CN217371439U

CN217371439U - Frock of fixed aircraft mounting panel processing

Info

Publication number: CN217371439U
Application number: CN202220446908.5U
Authority: CN
Inventors: 周维; 郭建华; 莫汝斌; 张明枝; 段香辉; 张韬
Original assignee: Chengdu Kaite Wanrui Precision Machinery Co ltd
Current assignee: Chengdu Kaite Wanrui Precision Machinery Co ltd
Priority date: 2022-03-03
Filing date: 2022-03-03
Publication date: 2022-09-06
Anticipated expiration: 2032-03-03

Abstract

The utility model belongs to the technical field of aviation part processing equipment, especially, be a frock of fixed aircraft mounting panel processing, the fruit pick-up device comprises a frame body, fixed mounting has the hydraulic stem on the top inner wall of framework, the expansion end fixed mounting of hydraulic stem has the lifter plate, the bottom side fixed mounting of lifter plate has two backup pads, rotates in two backup pads and installs same cross axle, fixed cover is equipped with the mounting disc on the cross axle, be central fixed mounting based on the cross axle on the mounting disc and have a plurality of processing motors, be provided with same adjusting part on lifter plate and the cross axle. The utility model relates to a rationally, easy operation can carry out the processing operation to the aircraft mounting panel as required the different processing motor of quick replacement, can make the aircraft mounting panel keep better stability in the in-process of carrying out processing simultaneously, and can adjust the machined position of aircraft mounting panel as required, and it is comparatively convenient to use.

Description

Frock of fixed aircraft mounting panel processing

Technical Field

The utility model relates to an aviation part processing equipment technical field, in particular to frock of fixed aircraft mounting panel processing.

Background

In the field of the aviation industry, airplanes need to face harsh environmental requirements, different mounting plates need to be used in airplane structural parts, and the mounting plates need to be processed according to requirements after production, such as drilling, milling and the like. Adding man-hour aircraft mounting panel and generally fixing at its border position, then wait to process the position through the processing motor to it and process, in the course of working, aircraft mounting panel processing position atress takes place deformation such as crooked or sunken easily, can influence the quality of aircraft structure, adds man-hour simultaneously and is not convenient for carry out quick adjustment to the position of aircraft mounting panel as required, and is not convenient for carry out the processing operation to the aircraft mounting panel as required different processing motors of quick replacement, consequently, the utility model provides a frock of fixed aircraft mounting panel processing is used for solving above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the defects of the prior art and providing a tool for fixing the processing of an aircraft mounting plate.

The above technical purpose of the present invention can be achieved by the following technical solutions: a tool for fixing the processing of an aircraft mounting plate comprises a frame body, wherein a hydraulic rod is fixedly mounted on the inner wall of the top of the frame body, a lifting plate is fixedly mounted at the movable end of the hydraulic rod, two supporting plates are fixedly mounted at the bottom side of the lifting plate, the two supporting plates are rotatably mounted with a same cross shaft, a mounting disc is fixedly sleeved on the cross shaft and provided with a plurality of processing motors based on the cross shaft as the center, the lifting plate and the cross shaft are provided with a same adjusting assembly, the lifting plate is provided with two pressing assemblies, a supporting box is slidably mounted on the inner wall of the bottom of the frame body, two strip-shaped openings are formed in the top of the supporting box, sliding blocks are slidably mounted in the two strip-shaped openings, clamping plates are fixedly mounted at the top ends of the two sliding blocks, and strip-shaped toothed plates are fixedly mounted on one side, close to each other, of the two sliding blocks, the pivot is installed in the last horizontal rotation of supporting box, the one end of pivot extends to the front side of supporting box and fixed cover is equipped with the hand wheel, the fixed cover in the outside of pivot is equipped with the link gear, and two bar pinion racks all mesh with the link gear mutually, one side that supporting box bottom portion and framework are close to each other is provided with same drive assembly.

Preferably, the adjusting component comprises an electric push rod, a vertical toothed plate and a transmission gear, a square plate is fixedly mounted on the supporting plate located on the right side, the vertical toothed plate is connected with the square plate in a vertical sliding mode, the electric push rod is vertically and fixedly mounted on the lifting plate, and the movable end of the electric push rod is fixedly connected with the vertical toothed plate.

Preferably, the pressing and holding assembly comprises a guide column, a pressing plate, a limiting block and a pushing spring, the guide column is vertically slidably mounted on the lifting plate, the limiting block is fixedly mounted at the top end of the guide column, the pressing plate is fixedly mounted at the bottom end of the guide column, two ends of the buffer spring are respectively fixedly connected with the pressing plate and the lifting plate, and the buffer spring is slidably sleeved on the outer side of the guide column.

Preferably, the bottom side of the pressure plate is provided with an installation groove, and a plurality of rubber wheels are rotatably installed in the installation groove.

Preferably, two L-shaped guide rails are fixedly mounted on the inner wall of the bottom of the frame body, guide grooves are formed in two sides of the supporting box, and the supporting box is connected with the corresponding L-shaped guide rails in a sliding mode through the two guide grooves.

Preferably, the same guide plate is horizontally and fixedly installed on the inner walls of the two sides of the strip-shaped opening, and the guide plate is connected with the sliding block in a sliding mode.

Preferably, one of the two sliding blocks is fixedly provided with a pushing spring, and one end of the pushing spring, which is far away from the sliding block, is fixedly connected with the inner wall of one side of the supporting box.

Preferably, the driving assembly comprises an adjusting motor, a driving gear and a rack, the rack is fixedly installed at the bottom of the supporting box, the adjusting motor is fixedly installed on the inner wall of the bottom of the frame body, the driving gear is fixedly sleeved on an output shaft of the adjusting motor, and the driving gear is meshed with the rack.

The utility model has the advantages that: in the utility model, the rotating shaft is rotated by the hand wheel, the two clamping plates can be controlled to move towards the directions away from each other under the coordination of the linkage gear, the strip-shaped toothed plate and the sliding block, thereby being convenient for placing the aircraft mounting plate to be processed on the supporting box and clamping the aircraft mounting plate, the aircraft mounting plate can be pressed and held before the processing operation is carried out on the aircraft mounting plate by the processing motor under the coordination of the guide post, the buffer spring, the pressing plate and the rubber wheel, thereby ensuring that the aircraft mounting plate can keep better stability in the processing process, the required processing motor can be adjusted to the position under the cross shaft according to the requirement under the coordination of the electric push rod, the vertical toothed plate, the transmission gear, the cross shaft and the mounting disc, the supporting box can be controlled to move according to the requirement under the coordination of the adjusting motor, the driving gear and the rack, thereby realizing the adjustment of the processing position of the aircraft mounting plate, meanwhile, the support box can stably slide under the matching of the L-shaped guide rail and the guide groove.

Drawings

In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.

Fig. 1 is a schematic perspective view of a fixture for fixing an aircraft mounting plate according to the present invention;

fig. 2 is a schematic cross-sectional structural view of a fixture for fixing an aircraft mounting plate to be processed according to the present invention;

fig. 3 is a schematic structural diagram of a part a of the tool for fixing the aircraft mounting plate processing provided by the present invention;

fig. 4 is a schematic structural diagram of a part B in the tooling for fixing the aircraft mounting panel processing provided by the utility model.

In the figure: 1. a frame body; 2. a hydraulic lever; 3. a lifting plate; 4. a support plate; 5. a horizontal axis; 6. mounting a disc; 7. a transmission gear; 8. processing a motor; 9. an electric push rod; 10. a vertical toothed plate; 11. a guide post; 12. pressing a plate; 13. a rubber wheel; 14. a buffer spring; 15. an L-shaped guide rail; 16. a support box; 17. a slider; 18. a clamping plate; 19. a strip toothed plate; 20. a rotating shaft; 21. a linkage gear; 22. a pushing spring; 23. adjusting the motor; 24. a driving gear; 25. a rack.

Detailed Description

The technical solution of the present invention will be clearly and completely described below with reference to the specific embodiments. It is obvious that the described embodiments are only some of the embodiments of the present invention, and not all of them. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.

The first embodiment is as follows:

referring to fig. 1-4, a tool for fixing the processing of an aircraft mounting plate comprises a frame body 1, a hydraulic rod 2 is fixedly installed on the inner wall of the top of the frame body 1, a lifting plate 3 is fixedly installed at the movable end of the hydraulic rod 2, the lifting plate 3 can be controlled to lift through the hydraulic rod 3, two support plates 4 are fixedly installed at the bottom side of the lifting plate 3, the same transverse shaft 5 is rotatably installed on the two support plates 4, a mounting disc 6 is fixedly installed on the transverse shaft 5, a plurality of processing motors 8 are fixedly installed on the mounting disc 6 based on the transverse shaft 5 as the center, the same adjusting assembly is arranged on the lifting plate 3 and the transverse shaft 5, the lifting plate 3 is provided with two pressing assemblies, a support box 16 is slidably installed on the inner wall of the bottom of the frame body 1, two strip-shaped openings are formed in the top of the support box 16, sliders 17 are slidably installed in the two strip-shaped openings, clamping plates 18 are fixedly installed at the top ends of the two sliders 17, equal fixed mounting in one side that two sliders 17 are close to each other has bar pinion rack 19, supporting box 16 is improved level and is rotated and install pivot 20, the one end of pivot 20 extends to the front side of supporting box 16 and fixed cover is equipped with the hand wheel, be convenient for operate pivot 20 through the hand wheel, the fixed cover in the outside of pivot 20 is equipped with link gear 21, two bar pinion racks 19 all mesh with link gear 21 mutually, can control two bar pinion racks 19 to the direction motion of difference under link gear 21's cooperation, one side that supporting box 16 bottom and framework 1 are close to each other is provided with same drive assembly.

In this embodiment, the adjusting part includes electric putter 9, erects toothed plate 10 and drive gear 7, and fixed mounting has the square plate in the backup pad 4 that is located the right side, erects toothed plate 10 and the vertical sliding connection of square plate, and the vertical fixed mounting of electric putter 9 is on lifter plate 3, and electric putter 9's expansion end and perpendicular toothed plate 10 fixed connection, can control mounting disc 6 through the regulation and carry out the angle deflection to can adjust a plurality of processing motor 8's position as required.

In this embodiment, the subassembly is held including guide post 11 to the pressure, clamp plate 12, stopper and top push spring 22, the vertical slidable mounting of guide post 11 is on lifter plate 3, stopper fixed mounting is on the top of guide post 11, clamp plate 12 fixed mounting is in the bottom of guide post 11, buffer spring 14's both ends respectively with clamp plate 12 and lifter plate 3 fixed connection, and buffer spring 14 sliding sleeve establishes in the outside of guide post 11, hold the subassembly through the pressure and make clamp plate 12 press the aircraft mounting panel when lifter plate 3 drives processing motor 8 downstream and hold fixedly.

In this embodiment, a mounting groove is formed in the bottom side of the pressing plate 12, a plurality of rubber wheels 13 are rotatably mounted in the mounting groove, and the position of the aircraft mounting plate can be adjusted by the plurality of rubber wheels 13 under the condition that the pressing state is not completely released.

In this embodiment, two L-shaped guide rails 15 are fixedly mounted on the inner wall of the bottom of the frame body 1, guide grooves are formed in both sides of the support box 16, the support box 16 is slidably connected with the corresponding L-shaped guide rails 15 through the two guide grooves, and the support box 16 can stably slide through the cooperation between the L-shaped guide rails 15 and the guide grooves.

In this embodiment, the same deflector is horizontally and fixedly installed on the inner walls of the two sides of the strip-shaped opening, and the deflector is connected with the sliding block 17 in a sliding manner, so that the sliding block 17 can stably slide along the strip-shaped opening through the deflector.

In this embodiment, a pushing spring 22 is fixedly installed on one sliding block 17 of the two sliding blocks 17, one end of the pushing spring 22 far away from the sliding block 17 is fixedly connected with the inner wall of one side of the supporting box 16, and the sliding block 17 can be pushed to slide towards the direction close to the rotating shaft 20 through the pushing spring 22.

In this embodiment, the driving assembly includes an adjusting motor 23, a driving gear 24 and a rack 25, the rack 25 is fixedly installed at the bottom of the support box 16, the adjusting motor 23 is fixedly installed on the inner wall of the bottom of the frame body 1, the driving gear 24 is fixedly installed on the output shaft of the adjusting motor 23 in a fixing mode, the driving gear 24 is meshed with the rack 25, the support box 16 can be controlled to slide along the L-shaped guide rail 15 according to needs through the driving assembly, and therefore the position of the aircraft mounting plate can be adjusted.

The working principle is as follows: when the device is used, firstly, a power supply is switched on, the rotating shaft 20 is rotated anticlockwise through the hand wheel, the two clamping plates 18 can be driven to move towards the directions away from each other under the matching of the linkage gear 21, the strip-shaped toothed plate 19 and the sliding block 17, the aircraft mounting plate to be processed is placed at the position between the two clamping plates 18, then the hand wheel is loosened, the sliding block 17 can drive the clamping plates 18 to clamp the aircraft mounting plate under the action of the pushing spring 22, the lifting plate 3 is pushed to move downwards through the hydraulic rod 2, the pressing plate 12 drives the plurality of rubber wheels 13 to stably press and hold the aircraft mounting plate, the hydraulic rod 2 is controlled to continue to move downwards, the processing motor 8 can be controlled to process the aircraft mounting plate, the lifting plate 3 is controlled to move upwards through the hydraulic rod 2 after the processing is finished, the processing motor 8 is separated from the contact with the aircraft mounting plate, the vertical toothed plate 10 is pushed to move downwards through the electric push rod 9, the mounting disc 6 can be controlled to rotate under the cooperation of the transmission gear 7, so that the other machining motor 8 can be controlled to move to the position right below the transverse shaft 5, the adjusting motor 23 is started, the adjusting motor 23 drives the support box 16 to slide along the L-shaped guide rail 15 through the driving gear 24 and the rack 25, meanwhile, the rubber wheel 13 rolls along the aircraft mounting plate, and then the lifting plate 3 is pushed through the hydraulic rod 2 to perform machining operation on the aircraft mounting plate again.

The second embodiment: the second embodiment is different from the first embodiment in that: referring to fig. 1, 2 and 4, a strip rubber plate is fixedly mounted on one side of each of the two clamping plates 18 close to each other, and the stability of the clamping plates 18 for clamping the aircraft mounting plate can be improved through the strip rubber plate.

It is right above the utility model provides a frock of fixed aircraft mounting panel processing has carried out detailed introduction. The principles and embodiments of the present invention have been explained herein using specific embodiments, which are merely used to help understand the method and its core ideas of the present invention. It should be noted that, for those skilled in the art, without departing from the principle of the present invention, the present invention can be further modified and modified, and such modifications and modifications also fall within the protection scope of the appended claims.

Claims

1. The utility model provides a frock of fixed aircraft mounting panel processing, its characterized in that includes framework (1), fixed mounting has hydraulic stem (2) on the top inner wall of framework (1), the expansion end fixed mounting of hydraulic stem (2) has lifter plate (3), the bottom side fixed mounting of lifter plate (3) has two backup pads (4), rotates on two backup pads (4) and installs same cross axle (5), fixed cover is equipped with mounting disc (6) on cross axle (5), there are a plurality of processing motors (8) for central fixed mounting based on cross axle (5) on mounting disc (6), be provided with same adjusting part on lifter plate (3) and cross axle (5), lifter plate (3) are provided with two and press the holding assembly, slidable mounting has support box (16) on the bottom inner wall of framework (1), two bar mouth have been seted up at the top of support box (16), equal slidable mounting has slider (17) in two bar mouths, and the equal fixed mounting in top of two slider (17) has grip block (18), and the equal fixed mounting in one side that two slider (17) are close to each other has bar pinion rack (19), support case (16) are improved level and are rotated and install pivot (20), the one end of pivot (20) extends to the front side of support case (16) and fixed cover and is equipped with the hand wheel, the fixed cover in the outside of pivot (20) is equipped with linkage gear (21), and two bar pinion racks (19) all mesh with linkage gear (21) mutually, one side that support case (16) bottom and framework (1) are close to each other is provided with same drive assembly.

2. The tool for fixing the machining of the aircraft mounting plate according to claim 1, wherein the tool comprises: the adjusting assembly comprises an electric push rod (9), a vertical toothed plate (10) and a transmission gear (7), a square plate is fixedly mounted on a supporting plate (4) located on the right side, the vertical toothed plate (10) is vertically connected with the square plate in a sliding mode, the electric push rod (9) is vertically fixedly mounted on the lifting plate (3), and the movable end of the electric push rod (9) is fixedly connected with the vertical toothed plate (10).

3. The tool for fixing the machining of the aircraft mounting plate according to claim 1, wherein the tool comprises: the pressing and holding assembly comprises a guide post (11), a pressing plate (12), a limiting block and a pushing spring (22), the guide post (11) is vertically slidably mounted on the lifting plate (3), the limiting block is fixedly mounted at the top end of the guide post (11), the pressing plate (12) is fixedly mounted at the bottom end of the guide post (11), two ends of a buffer spring (14) are fixedly connected with the pressing plate (12) and the lifting plate (3) respectively, and the buffer spring (14) is slidably sleeved on the outer side of the guide post (11).

4. The tool for fixing the machining of the aircraft mounting plate according to claim 3, characterized in that: the bottom side of the pressing plate (12) is provided with a mounting groove, and a plurality of rubber wheels (13) are rotatably mounted in the mounting groove.

5. The tool for fixing the machining of the aircraft mounting plate according to claim 1, wherein the tool comprises: fixed mounting has two L shape guide rails (15) on the bottom inner wall of framework (1), and the guide way has all been seted up to the both sides of supporting box (16), and supporting box (16) are through two guide ways and L shape guide rail (15) sliding connection who corresponds.

6. The tool for fixing the machining of the aircraft mounting plate according to claim 1, wherein the tool comprises: the inner walls of the two sides of the strip-shaped opening are horizontally and fixedly provided with the same guide plate, and the guide plates are connected with the sliding blocks (17) in a sliding mode.

7. The tool for fixing the machining of the aircraft mounting plate according to claim 1, wherein the tool comprises: one sliding block (17) of the two sliding blocks (17) is fixedly provided with a pushing spring (22), and one end of the pushing spring (22) far away from the sliding block (17) is fixedly connected with the inner wall of one side of the supporting box (16).

8. The tool for fixing the machining of the aircraft mounting plate according to claim 1, wherein the tool comprises: the driving assembly comprises an adjusting motor (23), a driving gear (24) and a rack (25), the rack (25) is fixedly installed at the bottom of the supporting box (16), the adjusting motor (23) is fixedly installed on the inner wall of the bottom of the frame body (1), the driving gear (24) is fixedly sleeved on an output shaft of the adjusting motor (23), and the driving gear (24) is meshed with the rack (25).