CN211073516U

CN211073516U - Multi-angle composite tool for aviation material processing

Info

Publication number: CN211073516U
Application number: CN201922164427.6U
Authority: CN
Inventors: 牛武
Original assignee: Changsha Aeronautical Vocational and Technical College
Current assignee: Changsha Aeronautical Vocational and Technical College
Priority date: 2019-12-05
Filing date: 2019-12-05
Publication date: 2020-07-24
Anticipated expiration: 2029-12-05

Abstract

The utility model discloses a compound frock of multi-angle is used in processing of aviation material, the on-line screen storage device comprises a base, the equal fixedly connected with fixed plate in base both ends top, two the fixed plate is parallel arrangement, the top of base is equipped with the backup pad, the both ends of backup pad are all connected with the fixed plate through the pivot. The utility model discloses in, rotate through adjusting first motor and second motor, the effect of adjusting the angle of fixing aviation spare part on the rotor plate has been reached to the centre gripping, make things convenient for the workman to process aviation spare part, furthermore, the device still adopts adjusting threaded rod to rotate, drive two tight piece relative motion of clamp, fix the mode at the rotor plate with aviation spare part centre gripping, be convenient for improve the device's suitability, the aviation spare part of convenient to different length size is fixed, the device simple structure, the suitability is strong, it is convenient to adjust, the cost is lower, still be convenient for remove simultaneously, therefore, has fine practicality.

Description

Multi-angle composite tool for aviation material processing

Technical Field

The utility model relates to an aviation spare part processingequipment technical field, more specifically say, in particular to compound frock of multi-angle is used in processing of aviation material.

Background

At present, along with the opening of the aviation manufacturing industry to civil enterprises, more and more small and micro enterprises are processed to the aviation manufacturing industry.

Because of the particularity of aviation parts, especially the processing of taking back-off aviation structure class part, more and more spare parts need five axle equipment of higher end, and this equipment value is very high usually, and most little, little enterprise does not have sufficient economic strength to purchase this equipment, has put forward a compound frock of multi-angle for aviation material processing now for make up little, little enterprise does not have the economic strength to purchase the current state of five axle high-end equipment, solves the back-off characteristic processing problem that aviation parts made through this frock.

Therefore, the multi-angle composite tool for machining the aviation materials is provided to solve the problems.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the problem existing in the prior art, and the compound frock of multi-angle is used in aviation material processing who provides.

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

a multi-angle composite tool for processing aviation materials comprises a base, wherein fixed plates are fixedly connected to the tops of two ends of the base, the two fixed plates are arranged in parallel, the top of the base is provided with a supporting plate, both ends of the supporting plate are connected with the fixed plate through rotating shafts, one end of each rotating shaft, far away from the supporting plate, penetrates through the fixed plate and extends outwards, the outer side wall of one of the fixed plates is fixedly connected with a first motor, the first motor is connected with one end of one of the rotating shafts through a connecting mechanism, the outer side wall of one of the fixed plates is fixedly connected with a controller, the controller is electrically connected with the first motor through a lead, the supporting plate is connected with a rotating plate through an adjusting mechanism, a rotating groove corresponding to the rotating plate is formed in the top of the supporting plate, and two symmetrically-arranged clamping mechanisms are fixedly connected to the top of the rotating plate.

Preferably, the connecting mechanism comprises a chain, the output shaft of the first motor penetrates through the fixing plate and one end, far away from the supporting plate, of one rotating shaft, and is fixedly connected with chain wheels, and the two chain wheels are connected through the chain.

Preferably, a detachable protective cover is installed on one side of the fixing plate, which is far away from the first motor.

Preferably, the adjusting mechanism comprises a second motor fixedly connected to the bottom of the supporting plate, an output shaft of the second motor penetrates through the supporting plate and is fixedly connected with the bottom of the rotating plate, and the second motor is electrically connected with the controller through a wire.

Preferably, fixture includes the fixed block of fixed connection at the rotor plate top, the last threaded connection of fixed block has the threaded rod, the one end of threaded rod runs through the fixed block and is connected with tight piece through the rotor plate, press from both sides to be equipped with the rotation cavity that corresponds with the rotor plate on the tight piece, press from both sides to be equipped with the rotation mouth that corresponds with the threaded rod on the tight piece, it communicates with each other with the rotation mouth to rotate the cavity, press from both sides tight piece and pass through the telescopic link and be connected with the fixed block, the threaded rod is kept away from the one end fixedly.

Preferably, the bottom of the base is fixedly connected with four rollers.

The embodiment of the utility model provides a technical scheme can include following beneficial effect:

the utility model discloses in, rotate through adjusting first motor and second motor, the effect of adjusting the angle of fixing aviation spare part on the rotor plate has been reached to the centre gripping, make things convenient for the workman to process aviation spare part, furthermore, the device still adopts adjusting threaded rod to rotate, drive two tight piece relative motion of clamp, fix the mode at the rotor plate with aviation spare part centre gripping, be convenient for improve the device's suitability, the aviation spare part of convenient to different length size is fixed, the device simple structure, the suitability is strong, it is convenient to adjust, the cost is lower, still be convenient for remove simultaneously, therefore, has fine practicality.

Drawings

FIG. 1 is a schematic structural view of a multi-angle composite tooling for processing aviation materials, which is provided by the present invention;

FIG. 2 is a schematic view of the structure at A in FIG. 1;

fig. 3 is the utility model provides a threaded rod, fixed block, press from both sides tight piece, handle, backup pad and rotor plate's connection structure sketch map in multi-angle composite frock for aviation material processing.

In the figure: 1. a base; 2. a fixing plate; 3. a controller; 4. a rotating shaft; 5. a support plate; 6. a first motor; 7. a chain; 8. a sprocket; 9. a second motor; 10. a protective cover; 11. a rotating plate; 12. a fixed block; 13. a threaded rod; 14. a clamping block; 15. a telescopic rod; 16. a handle; 17. and (6) rotating the block.

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, comprising a base 1, wherein fixed plates 2 are fixedly connected to the tops of two ends of the base 1, the two fixed plates 2 are arranged in parallel, a supporting plate 5 is arranged on the top of the base 1, two ends of the supporting plate 5 are connected with the fixed plates 2 through rotating shafts 4, one end of each rotating shaft 4 far away from the corresponding supporting plate 5 penetrates through the corresponding fixed plate 2 and extends outwards, a first motor 6 is fixedly connected to the outer side wall of one of the fixed plates 2, the first motor 6 is connected with one end of one of the rotating shafts 4 through a connecting mechanism, a controller 3 is fixedly connected to the outer side wall of one of the fixed plates 2, the controller 3 is electrically connected with the first motor 6 through a wire, the connecting mechanism comprises a chain 7, a chain wheel 8 is fixedly connected to one end of the first motor 6, the two chain wheels 8 are connected through the chain 7, it should be noted that the power supply modes of the first motor 6 and the first motor 6 are the prior art, and the description is not repeated here, the controller 3 is used for controlling the first motor 6 to rotate in the forward and reverse directions, the inclination angle of the supporting plate 5 can be adjusted through the forward and reverse rotation of the first motor 6, and workers can conveniently process aviation parts fixed on the rotating plate 11; it should be noted that the first motor 6 cannot rotate in the energized state, and the controller 3 can only be used to regulate the rotation of the first motor 6.

Wherein, the detachable safety cover 10 is installed to the one side that first motor 6 was kept away from to fixed plate 2, prevents that chain 7 and sprocket 8 from rotating and causing the damage to the workman, and safety cover 10 can play the effect of protection.

The supporting plate 5 is connected with a rotating plate 11 through an adjusting mechanism, a rotating groove corresponding to the rotating plate 11 is formed in the top of the supporting plate 5, the adjusting mechanism comprises a second motor 9 fixedly connected to the bottom of the supporting plate 5, an output shaft of the second motor 9 penetrates through the supporting plate 5 and is fixedly connected with the bottom of the rotating plate 11, the second motor 9 is electrically connected with the controller 3 through a wire, it needs to be noted that the power supply technologies of the second motor 9 and the second motor 9 are the prior art, too much description is not provided herein, the controller 3 controls the second motor 9 to rotate, the rotating plate 11 is finely adjusted, and workers can conveniently process aviation parts clamped and fixed on the rotating plate 11; it should be noted that the second motor 9 cannot rotate in the energized state, and the controller 3 can only be used to regulate the rotation of the second motor 9.

Wherein, the top of the rotating plate 11 is fixedly connected with two symmetrically arranged clamping mechanisms, each clamping mechanism comprises a fixed block 12 fixedly connected with the top of the rotating plate 11, the upper thread of the fixed block 12 is connected with a threaded rod 13, one end of the threaded rod 13 penetrates through the fixed block 12 and is connected with a clamping block 14 through a rotating block 17, the clamping block 14 is provided with a rotating cavity corresponding to the rotating block 17, the clamping block 14 is provided with a rotating port corresponding to the threaded rod 13, the rotating cavity is communicated with the rotating port, the clamping block 14 is connected with the fixed block 12 through a telescopic rod 15, one end of the threaded rod 13 far away from the clamping block 14 is fixedly connected with a handle 16, the two clamping blocks 14 are driven to move relatively by rotating the threaded rod 13, the distance between the two clamping blocks 14 is adjusted according to the length of an aviation part, so as to clamp and fix the aviation, the aviation parts are fixed by adopting the mode, so that the applicability is strong, and the aviation parts with different lengths can be fixed; the telescopic rod 15 is a multi-section telescopic rod.

Wherein, four gyro wheels of bottom fixedly connected with of base 1, it needs to explain that, two gyro wheels that lie in same one side are the universal wheel, and four gyro wheels all take self-locking function.

The utility model discloses in, add man-hour as needs to aviation spare part, the aviation spare part that will process is placed on rotor plate 11, then rotate two threaded rods 13, adjust two distances of pressing from both sides between tight piece 14, it is fixed to carry out the centre gripping to aviation spare part through two tight pieces 14 of pressing from both sides, fix aviation spare part on rotor plate 11, the workman is carrying out the in-process of processing to aviation spare part, can control the inclination of first motor 6 regulation backup pad 5 as required, also can control second motor 9 and finely tune rotor plate 11, the device simple structure, the suitability is strong, it is convenient to adjust, the cost is lower, still be convenient for simultaneously remove, therefore, has fine practicality.

The utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the description with the record of drawing of description, and the concrete connection mode of each part all adopts conventional means such as ripe bolt, rivet, welding among the prior art, and machinery, part and equipment all adopt prior art, and conventional model, including circuit connection adopts conventional connection mode among the prior art, does not detailed here again.

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 the aviation material processing comprises a base (1) and is characterized in that fixed plates (2) are fixedly connected to the tops of the two ends of the base (1), the two fixed plates (2) are arranged in parallel, a supporting plate (5) is arranged on the top of the base (1), the two ends of the supporting plate (5) are connected with the fixed plates (2) through rotating shafts (4), one end, far away from the supporting plate (5), of each rotating shaft (4) penetrates through the corresponding fixed plate (2) and extends outwards, a first motor (6) is fixedly connected to the outer side wall of one of the fixed plates (2), the first motor (6) is connected with one end of one of the rotating shafts (4) through a connecting mechanism, a controller (3) is fixedly connected to the outer side wall of one of the corresponding fixed plate (2), and the controller (3) is electrically connected with the first motor (6) through a wire, backup pad (5) are connected with rotor plate (11) through adjustment mechanism, the top of backup pad (5) is equipped with the rotation groove that corresponds with rotor plate (11), the fixture that two symmetries of rotor plate (11) top fixedly connected with set up.

2. The multi-angle composite tool for the machining of the aviation materials is characterized in that the connecting mechanism comprises a chain (7), an output shaft of the first motor (6) penetrates through the fixing plate (2) and one end, far away from the supporting plate (5), of one rotating shaft (4) to be fixedly connected with chain wheels (8), and the two chain wheels (8) are connected through the chain (7).

3. The multi-angle composite tool for the aviation material processing is characterized in that a detachable protective cover (10) is mounted on one side, away from the first motor (6), of the fixing plate (2).

4. The multi-angle composite tool for machining the aviation materials as claimed in claim 1, wherein the adjusting mechanism comprises a second motor (9) fixedly connected to the bottom of the supporting plate (5), an output shaft of the second motor (9) penetrates through the supporting plate (5) and is fixedly connected with the bottom of the rotating plate (11), and the second motor (9) is electrically connected with the controller (3) through a wire.

5. The multi-angle composite tooling for processing the aviation materials, according to claim 1, is characterized in that the clamping mechanism comprises a fixed block (12) fixedly connected to the top of a rotating plate (11), a threaded rod (13) is connected to the upper thread of the fixed block (12), one end of the threaded rod (13) penetrates through the fixed block (12) and is connected with a clamping block (14) through a rotating block (17), a rotating cavity corresponding to the rotating block (17) is formed in the clamping block (14), a rotating port corresponding to the threaded rod (13) is formed in the clamping block (14), the rotating cavity is communicated with the rotating port, the clamping block (14) is connected with the fixed block (12) through a telescopic rod (15), and a handle (16) is fixedly connected to one end, far away from the clamping block (14), of the threaded rod (13).

6. The multi-angle composite tool for machining the aviation material as claimed in claim 1, wherein four rollers are fixedly connected to the bottom of the base (1).