Auxiliary device for installing aviation parts

Abstract

The utility model discloses an auxiliary device for installing aviation parts, relates to the field of aviation parts, solves the problem that it is difficult for existing devices to pre-assemble aviation parts according to needs, and adopts the following scheme: it comprises a slide and an assembly component; the assembly component comprises a bottom plate and a top plate thereon, a rotating shaft is fixedly installed at the side of the bottom plate, and a shaft sleeve rotatably mounted on the rotating shaft is fixedly installed at the side of the top plate; an electric cylinder seat is fixedly installed on the top of the bottom plate, a sliding card is installed on the output shaft on the top side of the electric cylinder seat, and a card slot matched with the specification of the sliding card is opened on the bottom surface of the top plate; the auxiliary device for installing aviation parts can push the top plate upward through the arrangement of the assembly component on the slide, adjust the inclination angle of the top plate and the part plate limited thereon, so as to facilitate the assembly of small parts on the part plate, and the arrangement of the limiting component can press the part plate between the top plate and the top surface of the top plate.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation parts, in particular to an aviation parts installation auxiliary device. Background Art

[0002] Aviation parts refer to the components used in aviation equipment. With the continuous development of the aviation field, the number of parts required for aviation equipment has gradually increased.

[0003] After searching, the application with patent number CN202223010038.6 discloses an aviation parts installation auxiliary device. Provided is an aviation parts installation auxiliary device that can assist in the installation and clamping of special-shaped aviation parts, improve the clamping efficiency and prevent aviation parts from being damaged during clamping. An aviation parts installation auxiliary device includes a base, a mounting table and a support table, etc. The top of the base is rotatably connected to the mounting table, and the top of the mounting table is connected to the support table. The utility model drives the bidirectional screw to rotate through a first servo motor, so that the sliding seat drives the clamping column to approach each other on the guide seat, clamps and limits the aviation parts, and then cooperates with the clamping column and the second return spring to clamp the special-shaped aviation parts, thereby achieving the effect of facilitating people to install aviation parts and improving the stability when installing aviation parts;

[0004] The above application document realizes the limitation of parts by setting the limiting assembly, but due to the existing assembly type, it is necessary to assemble multiple small parts on a whole plate, and the above application document cannot meet the pre-assembly of multiple parts.

[0005] Therefore, we propose an auxiliary device for installing aviation parts. Utility Model Content

[0006] In view of the deficiencies of the prior art, the utility model provides an aviation parts installation auxiliary device, which solves the problem that the prior device is difficult to pre-assemble aviation parts according to demand.

[0007] To achieve the above objectives, the utility model is implemented through the following technical solutions: an auxiliary device for installing aviation parts, including a slide table and an assembly component of a slide set thereon;

[0008] The assembly assembly includes a bottom plate and a top plate thereon, a rotating shaft is fixedly installed at the side of the bottom plate, and a shaft sleeve rotatably mounted on the rotating shaft is fixedly installed at the side of the top plate;

[0009] An electric cylinder seat is fixedly installed on the top of the bottom plate, a sliding card is installed on the output shaft on the top side of the electric cylinder seat, and a card slot matching the specifications of the sliding card is opened on the bottom surface of the top plate;

[0010] A limiting component is arranged on the top surface of the top plate, and a part plate is pressed between the limiting component and the top surface of the top plate.

[0011] Preferably, the top end of the output shaft of the electric cylinder seat is fixedly connected with a slide card via a hinge seat;

[0012] Among them, the hinged connection between the electric cylinder seat and the slide card is convenient for adjusting the inclination angle of the top plate by the electric cylinder seat, thereby ensuring the auxiliary assembly of the parts plate.

[0013] Preferably, the top plate is a magnetic plate, and the top of the top plate is assembled with two sets of position-limiting assemblies in opposite positions through a bolt assembly;

[0014] Among them, the setting of the top plate magnetic plate is convenient for adsorbing the part plate, and the method of assembling the limit assembly bolts is convenient for adjusting its position, so as to facilitate the installation of part plates of different specifications in corresponding positions.

[0015] Preferably, the limit assembly includes a limit seat, the inner side of the limit assembly is provided with a hydraulic cylinder seat fixedly mounted on the top surface of the top plate, the top end of the hydraulic cylinder seat is fixedly connected to a press table, and the outer wall of the press table is fixedly connected to a press plate located above the part plate;

[0016] Among them, the setting of the hydraulic cylinder seat is convenient for adjusting the height of the top plate, so as to press-fit the part plates of different thicknesses.

[0017] Preferably, a ring-shaped clamping sleeve is fixedly installed at the bottom of the press table, and a clamping frame slidably mounted on the outside of the clamping sleeve is fixedly installed at the top of the limiting assembly;

[0018] Among them, the arrangement of the card sleeve and the card frame facilitates the stability when it is adjusted up and down.

[0019] Preferably, a slide groove is provided on the slide table, a driving motor is fixedly installed on the inner side of the slide groove, the output shaft of the driving motor is a screw shaft, and a screw seat threadedly mounted on the screw shaft is fixedly installed at the bottom of the assembly component;

[0020] The drive motor is arranged to drive the assembly component to slide left and right on the slide table by rotating the drive screw shaft, thereby causing the assembly component to move laterally, so as to facilitate the gradual installation of different small parts.

[0021] The utility model provides an auxiliary device for installing aviation parts, which has the following beneficial effects:

[0022] The aviation parts installation auxiliary device, through the setting of the assembly component on the slide, can push the top plate upward through the setting of the electric cylinder seat, and adjust the inclination angle of it and the part plate limited thereon, so as to facilitate the assembly of small parts on the part plate, and the setting of the limiting component can press the part plate between it and the top surface of the top plate, ensuring the limiting effect and facilitating subsequent auxiliary installation, thereby solving the problem that the existing device is difficult to pre-assemble aviation parts according to demand. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] Figure 1 It is a structural schematic diagram of the utility model;

[0024] Figure 2 It is a schematic diagram of the structure of the bottom side of the utility model;

[0025] Figure 3 This is a schematic diagram of the structure of the bottom plate of the utility model;

[0026] Figure 4 It is a structural schematic diagram of the top plate of the utility model;

[0027] Figure 5 It is a structural schematic diagram of the limit assembly of the utility model;

[0028] Figure 6 It is a structural schematic diagram of the limit seat of the utility model.

[0029] In the figure: 1. slide; 11. slide groove; 2. assembly component; 21. bottom plate; 211. rotating shaft; 212. electric cylinder seat; 213. slide card; 22. top plate; 221. bushing; 222. slot; 23. limit assembly; 231. limit seat; 232. clamping sleeve; 233. press table; 234. press plate; 235. hydraulic cylinder seat; 236. clamping frame; 24. screw seat; 3. drive motor; 31. screw shaft. DETAILED DESCRIPTION

[0030] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0031] See also Figure 1-6The embodiment of the utility model provides a technical solution: an auxiliary device for installing aviation parts, including a slide table 1 and an assembly component 2 slidingly mounted thereon; the assembly component 2 includes a bottom plate 21 and a top plate 22 thereon, a rotating shaft 211 is fixedly mounted on the side of the bottom plate 21, and a shaft sleeve 221 rotatably mounted on the rotating shaft 211 is fixedly mounted on the side of the top plate 22; an electric cylinder seat 212 is fixedly mounted on the top of the bottom plate 21, a sliding card 213 is mounted on the output shaft on the top side of the electric cylinder seat 212, and a card slot 222 matching the specification of the sliding card 213 is opened on the bottom surface of the top plate 22; a limit assembly 23 is arranged on the top surface of the top plate 22, and a part plate is pressed between the limit assembly 23 and the top surface of the top plate 22;

[0032] Among them, the aviation parts installation auxiliary device, through the setting of the assembly component 2 on the slide 1, can push the top plate 22 upward through the setting of the electric cylinder seat 212, and adjust the inclination angle of it and the part plate limited thereon, so as to facilitate the assembly of small parts on the part plate, and the setting of the limiting component 23 can press the part plate between it and the top surface of the top plate 22, ensuring the limiting effect and facilitating subsequent auxiliary installation, thereby solving the problem that the existing device is difficult to pre-assemble aviation parts according to demand.

[0033] Embodiment 2:

[0034] The top end of the output shaft of the electric cylinder seat 212 is fixedly connected to a slide card 213 via a hinge seat; wherein, the hinged connection between the electric cylinder seat 212 and the slide card 213 facilitates the electric cylinder seat 212 to adjust the inclination angle of the top plate 22, thereby ensuring the auxiliary assembly of the parts plate.

[0035] The top plate 22 is a magnetic plate, and the top of the top plate 22 is assembled with two sets of relatively positioned limit assemblies 23 through bolt assemblies; wherein, the arrangement of the magnetic plate of the top plate 22 is convenient for adsorbing the part plate, and the bolt assembly method of the limit assemblies 23 is convenient for adjusting the position thereof, so as to facilitate the installation of part plates of different specifications at corresponding positions.

[0036] The limit assembly 23 includes a limit seat 231, and a hydraulic cylinder seat 235 fixedly installed on the top surface of the top plate 22 is arranged on the inner side of the limit assembly 23, and the top of the hydraulic cylinder seat 235 is fixedly connected to a press platform 233, and the outer wall of the press platform 233 is fixedly connected to a press plate 234 located above the part plate; wherein, the setting of the hydraulic cylinder seat 235 facilitates the adjustment of the height of the press platform 233, so as to press-fit part plates of different thicknesses.

[0037] An annular clamping sleeve 232 is fixedly installed at the bottom of the press table 233, and a clamping frame 236 that is slidably mounted on the outside of the clamping sleeve 232 is fixedly installed at the top of the limiting component 23; wherein, the arrangement of the clamping sleeve 232 and the clamping frame 236 facilitates ensuring its stability when it is adjusted up and down.

[0038] A slide groove 11 is provided on the slide 1, and a driving motor 3 is fixedly installed on the inner side of the slide groove 11. The output shaft of the driving motor 3 is a screw shaft 31, and a screw seat 24 threadedly mounted on the screw shaft 31 is fixedly installed on the bottom of the assembly component 2; wherein, the arrangement of the driving motor 3 facilitates the assembly component 2 to slide left and right on the slide 1 by rotating the driving screw shaft 31, thereby causing the assembly component 2 to move horizontally, so as to facilitate the gradual installation of different small parts thereon.

[0039] The working principle and use process of the utility model are as follows: when the device is needed to work, the driving motor 3 drives the assembly component 2 to move horizontally on the slide 1, adjusts the lateral position of the assembly component 2, and then places the part plate on the top surface of the top plate 22, and opens the hydraulic cylinder seat 235 to drive the press table 233 to move downward, and presses the part plate between it and the top plate 22, and finally opens the electric cylinder seat 212 to drive the top plate 22 to tilt accordingly to ensure the pre-assembly effect.

[0040] The above shows and describes the basic principles and main features of the utility model and the advantages of the utility model. For those skilled in the art, it is obvious that the utility model is not limited to the details of the above exemplary embodiments, and can be implemented in other specific forms without departing from the spirit or basic features of the utility model. Therefore, no matter from which point of view, the embodiments should be regarded as exemplary and non-restrictive. The scope of the utility model is limited by the attached claims rather than the above description, and it is intended to include all changes within the meaning and scope of the equivalent elements of the claims. Any figure mark in the claims should not be regarded as limiting the claims involved.

[0041] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.

Claims

1. An auxiliary device for installing aviation parts, characterized in that: It comprises a slide table (1) and an assembly component (2) of a sliding sleeve thereon; The assembly component (2) comprises a bottom plate (21) and a top plate (22) thereon; a rotating shaft (211) is fixedly mounted on a side edge of the bottom plate (21); and a shaft sleeve (221) rotatably mounted on the rotating shaft (211) is fixedly mounted on a side edge of the top plate (22); An electric cylinder seat (212) is fixedly mounted on the top of the bottom plate (21), a slide card (213) is mounted on the output shaft on the top side of the electric cylinder seat (212), and a card slot (222) matching the specifications of the slide card (213) is provided on the bottom surface of the top plate (22); A limiting component (23) is arranged on the top surface of the top plate (22), and a part plate is pressed between the limiting component (23) and the top surface of the top plate (22).

2. The aviation component installation auxiliary device according to claim 1, characterized in that: The top end of the output shaft of the electric cylinder seat (212) is fixedly connected to a slide card (213) via a hinge seat.

3. The aviation component installation auxiliary device according to claim 1, characterized in that: The top plate (22) is a magnetic plate, and the top of the top plate (22) is assembled with two sets of position-limiting assemblies (23) in opposite positions via bolt assemblies.

4. The aviation component installation auxiliary device according to claim 3, characterized in that: The limiting assembly (23) comprises a limiting seat (231), the inner side of the limiting assembly (23) is provided with a hydraulic cylinder seat (235) fixedly mounted on the top surface of the top plate (22), the top end of the hydraulic cylinder seat (235) is fixedly connected to a press platform (233), and the outer wall of the press platform (233) is fixedly connected to a press plate (234) located above the part plate.

5. The aviation component installation auxiliary device according to claim 4, characterized in that: A ring-shaped clamping sleeve (232) is fixedly mounted on the bottom of the pressing platform (233), and a clamping frame (236) slidably mounted on the outside of the clamping sleeve (232) is fixedly mounted on the top of the limiting component (23).

6. The aviation component installation auxiliary device according to claim 1, characterized in that: The slide table (1) is provided with a slide groove (11), a driving motor (3) is fixedly installed on the inner side of the slide groove (11), the output shaft of the driving motor (3) is a screw shaft (31), and a screw seat (24) threadedly mounted on the screw shaft (31) is fixedly installed at the bottom of the assembly component (2).

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