder section product side bracing tooling according to claim 3 is characterized by: The screw shaft groove (22) is adapted to the screw rod (23), the screw shaft groove (22) is connected to the screw rod (23), the screw rod (23) rotates inside the screw shaft groove (22), the front part of the screw rod (23) is fixedly connected to the hand wheel plate (24), the rear part of the hand wheel (25) is fixedly connected to the docking protrusion (26), the hand wheel plate (24) is adapted to the docking protrusion (26), the hand wheel plate (24) is connected to the docking protrusion (26), the docking protrusion (26) is inserted into the hand wheel plate (24), the support tube (21) is adapted to the inner support seat (27), the support tube (21) is connected to the inner support seat (27), the inner support seat (27) slides inside the support tube (21), and the lower part of the inner support plate (28) is fixedly connected to the suspension seat (29).

5. The aerospace cylinder section product side bracing tooling according to claim 4 is characterized by: The inner support seat (27) and the suspension seat (29) are both fixedly connected to the suspension shaft (30), the inner support seat (27) is threadedly connected to the screw rod (23), the suspension shaft (30) is adapted to the inner support frame (31), the suspension shaft (30) is connected to the inner support frame (31), the inner support frame (31) rotates inside the suspension shaft (30), the rear part of the inner support plate (28) is provided with a positioning seat (32), the side of the shaft disc (20) is fixedly connected to the positioning rod (33), the positioning rod (33) is adapted to the positioning seat (32), the positioning seat (32) is connected to the positioning rod (33), and the positioning rod (33) slides inside the positioning seat (32).

Citation Information

Patent Citations

  • Novel outer cylinder body inner supporting tool

    CN112112446A