CN213439206U

CN213439206U - Multi-angle composite tool for aviation material processing

Info

Publication number: CN213439206U
Application number: CN202021804727.2U
Authority: CN
Inventors: 许贞
Original assignee: Chengdu Haoyu Aviation Equipment Manufacturing Co ltd
Current assignee: Chengdu Haoyu Aviation Equipment Manufacturing Co ltd
Priority date: 2020-08-26
Filing date: 2020-08-26
Publication date: 2021-06-15
Anticipated expiration: 2030-08-26

Abstract

The utility model discloses a compound frock of multi-angle for aviation material processing, the on-line screen storage device comprises a base, be equipped with the rotation groove on the up end of base, it is connected with the turning block to rotate the inslot rotation, the turning block is kept away from fixedly connected with supporting disk on the lateral wall of rotation groove, the supporting disk is kept away from fixedly connected with supporting shoe on the lateral wall of turning block, all be equipped with strutting arrangement on two lateral walls of supporting shoe, be equipped with a plurality of clamping device that are equidistant setting on the supporting disk, be equipped with a plurality of screw holes that are central symmetry setting on the supporting disk, it is a plurality of equal threaded connection has the screw in the screw hole, four support columns that are mutual symmetry setting of fixedly connected with on the up end. The utility model discloses the fixed work of completion different shapes aviation material piece that can be stable, the position cooperation processing of adjustment aviation material piece that can also be convenient, very big different user demands who has satisfied the user.

Description

Multi-angle composite tool for aviation material processing

Technical Field

The utility model relates to an aeronautical material technical field especially relates to a compound frock of multi-angle is used in aeronautical material processing.

Background

The aviation material is a material of an aviation aircraft, when the aviation material is used for manufacturing the aviation aircraft, a large amount of processing work such as cutting, grinding, polishing, welding and the like needs to be carried out on the aviation material, and in order to ensure that the aviation material can stably complete the processing work, a corresponding tool needs to be used for fixing the corresponding material.

Because the aviation material adds man-hour in putting into the frock and has had corresponding shape, current frock shape is fixed, so current frock can't be convenient carry out convenient fixed to the aviation material of different shape size, and current frock is my after accomplishing the fixed work to the aviation material, can't be convenient again to the position of aviation material adjust, and the very big user of being not convenient for uses like this.

SUMMERY OF THE UTILITY MODEL

The purpose of the utility model is to solve the shortcoming that exists among the prior art, if: the existing tool cannot conveniently complete the fixing work of the aviation materials with different shapes and sizes, and cannot conveniently adjust the position of the fixed aviation materials, so that the tool is not convenient for users to use.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides an aviation material processing is with compound frock of multi-angle, includes the base, be equipped with on the up end of base and rotate the groove, it is connected with the turning block to rotate the inslot internal rotation, fixedly connected with supporting disk on the lateral wall of rotation groove is kept away from to the turning block, the supporting disk is kept away from fixedly connected with supporting shoe on the lateral wall of turning block, all be equipped with strutting arrangement on two lateral walls of supporting shoe, be equipped with a plurality of clamping device that are equidistant setting on the supporting disk, be equipped with a plurality of screw holes that are central symmetry setting on the supporting disk, it is a plurality of equal threaded connection has the screw in the screw hole, four fixedly connected with support columns that are mutual symmetry setting on the up end of base, four common fixedly connected with footstock on the lateral wall that the base was kept away from to the support column.

Preferably, the supporting device comprises a plurality of auxiliary devices, one of the auxiliary devices is arranged close to the supporting block, each auxiliary device comprises two connecting blocks which are symmetrically arranged, a sliding groove is formed in one side wall of each of the two connecting blocks, which is far away from the supporting block, a sliding rod is connected in each of the two sliding grooves in a sliding manner, a working spring is fixedly connected to one side wall of each of the two sliding rods, which is close to the supporting block, one end of each of the two working springs, which is far away from the two sliding rods, is fixedly connected to the inner wall of one side of each of the two sliding grooves, which is close to the supporting block, and one end of each of the two sliding rods, which, one end of the auxiliary rod, far away from the sliding rod, is fixedly connected to two connecting blocks in another auxiliary device, and the two connecting blocks close to the supporting block are fixedly connected to the supporting block.

Preferably, clamping device includes the supporting seat of fixed connection on the supporting disk, the one end fixedly connected with thread groove of base is kept away from to the supporting seat, thread groove female connection has the threaded rod, the one end fixedly connected with clamp plate of base is kept away from to the threaded rod, it is connected with the change to rotate on the threaded rod, fixedly connected with grip block on the outer wall of change, the grip block is close to fixedly connected with protection pad on the lateral wall of base.

Preferably, the threaded rod is rotatably connected with a rotating ring, the rotating ring is close to a side wall of the base and is fixedly connected with a supporting spring, and one end of the supporting spring close to the base is fixedly connected to the side wall of the supporting seat.

Preferably, the supporting plate is provided with two grooves on one side wall far away from the base, the two grooves are respectively arranged on two sides of the supporting block, the two grooves are internally provided with supporting rods, the supporting rods are connected with the supporting rods in a sliding mode, and one ends, far away from the base, of the supporting rods are respectively fixedly connected to the auxiliary rods.

Preferably, an annular groove is formed in the upper end face of the base and matched with a plurality of screws.

The utility model has the advantages that: the user can make unsmooth with the help of the position removal of auxiliary rod in this device, the aviation material spare that the shape is different can be stable place on supporting shoe and auxiliary rod, recycle the convenient completion centre gripping work of clamping device, very big different user demands that have satisfied the user, the user can also make the rotation aviation material spare that the user can be convenient with the help of the rotation of supporting disk and the setting of screw, make the user can accomplish the processing work on the different positions of aviation material spare, very big has made things convenient for the user to use.

Drawings

FIG. 1 is a front structural cross-sectional view of a multi-angle composite tooling for processing aviation materials, which is provided by the utility model;

FIG. 2 is a sectional view of a front structure of a part of a clamping device of the multi-angle composite tool for processing aviation materials, which is provided by the utility model;

fig. 3 is the utility model provides a compound frock of multi-angle for aviation material processing overlook structure cross-sectional view.

In the figure: the device comprises a base 1, a rotating groove 2, a rotating block 3, a supporting disc 4, a supporting block 5, a screw 6, a supporting column 7, a top seat 8, a connecting block 9, a sliding groove 10, a sliding rod 11, a working spring 12, an auxiliary rod 13, a threaded groove 14, a threaded rod 15, a pressing plate 16, a rotating ring 17, a clamping plate 18, a rotating ring 19, a supporting spring 20, a groove 21, a supporting rod 22, an annular groove 23, a threaded hole 24, a processing device 25 and a supporting seat 26.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

Referring to fig. 1-3, a multi-angle composite tool for processing aviation materials, which comprises a base 1, a rotation groove 2 is arranged on the upper end surface of the base 1, a rotation block 3 is rotatably connected in the rotation groove 2, a support plate 4 is fixedly connected to one side wall of the rotation block 3 far away from the rotation groove 2, a support block 5 is fixedly connected to one side wall of the support plate 4 far away from the rotation block 3, two side walls of the support block 5 are respectively provided with a support device, the support device comprises a plurality of auxiliary devices, one of the auxiliary devices is arranged close to the support block 5, each auxiliary device comprises two symmetrically arranged connecting blocks 9, one side wall of each of the two connecting blocks 9 far away from the support block 5 is provided with a sliding groove 10, a sliding rod 11 is slidably connected in each of the two sliding grooves 10, the sliding connection of the sliding rod 11 and the sliding groove 10 enables a user to conveniently adjust the position of, the auxiliary rod 13 can move to different positions to support the aviation material piece, the aviation material pieces with different shapes cannot be interfered, one side wall of each of the two sliding rods 11, which is close to the supporting block 5, is fixedly connected with a working spring 12, one ends of the two working springs 12, which are far away from the two sliding rods 11, are respectively and fixedly connected with the inner wall of one side, which is close to the supporting block 5, of the two sliding grooves 10, the working springs 12 can pull the sliding rods 11 and then pull the auxiliary rods 13, so that the auxiliary rods 13 can be pulled by means of the elasticity of the working springs 12 to partially clamp the rugged aviation material piece, one ends of the two sliding rods 11, which are far away from the supporting block 5, are fixedly connected with the auxiliary rods 13 together, the auxiliary rods 13 can be matched with the supporting block 5 to support the aviation material piece at partial positions, and the aviation material, one end of the auxiliary rod 13 far away from the sliding rod 11 is fixedly connected to two connecting blocks 9 in another auxiliary device;

two connecting blocks 9 close to the supporting block 5 are fixedly connected to the supporting block 5, two grooves 21 are arranged on one side wall of the supporting plate 4 far away from the base 1, the two grooves 21 are respectively arranged at two sides of the supporting block 5, supporting rods 22 are respectively connected in the two grooves 21 in a sliding manner, one ends of the two supporting rods 22 far away from the base 1 are respectively fixedly connected to the auxiliary rods 13, the supporting rods 22 can be used for carrying out auxiliary supporting on the auxiliary rods 13, so that the auxiliary rods 13 can more stably complete supporting work on aviation material pieces, a plurality of clamping devices which are arranged at equal intervals are arranged on the supporting plate 4, each clamping device comprises a supporting seat 26 fixedly connected to the supporting plate 4, one end of the supporting seat 26 far away from the base 1 is fixedly connected with a thread groove 14, a threaded rod 15 is in threaded connection with the thread groove 14, and one, the threaded rod 15 is rotatably connected with a rotating ring 17, the arrangement of the converting ring 17 enables a user to rotate the rotating ring 17 to rotate the clamping plate 18 to different positions to complete clamping work on different positions, the clamping requirement of the user is greatly met, the clamping plate 18 is fixedly connected to the outer wall of the rotating ring 17, a protective pad is fixedly connected to one side wall of the clamping plate 18 close to the base 1, the safety of the clamped aviation material piece is protected due to the arrangement of the protective pad, a rotating ring 19 is rotatably connected to the threaded rod 15, the arrangement of the rotating ring 19 enables the arrangement of the supporting spring 20 not to interfere with the rotation of the rotating ring 17, supporting springs 20 are fixedly connected to one side wall of the rotating ring 19 close to the base 1, one ends of the supporting springs 20 close to the base 1 are fixedly connected to the side wall of the supporting seat 26, the supporting springs 20 can push the rotating ring 19, then the rotating ring 17 is pushed, the clamping plate 18 on the rotating ring 17 can complete clamping work more, inclination can not take place, be equipped with a plurality of screw holes 24 that are central symmetry and set up on supporting disk 4, equal threaded connection has screw 6 in a plurality of screw holes 24, be equipped with ring channel 23 on base 1's the up end, ring channel 23 matches a plurality of screw 6 settings, ring channel 23 makes screw 6 can be better in inserting ring channel 23 the fixed work of completion supporting disk 4, four fixedly connected with's support columns 7 that are mutual symmetry and set up on base 1's the up end, common fixedly connected with footstock 8 on base 1's the lateral wall is kept away from to four support columns 7, footstock 8 is equipped with processing equipment 25 on being close to a lateral wall of base 1, processing equipment 25 is prior art, can accomplish the processing work on the assigned position.

In the utility model, when the user uses the device, firstly, the aviation material piece is placed above the supporting block 5, then the plurality of supporting rods 22 are pulled, the supporting rods 22 drive the auxiliary rods 13, then the sliding rods 11 are driven to slide in the sliding grooves 10 and the working springs 12 are stretched, so the plurality of auxiliary rods 13 can be mutually far away from a certain position, the rugged aviation material piece can be stably placed on the supporting block 5 and the auxiliary rods 13 without interference, the auxiliary rods 13 can clamp the aviation material piece by the aid of the elasticity of the working springs 12, then the user can rotate the threaded rod 15, the threaded rod 15 can drive the pressing plate 16 to push the rotating ring 17 to descend when rotating in the threaded groove 14, then the clamping plate 18 is driven to descend to complete the clamping and fixing work of the aviation material piece, thus the clamping and fixing work of the aviation material pieces with different shapes is completed, very big different user demands that have satisfied the user, then the user alright in order to rotate supporting disk 4 to the assigned position on, rotate screw 6 again for screw 6 inserts annular groove 23 and supports the inner wall of annular groove 23 and accomplish fixedly in the screw hole 24 internal rotation, so just convenient completion the position adjustment work of aviation material spare, then open processing equipment 25 alright in order convenient completion the processing work of aviation material.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The multi-angle composite tool for processing the aviation materials comprises a base (1) and is characterized in that a rotating groove (2) is formed in the upper end face of the base (1), a rotating block (3) is connected to the rotating groove (2) in a rotating mode, a supporting plate (4) is fixedly connected to one side wall, away from the rotating groove (2), of the rotating block (3), a supporting block (5) is fixedly connected to one side wall, away from the rotating block (3), of the supporting plate (4), supporting devices are arranged on two side walls of the supporting block (5), a plurality of clamping devices which are arranged at equal intervals are arranged on the supporting plate (4), a plurality of threaded holes (24) which are arranged in a central symmetry mode are formed in the supporting plate (4), screws (6) are connected to the threaded holes (24) in a uniform mode through threads, four supporting columns (7) which are arranged in a mutual symmetry mode are fixedly connected to the upper end face of the, four support column (7) keep away from common fixedly connected with footstock (8) on the lateral wall of base (1), footstock (8) are equipped with processing equipment (25) on being close to a lateral wall of base (1).

2. The multi-angle composite tool for the aviation material processing according to claim 1, wherein the supporting device comprises a plurality of auxiliary devices, one of the auxiliary devices is arranged close to the supporting block (5), each auxiliary device comprises two symmetrically arranged connecting blocks (9), a side wall of each connecting block (9) far away from the supporting block (5) is provided with a sliding groove (10), the two sliding grooves (10) are connected with sliding rods (11) in a sliding manner, one side wall of each sliding rod (11) near the supporting block (5) is fixedly connected with a working spring (12), one ends of the two working springs (12) far away from the two sliding rods (11) are respectively fixedly connected to the inner wall of one side of each sliding groove (10) near the supporting block (5), one ends of the two sliding rods (11) far away from the supporting block (5) are fixedly connected with an auxiliary rod (13), one end of the auxiliary rod (13) far away from the sliding rod (11) is fixedly connected to two connecting blocks (9) in another auxiliary device and is arranged, and the two connecting blocks (9) close to the supporting block (5) are fixedly connected to the supporting block (5) and are arranged.

3. The multi-angle composite tooling for processing the aviation materials, according to claim 1, is characterized in that the clamping device comprises a supporting seat (26) fixedly connected to the supporting disk (4), a threaded groove (14) is fixedly connected to one end, far away from the base (1), of the supporting seat (26), a threaded rod (15) is connected to the threaded groove (14) in a threaded manner, a pressing plate (16) is fixedly connected to one end, far away from the base (1), of the threaded rod (15), a rotating ring (17) is rotatably connected to the threaded rod (15), a clamping plate (18) is fixedly connected to the outer wall of the rotating ring (17), and a protection pad is fixedly connected to one side wall, close to the base (1), of the clamping plate (18).

4. The multi-angle composite tooling for processing the aviation materials as claimed in claim 3, wherein the threaded rod (15) is rotatably connected with a rotating ring (19), one side wall of the rotating ring (19) close to the base (1) is fixedly connected with a supporting spring (20), and one end of the supporting spring (20) close to the base (1) is fixedly connected to the side wall of the supporting seat (26).

5. The multi-angle composite tooling for processing the aviation materials as claimed in claim 2, wherein two grooves (21) are formed in one side wall of the supporting plate (4) far away from the base (1), the two grooves (21) are respectively arranged at two sides of the supporting block (5), supporting rods (22) are respectively connected in the two grooves (21) in a sliding manner, and one ends of the two supporting rods (22) far away from the base (1) are respectively fixedly connected to the plurality of auxiliary rods (13).

6. The multi-angle composite tool for the machining of the aviation materials is characterized in that an annular groove (23) is formed in the upper end face of the base (1), and the annular groove (23) is matched with a plurality of screws (6).