CN220825904U

CN220825904U - Aviation spare part frock

Info

Publication number: CN220825904U
Application number: CN202322465282.XU
Authority: CN
Inventors: 曹洋; 祝燕莉; 邵琴; 覃运霜
Original assignee: Guizhou Hangfa Technology Industry And Trade Co ltd
Current assignee: Guizhou Hangfa Technology Industry And Trade Co ltd
Priority date: 2023-09-12
Filing date: 2023-09-12
Publication date: 2024-04-23
Anticipated expiration: 2033-09-12

Abstract

The utility model provides an aviation part tool, which comprises: a bottom frame; the sliding rods are respectively and fixedly arranged at two ends of the top of the bottom frame, the outer side faces of the sliding rods are in sliding connection with sliding blocks, sliding sleeves are fixedly arranged at two sides of the sliding blocks, limiting rods are in sliding connection with the inner side faces of the sliding sleeves, and a moving plate is fixedly arranged at one end of each limiting rod; the backup pad, backup pad fixed mounting in one side of movable plate. According to the aviation part tool provided by the utility model, the structures such as the sliding block, the sliding sleeve, the movable plate, the limiting rod, the supporting plate, the movable plate, the pressing plate and the rubber pad are matched with each other, and when the aviation part tool is used, the limiting rod slides on the inner side surface of the sliding sleeve, so that a user can conveniently adjust the position of the pressing plate, and when the aviation part tool is used, parts with different sizes can be conveniently clamped, and the adaptability of the aviation part tool is improved.

Description

Aviation spare part frock

Technical Field

The utility model relates to the technical field of fixtures, in particular to an aviation part fixture.

Background

The fixture is used to fix the machining object in the correct position during the machining process to accept the construction or detection. In a broad sense, any process in the process, the device for rapidly, conveniently and safely installing the workpiece can be called a fixture, and the fixture is often required to fix the workpiece in the processing of the aviation parts, so that the workpiece can be processed and manufactured conveniently.

The utility model provides a patent application that publication number is CN 212043625U among the prior art, it is through setting up the operation panel, the fly leaf, the clamp plate, the screw hole, first lead screw, control cavity, first bearing, the worm wheel, the worm, the cooperation effect of second bearing, elastic mechanism and actuating mechanism, only need place the machined part between clamp plate and operation panel, and then the clamp plate is from the automatic machined part of pressing down, the operating procedure is simple convenient, because fly leaf and clamp plate elastic connection, and then make the clamp plate elasticity press the machined part, through the deformation degree of spring, be convenient for know the dynamics of clamp plate pressing the machined part, avoid the pressure too big, lead to the machined part to warp.

However, when the device is used, the position of the pressing plate cannot be adjusted, so that different parts cannot be clamped, and the adaptability of the device is reduced.

Therefore, it is necessary to provide an aviation component fixture to solve the above technical problems.

Disclosure of utility model

The utility model provides an aviation part tool, which solves the problems that parts with different sizes cannot be clamped and the adaptability of the device is reduced.

In order to solve the technical problems, the utility model provides an aviation part tool, which comprises:

A bottom frame;

The sliding rods are respectively and fixedly arranged at two ends of the top of the bottom frame, the outer side faces of the sliding rods are in sliding connection with sliding blocks, sliding sleeves are fixedly arranged at two sides of the sliding blocks, limiting rods are in sliding connection with the inner side faces of the sliding sleeves, and a moving plate is fixedly arranged at one end of each limiting rod;

The support plate, backup pad fixed mounting in one side of movable plate, the inside of the both ends of backup pad is all sliding connection has the movable rod, the bottom fixed mounting of movable rod has the clamp plate, the bottom fixed mounting of clamp plate has the rubber pad, the lateral surface cover of movable rod is equipped with the spring, the spring set up in the bottom of backup pad.

Preferably, a driving motor is fixedly arranged on one side of the bottom frame, a worm is fixedly arranged at the output end of the driving motor, and one end of the worm is rotatably connected to one side of the inner side surface of the bottom frame.

Preferably, both ends of the bottom of the inner side surface of the bottom frame are rotatably connected with rotating shafts, and the top of each rotating shaft penetrates through the top of the inner side surface of the bottom frame and extends to the top.

Preferably, the top of the rotating shaft is fixedly provided with a worm wheel, the worm wheel is meshed with one side of the worm, the top of the rotating shaft is fixedly provided with a screw rod, the outer side surface of the screw rod is in threaded connection with a threaded block, and the threaded block is fixedly arranged on one side of the sliding block.

Preferably, the front surface of the bottom frame is fixedly provided with a controller.

Preferably, a threaded rod is fixedly arranged at the bottom of the movable rod, and a thread ring is connected to the outer side surface of the threaded rod in a threaded manner.

Preferably, the bottom of the thread ring is fixedly arranged at the top of the pressing plate.

Compared with the related art, the aviation part tool provided by the utility model has the following beneficial effects:

The utility model provides an aviation part tool, which is matched with structures such as a sliding block, a sliding sleeve, a moving plate, a limiting rod, a supporting plate, a moving plate, a pressing plate and a rubber pad, wherein the limiting rod slides on the inner side surface of the sliding sleeve when the aviation part tool is used, so that a user can conveniently adjust the position of the pressing plate, and parts with different sizes can be conveniently clamped when the aviation part tool is used, and the adaptability of the aviation part tool is improved.

Drawings

Fig. 1 is a schematic structural diagram of a first embodiment of an aviation component tool provided by the utility model;

FIG. 2 is a schematic cross-sectional view of the bottom frame shown in FIG. 1;

FIG. 3 is a schematic side view of the movable plate shown in FIG. 1;

FIG. 4 is an enlarged schematic view of portion A shown in FIG. 2;

Fig. 5 is a schematic structural diagram of a second embodiment of an aviation component tool provided by the utility model.

Reference numerals in the drawings: 1. the device comprises a bottom frame, 11, a controller, 12, a driving motor, 13, a worm, 14, a worm wheel, 15, a rotating shaft, 16, a screw rod, 17, a threaded block, 2, a sliding block, 21, a sliding rod, 22, a sliding sleeve, 23, a moving plate, 24, a limiting rod, 25, a supporting plate, 26, a moving rod, 27, a spring, 28, a pressing plate, 29, a rubber pad, 3, a threaded ring, 31 and a threaded rod.

Detailed Description

The utility model will be further described with reference to the drawings and embodiments.

First embodiment

Referring to fig. 1, fig. 2, fig. 3, and fig. 4 in combination, fig. 1 is a schematic structural diagram of a first embodiment of an aviation component fixture according to the present utility model; FIG. 2 is a schematic cross-sectional view of the bottom frame shown in FIG. 1; FIG. 3 is a schematic side view of the movable plate shown in FIG. 1; fig. 4 is an enlarged schematic view of a portion a shown in fig. 2. An aerospace component tooling, comprising: a bottom frame 1;

the sliding rod 21 is fixedly arranged at two ends of the top of the bottom frame 1 respectively, the outer side face of the sliding rod 21 is connected with a sliding block 2 in a sliding manner, sliding sleeves 22 are fixedly arranged at two sides of the sliding block 2, a limiting rod 24 is fixedly connected with the inner side face of the sliding sleeve 22 in a sliding manner, and a moving plate 23 is fixedly arranged at one end of the limiting rod 24;

The backup pad 25, backup pad 25 fixed mounting in one side of movable plate 23, the inside at the both ends of backup pad 25 all sliding connection has movable rod 26, the bottom fixed mounting of movable rod 26 has clamp plate 28, the bottom fixed mounting of clamp plate 28 has rubber pad 29, the lateral surface cover of movable rod 26 is equipped with spring 27, spring 27 set up in the bottom of backup pad 25.

One side of the bottom frame 1 is fixedly provided with a driving motor 12, the output end of the driving motor 12 is fixedly provided with a worm 13, and one end of the worm 13 is rotatably connected to one side of the inner side surface of the bottom frame 1.

Both ends of the bottom of the inner side surface of the bottom frame 1 are rotatably connected with rotating shafts 15, and the top of each rotating shaft 15 penetrates through the top of the inner side surface of the bottom frame 1 and extends to the top.

The top of the rotating shaft 15 is fixedly provided with a worm wheel 14, the worm wheel 14 is meshed with one side of the worm 13, the top of the rotating shaft 15 is fixedly provided with a screw rod 16, the outer side surface of the screw rod 16 is in threaded connection with a threaded block 17, and the threaded block 17 is fixedly arranged on one side of the sliding block 2.

The front surface of the bottom frame 1 is fixedly provided with a controller 11.

When in use, the controller 11 and the driving motor 12 are connected through wires, so that the controller 11 is convenient for a user to control the on-off and forward-reverse rotation of the driving motor 12.

The working principle of the aviation part tool provided by the utility model is as follows:

When the device is used, a user puts a part on the top of the bottom frame 1, then moves the moving plate 23, the moving plate 23 drives the limiting rod 24 to slide on the inner side surface of the sliding sleeve 22, the pressing plate 28 drives the rubber pad 29 to move to the top of the part, then the user starts the driving motor 12, the driving motor 12 drives the worm 13 to rotate, the worm 13 drives the worm wheel 14 and the rotating shaft 15 to rotate, then the rotating shaft 15 drives the screw rod 16 to be in threaded connection in the threaded block 17, then the threaded block 17 drives the sliding block 2 to move downwards, when the sliding block 2 moves downwards, the sliding block 2 slides on the outer side surface of the sliding rod 21, and the pressing plate 28 and the rubber pad 29 are driven by the sliding block 2 to move downwards to be pressed on the top of the part, so that the part is limited and fixed.

Through the structure such as slider 2, sliding sleeve 22, movable plate 23, gag lever post 24, backup pad 25, movable plate 26, clamp plate 28 and rubber pad 29 mutually support, when using, gag lever post 24 slides at the medial surface of sliding sleeve 22 to the convenience of customers adjusts the position of clamp plate 28, so when using, conveniently carries out the centre gripping to the part of equidimension not, thereby has increased the adaptability of device.

Second embodiment

Referring to fig. 5 in combination, another tooling for aviation components is provided according to a second embodiment of the present application. The second embodiment is merely a preferred manner of the first embodiment, and implementation of the second embodiment does not affect the implementation of the first embodiment alone.

Specifically, the second embodiment of the present application provides an aviation component tool, which is different in that a threaded rod 31 is fixedly installed at the bottom of the moving rod 26, and a thread ring 3 is screwed on the outer side surface of the threaded rod 31.

The bottom of the thread ring 3 is fixedly mounted on the top of the pressing plate 28.

When the user performs the operation for a long time, the user can rotate the moving rod 26 when the elasticity of the spring 27 is reduced, so that one end of the moving rod 26 drives the threaded rod 31 to be in threaded connection with the inner side surface of the thread ring 3, and the spring 27 is detached.

Through the mutual cooperation of structures such as screw thread circle 3 and threaded rod 31, when using, the user is through rotating movable rod 26, makes movable rod 26 drive threaded rod 31 and carries out threaded connection at the medial surface of screw thread circle 3 to the facilitate the use user dismantles the change to spring 27, thereby facilitates the use of user.

The foregoing description is only illustrative of the present utility model and is not intended to limit the scope of the utility model, and all equivalent structures or equivalent processes or direct or indirect application in other related technical fields are included in the scope of the present utility model.

Claims

1. An aerospace component tooling, comprising:

A bottom frame;

2. The aviation component tool according to claim 1, wherein a driving motor is fixedly installed on one side of the bottom frame, a worm is fixedly installed at the output end of the driving motor, and one end of the worm is rotatably connected to one side of the inner side face of the bottom frame.

3. The aviation component fixture of claim 2, wherein two ends of the bottom of the inner side surface of the bottom frame are rotatably connected with rotating shafts, and the top of each rotating shaft penetrates through the top of the inner side surface of the bottom frame and extends to the top.

4. The aviation component tool according to claim 3, wherein a worm wheel is fixedly installed at the top of the rotating shaft, the worm wheel is meshed with one side of the worm, a screw rod is fixedly installed at the top of the rotating shaft, a threaded block is connected to the outer side face of the screw rod in a threaded mode, and the threaded block is fixedly installed on one side of the sliding block.

5. The tooling for aviation components of claim 4, wherein the front surface of the bottom frame is fixedly provided with a controller.

6. The aerospace component tool of claim 5, wherein a threaded rod is fixedly mounted at the bottom of the movable rod, and a threaded ring is in threaded connection with the outer side surface of the threaded rod.

7. The aerospace component tooling of claim 6, wherein the bottom of the threaded collar is fixedly mounted to the top of the platen.