Supporting device for maintaining aviation parts
By designing a support device for aviation components, including a lower mounting plate, an upper mounting plate and a hydraulic cylinder seat, combined with a combination of a guide rack and a clamping plate, the vertical clamping of the components and adaptation to different specifications is achieved. The components of the existing devices solve the problem of inconvenient installation inconveniently and improve maintenance efficiency.
Patent Information
- Application Number
- CN202421149291.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Priority Date
- 2024-02-26
- Filing Date
- 2024-05-24
- Publication Date
- 2025-02-18
- Estimated Expiration
- 2034-05-24
AI Technical Summary
The existing support devices used for repairing aviation components can only be installed horizontally on the parts, resulting in inconvenient clamping and observation processing.
A support device including a lower mounting plate, an upper mounting plate and a hydraulic cylinder seat is designed. Through the combination of a guide frame and a clamping plate, vertical clamping of parts is realized, and the guide is adjusted by a rotating screw shaft. The spacing of the racks is suitable for parts of different specifications.
It realizes efficient vertical clamping and observation of aviation components, solves the problem of inconvenience in horizontal installation, and improves maintenance efficiency.
Smart Images

Figure CN222493935U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of auxiliary processing of aviation parts, in particular to a supporting device for repairing aviation parts. Background Art
[0002] Aviation parts mainly refer to various spare parts of aircraft, including aircraft body parts, aircraft engine parts, instruments, airborne equipment, hydraulic systems and accessories, etc. When repairing aviation parts, support devices are needed to support them, and the parts need to be clamped and fixed during maintenance;
[0003] After searching, the application with patent number CN202222390155.3 discloses a support device for repairing aviation parts, including a support table, a rotating shaft is rotatably provided on the top surface of the support table, the top of the rotating shaft is connected to a turntable, a motor 2 for driving the rotating shaft to rotate is provided in the support table, mounting seats are provided on both sides of the top surface of the turntable, an electric push rod 1 is connected to the top of the mounting seat, an end of the electric push rod is connected to the motor 1, an output shaft of the motor 1 is connected to a fixed frame, a shell is provided on both sides of the mounting seat, and the shell is connected to the top surface of the turntable;
[0004] The above application documents use various driving components to achieve the effect of horizontal placement and subsequent adjustment of parts. However, in the actual support operation of parts, the parts are generally placed horizontally, which makes subsequent observation and driving operation relatively inconvenient.
[0005] Therefore, we propose a supporting device for repairing aviation parts. Utility Model Content
[0006] In view of the deficiencies of the prior art, the utility model provides a supporting device for repairing aviation parts, which solves the problem that the prior devices can only install the parts horizontally and are not convenient for subsequent clamping and subsequent observation and processing.
[0007] To achieve the above purpose, the utility model is implemented through the following technical solutions: a support device for repairing aviation parts, comprising a lower mounting plate and an upper mounting plate above the lower mounting plate, a hydraulic cylinder seat is installed between the lower mounting plate and the upper mounting plate, and two sets of guide racks are respectively installed on the outer side walls of the lower mounting plate and the hydraulic cylinder seat;
[0008] The lower mounting plate has the same specifications as the upper mounting plate, a slide groove is provided on the outer wall of the bottom side of the lower mounting plate, and a lead screw seat located outside the outer end of the slide groove is fixedly installed on the outer wall of the bottom side of the lower mounting plate;
[0009] The main body of the guide frame is an L-shaped frame, and a slider matching the specifications of the slide groove is arranged at the outer end of the guide frame, a screw sleeve is arranged between the slider and the end of the guide frame, and a screw shaft is threadedly arranged between the screw sleeve and the screw seat;
[0010] A clamping plate is fixedly mounted on the top of the material guide frame.
[0011] Preferably, the card plate is an oblique L-shaped plate, and the card plate is an elastic sheet plate;
[0012] Among them, the setting of the shape of the pallet can clamp parts of different thicknesses between the pallet and the end of the guide rack, thereby achieving the effect of clamping and limiting parts of different specifications.
[0013] Preferably, a U-shaped plastic belt is fixedly installed between the clamping plate and the inner side wall of the top end of the material guide frame;
[0014] Among them, the U-shaped setting of the plastic belt can be set between the pallet and the parts to ensure the protective effect thereon.
[0015] Preferably, the directions of the threads in the inner grooves of the screw sleeves at the ends of the left and right groups of material guide racks on the outer walls of the lower mounting plate and the upper mounting plate are opposite;
[0016] Among them, the setting of the screw sleeves on the left and right groups of guide racks can synchronously adjust the distance between the two groups of guide racks by rotating the inner screw shaft, so as to clamp parts of different specifications accordingly according to needs.
[0017] Preferably, a sleeve column is fixedly mounted on the top end of the lower mounting plate, and a sleeve groove matching the specifications of the sleeve column is opened at a corresponding position on the bottom of the upper mounting plate;
[0018] Among them, the arrangement of the sleeve column and the sleeve groove can increase the stability of the upper mounting plate when the hydraulic cylinder seat drives the upper mounting plate to move up and down.
[0019] Preferably, the lower mounting plate and the upper mounting plate can be installed vertically or horizontally;
[0020] Among them, the two-way installation setting can assemble parts horizontally and vertically according to needs.
[0021] The utility model provides a supporting device for repairing aviation parts, which has the following beneficial effects:
[0022] 1. The support device for repairing aviation parts can set the four groups of guide racks to be vertically arranged through the arrangement of the components on the lower mounting plate and the upper mounting plate, so that the parts clamped therebetween are arranged vertically, so as to facilitate the subsequent observation and processing by the staff. With the arrangement of the upper hydraulic cylinder seat, parts of different specifications can be efficiently clamped and limited according to the needs, which solves the problem that the existing device can only install the parts horizontally, which is not convenient for subsequent clamping and subsequent observation and processing;
[0023] 2. The support device for repairing aviation parts can clamp parts of different thicknesses through the top clamping plate of the guide rack through the arrangement of the components on the lower mounting plate and the upper mounting plate. At the same time, the distance between the two sets of guide racks can be adjusted by rotating the screw shaft, thereby achieving the effect of clamping and limiting parts of different specifications according to needs. BRIEF DESCRIPTION OF THE DRAWINGS
[0024] Figure 1 It is a schematic diagram of the structure of the utility model;
[0025] Figure 2 It is a schematic diagram of the structure of the utility model from the side;
[0026] Figure 3 This is a schematic diagram of the structure of the mounting plate of the utility model;
[0027] Figure 4 It is a structural schematic diagram of the material guide rack of the utility model.
[0028] In the figure: 1. lower mounting plate; 2. upper mounting plate; 3. material guide rack; 31. clamping plate; 32. plastic tape; 33. screw sleeve; 34. slider; 4. screw shaft; 5. hydraulic cylinder seat; 6. screw seat; 7. slide groove. DETAILED DESCRIPTION
[0029] 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.
[0030] Embodiment 1:
[0031] A support device for repairing aviation parts, comprising a lower mounting plate 1 and an upper mounting plate 2 above the lower mounting plate 1, a hydraulic cylinder seat 5 is installed between the lower mounting plate 1 and the upper mounting plate 2, and two groups of guide racks 3 are respectively installed on the outer side walls of the lower mounting plate 1 and the hydraulic cylinder seat 5; the lower mounting plate 1 has the same specifications as the upper mounting plate 2, a slide groove 7 is opened on the outer wall of the bottom side of the lower mounting plate 1, and a screw seat 6 located outside the outer end of the slide groove 7 is fixedly installed on the outer wall of the bottom side of the lower mounting plate 1; the main body of the guide rack 3 is an L-shaped rack, and a slider 34 matching the specifications of the slide groove 7 is provided at the outer end of the guide rack 3, a screw sleeve 33 is provided between the slider 34 and the end of the guide rack 3, and a screw shaft 4 is threadedly sleeved between the screw sleeve 33 and the screw seat 6; a clamping plate 31 is fixedly installed at the top of the guide rack 3;
[0032] Among them, the support device for repairing aviation parts can set the four groups of guide racks 3 to be vertically set through the settings of the components on the lower mounting plate 1 and the upper mounting plate 2, so that the parts clamped therebetween are set vertically, so as to facilitate subsequent observation and processing by the staff, and with the setting of the upper hydraulic cylinder seat 5, it can perform efficient clamping and limiting of parts of different specifications according to needs, which solves the problem that the existing device can only install the parts horizontally, which is not convenient for subsequent clamping and subsequent observation and processing.
[0033] Embodiment 2:
[0034] The clamping plate 31 is an inclined L-shaped plate, and the clamping plate 31 is an elastic sheet plate; wherein, the shape of the clamping plate 31 can clamp parts of different thicknesses between the clamping plate 31 and the end of the guide frame 3, thereby achieving the effect of clamping and limiting parts of different specifications.
[0035] A U-shaped plastic tape 32 is fixedly installed between the card plate 31 and the inner side wall of the top end of the guide frame 3; wherein, the U-shaped setting of the plastic tape 32 can be set between the card plate 31 and the parts to ensure the protection effect thereon.
[0036] The directions of the threads in the inner grooves of the screw sleeves 33 at the ends of the left and right groups of guide racks 3 on the outer walls of the lower mounting plate 1 and the upper mounting plate 2 are opposite; wherein, the arrangement of the screw sleeves 33 on the left and right groups of guide racks 3 enables the rotation of the inner screw shafts 4 to synchronously adjust the spacing between the two groups of guide racks 3, so as to facilitate the corresponding clamping of parts of different specifications according to needs.
[0037] A sleeve column is fixedly installed at the top end of the lower mounting plate 1, and a sleeve groove matching the specifications of the sleeve column is opened at the corresponding position of the bottom of the upper mounting plate 2; wherein, the setting of the sleeve column and the sleeve groove can increase its stability when the hydraulic cylinder seat 5 drives the upper mounting plate 2 to move up and down.
[0038] The lower mounting plate 1 and the upper mounting plate 2 can be installed vertically or horizontally; wherein, the two-way installation setting can perform both horizontal and vertical dual assembly of components according to requirements.
[0039] Among them, the support device for repairing aviation parts, through the arrangement of various components on the lower mounting plate 1 and the upper mounting plate 2, can clamp parts of different thicknesses through the top clamping plate 31 of the guide rack 3, and at the same time, the distance between the two groups of guide racks 3 can be adjusted by rotating the screw shaft 4, so as to achieve the effect of corresponding clamping and limiting of parts of different specifications according to needs.
[0040] The working principle and use process of the utility model are as follows: when the device is needed to work, the hydraulic cylinder seat 5 is opened in advance according to the needs to adjust the distance between the lower mounting plate 1 and the upper mounting plate 2, and the upper and lower groups of screw shafts 4 are rotated to adjust the distance between the two adjacent groups of guide racks 3, and finally the parts are inserted into the inner side of the clamping plate 31 at the end of the guide rack 3, so as to achieve the effect of efficient clamping of parts of different specifications. At the same time, the parts are installed vertically to facilitate the staff to observe and subsequently process them.
[0041] 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.
[0042] 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. A support device for repairing aviation parts, characterized in that: The invention comprises a lower mounting plate (1) and an upper mounting plate (2) above the lower mounting plate (1), a hydraulic cylinder seat (5) being arranged between the lower mounting plate (1) and the upper mounting plate (2), and two groups of guide frames (3) being arranged on the outer side walls of the lower mounting plate (1) and the hydraulic cylinder seat (5); the lower mounting plate (1) and the upper mounting plate (2) have the same specifications, a slide groove (7) is arranged on the outer side wall of the bottom side of the lower mounting plate (1), and a screw seat (6) located outside the outer end of the slide groove (7) is fixedly installed on the outer side wall of the bottom side of the lower mounting plate (1); the main body of the guide frame (3) is an L-shaped frame, a slider (34) matching the specifications of the slide groove (7) is arranged at the outer end of the guide frame (3), a screw sleeve (33) is arranged between the slider (34) and the end of the guide frame (3), and a screw shaft (4) is threadedly sleeved between the screw sleeve (33) and the screw seat (6); a clamping plate (31) is fixedly installed at the top end of the guide frame (3).
2. A supporting device for repairing aviation parts according to claim 1, characterized in that: The clamping plate (31) is an oblique L-shaped plate, and the clamping plate (31) is an elastic sheet plate.
3. A supporting device for repairing aviation parts according to claim 1, characterized in that: A U-shaped plastic belt (32) is fixedly installed between the clamping plate (31) and the inner side wall of the top end of the material guide frame (3).
4. A supporting device for repairing aviation parts according to claim 1, characterized in that: The directions of the threads in the inner grooves of the lead screw sleeves (33) at the ends of the left and right groups of material guide frames (3) on the outer walls of the lower mounting plate (1) and the upper mounting plate (2) are opposite.
5. The supporting device for repairing aviation parts according to claim 1, characterized in that: A sleeve column is fixedly mounted on the top end of the lower mounting plate (1), and a sleeve groove matching the specifications of the sleeve column is provided at a corresponding position on the bottom of the upper mounting plate (2).
6. A supporting device for repairing aviation parts according to claim 1, characterized in that: The lower mounting plate (1) and the upper mounting plate (2) can be installed vertically or horizontally.
Citation Information
Patent Citations
Supporting device for maintaining aviation parts
CN218504450U