CN218658976U

CN218658976U - Aviation spare part installation auxiliary device

Info

Publication number: CN218658976U
Application number: CN202223010038.6U
Authority: CN
Inventors: 余冬英
Original assignee: Shanghai Qinqi Aviation Technology Co ltd
Current assignee: Shanghai Qinqi Aviation Technology Co ltd
Priority date: 2022-11-12
Filing date: 2022-11-12
Publication date: 2023-03-21
Anticipated expiration: 2032-11-12

Abstract

The utility model relates to a space flight and aviation apparatus assembly technical field especially relates to an aviation spare part installation auxiliary device. The aviation part installation auxiliary device can be used for assisting in installation and clamping of special-shaped aviation parts, improves clamping efficiency and prevents damage of the aviation parts during clamping. The utility model provides an aviation spare part installation auxiliary device, includes base, mount table and brace table etc. and base top rotary type is connected with the mount table, and the mount table top is connected with the brace table. The utility model discloses a first servo motor drives two-way lead screw and rotates for the sliding seat drives and presss from both sides tight post and be close to each other on the guide holder, presss from both sides tight spacing to aviation spare part, and the rethread presss from both sides tight post and cooperates with second reset spring, presss from both sides tightly heterotypic aviation spare part, thereby has reached and has made things convenient for people to install aviation spare part, improves the effect of the stability when installing aviation spare part.

Description

Aviation spare part installation auxiliary device

Technical Field

The utility model relates to a space flight and aviation apparatus assembly technical field especially relates to an aviation spare part installation auxiliary device.

Background

Aviation spare part is the part of application in the aeronautical equipment, and the continuous development in aviation field, spare part that the aeronautical equipment needs to make increases gradually, and the aviation spare part is comparatively huge usually, need consolidate or lift by crane the aviation spare part through the instrument to be convenient for assemble the aviation spare part, when installing the aviation spare part, can use aviation spare part installation auxiliary device usually.

The prior aviation part auxiliary device is used for hoisting large aviation parts through hoisting equipment when assisting the large aviation parts, then the aviation parts are hoisted through providing a placing platform to be matched with the hoisting equipment to assist installation, and some placing platforms can be provided with adjustable clamping devices, but as the aviation parts are made of special-shaped materials, the problems of unstable clamping and damage to the aviation parts easily occur when clamping is carried out.

To the not enough of above-mentioned prior art, developed now and can assisted the flexibility to press from both sides tightly heterotypic aviation spare part, improved and pressed from both sides tight efficiency and prevent aviation spare part installation auxiliary device that aviation spare part damaged when pressing from both sides tightly.

SUMMERY OF THE UTILITY MODEL

In order to overcome the defects that the conventional aviation part auxiliary device is unstable in clamping and damages aviation parts when clamping special-shaped parts, the aviation part auxiliary device can be used for assisting in mounting and clamping the special-shaped aviation parts, improving the clamping efficiency and preventing the aviation parts from being damaged when clamping the special-shaped parts.

The technical scheme is as follows: the utility model provides an aviation spare part installation auxiliary device, is including base, mount table, brace table, buffing pad, first reset spring and flexible clamping mechanism, and base top rotary type is connected with the mount table, and the mount table top is connected with the brace table, and brace table upper portion slidingtype is connected with the buffing pad, is connected with a plurality of first reset springs between buffing pad and the mount table, is equipped with flexible clamping mechanism on the mount table.

As a preferred technical scheme of the utility model, flexible clamping mechanism is including first servo motor, two-way lead screw, the guide holder, the sliding seat, press from both sides tight post and second reset spring, mount table right part upside is connected with first servo motor, be connected with two-way lead screw on the first servo motor output shaft, two-way lead screw is connected with mount table left part rotary type, two-way lead screw left and right sides equal screw thread formula is connected with the sliding seat, two upsides all are connected with the guide holder about the mount table, the sliding seat of left part and the guide holder sliding type connection of left part, the sliding seat of right part and the guide holder sliding type connection of right part, all be connected with a plurality of tight posts of clamp on one side that the sliding seat is close to each other, the tight post of left part all is connected with second reset spring with between the sliding seat of left part, the tight post of right part all with also be connected with second reset spring between the sliding seat of right part.

As the utility model discloses a preferred technical scheme still including automatic rotary mechanism, automatic rotary mechanism is connected with second servo motor including second servo motor, worm and worm wheel bottom the base, is connected with the worm on the second servo motor output shaft, and the mount table sub-unit connection has the worm wheel, worm and worm wheel meshing.

As an optimized technical scheme of the utility model, the base bottom is equipped with the rubber pad.

As an optimized technical proposal of the utility model, the base is circular.

As an optimized technical scheme of the utility model, press from both sides and all have the rubber contact on the tight post.

Compared with the prior art, the utility model has the advantages of it is following: 1. the utility model discloses a first servo motor drives two-way lead screw and rotates for the sliding seat drives and presss from both sides tight post and is close to each other on the guide holder, presss from both sides tight spacing to aviation spare part, and the rethread presss from both sides tight post and cooperates with second reset spring, presss from both sides tight to heterotypic aviation spare part, thereby has reached and has made things convenient for people to install aviation spare part, improves the effect of the stability when installing aviation spare part.

2. The utility model discloses a second servo motor drives the worm and rotates, drives the worm wheel through the worm and rotates for the mount table is automatic to be rotated, thereby has reached supplementary people and has rotated the mount table, and control slew velocity prevents to appear unexpected, and the people of being convenient for carry out the effect installed to aviation spare part.

Drawings

Fig. 1 is a schematic perspective view of the present invention.

Fig. 2 is a schematic structural diagram of the present invention.

Fig. 3 is a schematic view of the three-dimensional structure of the flexible clamping mechanism of the present invention.

Fig. 4 is a perspective sectional view of the flexible clamping mechanism of the present invention.

Fig. 5 is a schematic view of the three-dimensional structure of the automatic rotating mechanism of the present invention.

Wherein: 1-base, 2-mounting table, 3-supporting table, 4-buffering seat, 5-first return spring, 6-flexible clamping mechanism, 61-first servo motor, 62-bidirectional screw rod, 63-guiding seat, 64-sliding seat, 65-clamping column, 66-second return spring, 7-automatic rotating mechanism, 71-second servo motor, 72-worm and 73-worm wheel.

Detailed Description

The present invention will be described in detail with reference to the accompanying drawings and specific embodiments, but the present invention is not limited thereto.

The utility model provides an aviation spare part installation auxiliary device, as shown in fig. 1 and fig. 2, including base 1, mount table 2, brace table 3, cushion socket 4, first reset spring 5 and flexible clamping mechanism 6, base 1 top rotary type is connected with mount table 2, base 1 bottom is equipped with the rubber pad, can increase the frictional force between base 1 and the ground, improve the stability that base 1 supported, base 1 is circular, it is clean to be convenient for people to base 1 contact area, reduce clean dead angle, 2 tops of mount table are connected with brace table 3, 3 upper portion sliding type of brace table are connected with cushion socket 4, be connected with a plurality of first reset spring 5 between cushion socket 4 and the mount table 2, be equipped with the flexible clamping mechanism 6 that is used for carrying out flexible centre gripping to aviation spare part on the mount table 2.

As shown in fig. 1 to 4, the flexible clamping mechanism 6 includes a first servo motor 61, a bidirectional screw 62, a guide seat 63, a sliding seat 64, clamping posts 65 and a second return spring 66, the upper side of the right portion of the mounting platform 2 is connected with the first servo motor 61, the output shaft of the first servo motor 61 is connected with the bidirectional screw 62, the bidirectional screw 62 is rotatably connected with the left portion of the mounting platform 2, the sliding seat 64 is threadedly connected with both the left and right portions of the bidirectional screw 62, the guide seat 63 is connected with both the upper sides of both the left and right portions of the mounting platform 2, the sliding seat 64 of the left portion is slidably connected with the guide seat 63 of the left portion, the sliding seat 64 of the right portion is slidably connected with the guide seat 63 of the right portion, the sliding seat 64 is connected with a plurality of clamping posts 65 on the side where the sliding seat 64 are close to each other, the clamping posts 65 are provided with rubber contact heads on the clamping posts 65, so that the friction force between the aviation parts can be increased, the aviation parts can be protected and buffered, the aviation parts, the clamping posts 65 are connected with the second return spring 66 between the clamping posts 65 and the sliding seat 64, the aviation parts are driven by the servo motor, the bidirectional screw 61, the bidirectional screw 62 and the guide seat 66, so that the aviation parts close to drive the aviation parts close to the bidirectional screw 62, and the aviation parts close to the guide seat 64, and the aviation parts.

The aviation parts are parts applied to aviation equipment, the aviation field is continuously developed, parts required by the aviation equipment are gradually increased, the aviation parts are usually huge and need to be reinforced or lifted by tools, so that the aviation parts are convenient to assemble, when the aviation parts are installed, the device can be used for assisting, the device is firstly placed in an installation area, then the aviation parts are placed on a buffer seat 4, large aviation parts are placed on the buffer seat 4 through a hoisting device, a heavy object placed on the buffer seat 4 can move downwards on a support table 3 to extrude a first reset spring 5, the first reset spring 5 is matched with the buffer seat 4 to buffer the aviation parts, the installation surface of the aviation parts can be adjusted through rotating the installation table 2, in order to install the aviation parts, the flexible clamping mechanism 6 of the device can be used, after the aviation parts are placed, the first servo motor 61 is started, a first servo motor 61 drives a bidirectional output shaft 62 to rotate, a sliding seat 64 is arranged on a guide seat 63, the aviation parts can be installed, the aviation parts can be driven to be close to a first clamping post 65 through a first clamping post 65, the aviation parts can be driven to be close to a first clamping post 65, the aviation parts can be driven by a first servo motor 61 when the aviation parts rotating and the aviation parts rotating post 65, make and press from both sides tight post 65 and follow sliding seat 64 and keep away from each other on guide holder 63 and reset, press from both sides tight post 65 and aviation spare part after breaking away from, second reset spring 66 recovers and drives and press from both sides tight post 65 and reset, sliding seat 64 restores to the throne after accomplishing, close first servo motor 61, later take off aviation spare part from buffer seat 4, make first reset spring 5 recover and drive buffer seat 4 and reset, accomplish the installation assistance work to aviation spare part, to sum up, it rotates to drive two-way lead screw 62 through first servo motor 61, make sliding seat 64 drive and press from both sides tight post 65 and be close to each other on guide holder 63, press from both sides tight spacing to aviation spare part, rethread presss from both sides tight post 65 and second reset spring 66 and cooperates, press from both sides heterotypic aviation spare part tightly, thereby reached and made things convenient for people to install aviation spare part, the effect of stability when improving installation aviation spare part.

As shown in fig. 1, 2 and 5, the aircraft component mounting device further comprises an automatic rotating mechanism 7, the automatic rotating mechanism 7 comprises a second servo motor 71, a worm 72 and a worm wheel 73, the bottom of the base 1 is connected with the second servo motor 71, the output shaft of the second servo motor 71 is connected with the worm 72, the lower portion of the mounting table 2 is connected with the worm wheel 73, the worm 72 is meshed with the worm wheel 73, the output shaft of the second servo motor 71 drives the worm 72 to rotate, and the worm 72 is meshed with the worm wheel 73 to drive the mounting table 2 to rotate, so that people can rotate and adjust the mounting area of the aircraft component.

In order to facilitate the rotation of the mounting table 2 by people, the automatic rotating mechanism 7 of the device can be used, when the mounting table 2 needs to be rotated, the second servo motor 71 is started, the second servo motor 71 drives the worm 72 to rotate, the worm 72 is meshed with the worm wheel 73, the mounting table 2 is driven by the worm wheel 73 to slowly rotate at a constant speed, the aviation parts are prevented from being thrown out too fast in rotation, after the mounting table 2 is adjusted in rotation, the second servo motor 71 is closed, in sum, the second servo motor 71 drives the worm 72 to rotate, the worm wheel 73 is driven by the worm 72 to rotate, the mounting table 2 automatically rotates, and therefore the effects that people are assisted to rotate the mounting table 2, the rotating speed is controlled to prevent accidents, and people can conveniently mount the aviation parts are achieved.

The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations should also be regarded as the protection scope of the present invention.

Claims

1. The utility model provides an aviation spare part installation auxiliary device, a serial communication port, including base (1), mount table (2), brace table (3), buffing pad (4), a reset spring (5) and flexible clamping mechanism (6), base (1) top rotary type is connected with mount table (2), mount table (2) top is connected with brace table (3), brace table (3) upper portion slidingtype is connected with buffing pad (4), be connected with a plurality of a reset spring (5) between buffing pad (4) and mount table (2), be equipped with flexible clamping mechanism (6) on mount table (2).

2. The aviation component installation auxiliary device according to claim 1, wherein the flexible clamping mechanism (6) comprises a first servo motor (61), a bidirectional screw rod (62), a guide seat (63), a sliding seat (64), clamping columns (65) and a second return spring (66), the first servo motor (61) is connected to the upper side of the right portion of the installation platform (2), the bidirectional screw rod (62) is connected to an output shaft of the first servo motor (61), the bidirectional screw rod (62) is rotatably connected to the left portion of the installation platform (2), the sliding seat (64) is in threaded connection with the left portion and the right portion of the bidirectional screw rod (62), the guide seat (63) is connected to the upper side of the left portion and the upper side of the right portion of the installation platform (2), the sliding seat (64) of the left portion is in sliding connection with the guide seat (63) of the left portion, the sliding seat (64) of the right portion is in sliding connection with the guide seat (63) of the right portion, the clamping columns (65) of the left portion are connected to the sliding seat (64), and the second return spring (66) is connected between the sliding seat (64) of the clamping columns (65) and the right portion.

3. The aviation part installation auxiliary device of claim 2, further comprising an automatic rotating mechanism (7), wherein the automatic rotating mechanism (7) comprises a second servo motor (71), a worm (72) and a worm wheel (73), the bottom of the base (1) is connected with the second servo motor (71), the output shaft of the second servo motor (71) is connected with the worm (72), the lower portion of the installation table (2) is connected with the worm wheel (73), and the worm (72) is meshed with the worm wheel (73).

4. An auxiliary device for the installation of aviation components and parts according to claim 1, wherein a rubber pad is arranged at the bottom of the base (1).

5. An aircraft component mounting aid according to claim 1 characterised in that the base (1) is circular.

6. An aircraft component mounting aid according to claim 2 wherein the clamping posts (65) are each provided with rubber contacts.