Horizontal supporting device for aircraft parts

Abstract

The utility model discloses an aircraft part horizontal supporting device which comprises a supporting table and a supporting plate, a ball head is arranged at the bottom of the supporting plate, a ball sleeve is arranged on the supporting table, a supporting rod and a plumb bob are arranged at the bottom of the ball head, a plurality of supporting bolts are arranged on the supporting table, moving grooves are symmetrically formed in the supporting plate, and moving blocks are arranged on the moving grooves in a sliding mode. A connecting device and a clamping frame are arranged on the moving block, the connecting device comprises a connecting block, a clamping block is rotationally arranged on the connecting block, a limiting groove is formed in the clamping block, a limiting plate and a limiting rod are slidably arranged on the limiting groove, a limiting hole is formed in the connecting block, the connecting block is connected with a plumb bob through a ball head, and under the gravity effect of the plumb bob, the supporting plate is driven to be in a horizontal state; the supporting plate is horizontally supported through the supporting bolts, then the aircraft parts are horizontally supported by the supporting plate, the position of the clamping block is fixed through cooperation of the limiting rod on the limiting plate and the limiting hole in the connecting block, and then the clamping frame and the moving block are installed.

Description

Technical Field

[0001] This utility model relates to the field of aircraft technology, and more specifically, to a horizontal support device for aircraft components. Background Technology

[0002] The aviation parts manufacturing industry mainly refers to the manufacturing of various parts and components for aircraft, including the manufacturing of aircraft fuselage components, aero-engine parts, instruments, airborne equipment, hydraulic systems and accessories, etc., but does not include parts assembly, aero-engine final assembly and complete aircraft assembly. When manufacturing aircraft parts, horizontal support is required for the parts.

[0003] In existing technologies, the operating tables for processing some aircraft parts are not easy to level and support, which can lead to increased flatness errors in the processed parts and affect the assembly accuracy of the parts. If the verticality of the operating table is insufficient, the processed holes, guide rails, etc. will not meet the design requirements, affecting the interchangeability and functionality of the parts. An uneven operating table requires frequent equipment adjustments or repositioning, wasting a lot of time. At the same time, the position of the clamping components is not convenient for installation and position adjustment, which increases the assembly time for manual adjustment and reduces work efficiency. Utility Model Content

[0004] (a) Technical problems to be solved

[0005] In view of the problems existing in the prior art, this utility model provides a horizontal support device for aircraft parts, so as to solve the technical problems mentioned in the background art, such as the inconvenience of leveling the operating table and the inconvenience of installing and adjusting the position of the clamping components.

[0006] (II) Technical Solution

[0007] To achieve the above objectives, this utility model provides the following technical solution: a horizontal support device for aircraft components, comprising a support platform and a support plate. The support plate has a ball head at its bottom, a ball sleeve on the support platform, a support rod at the bottom of the ball head, a plumb bob at the bottom of the support rod, and multiple support bolts on the support platform. The support plate has symmetrically arranged moving grooves, and a moving block is slidably arranged on the moving grooves. The moving block has a connecting device and a clamping frame. The connecting device includes a connecting block, which is disposed on the moving block. A snap-fit ​​block is rotatably arranged on the connecting block, and a limiting groove is provided on the snap-fit ​​block. A limiting plate is slidably arranged on the limiting groove, and limiting rods are symmetrically arranged on the limiting plate. The connecting block has limiting holes that cooperate with the limiting rods.

[0008] The present invention is further provided with a plurality of ball bearings rotatably disposed on the side wall of the ball sleeve, so as to facilitate the rotation of the ball head inside the ball sleeve.

[0009] The present invention is further provided that the ball sleeve is provided with fastening bolts on symmetrical threaded connections, which facilitates fixing the position of the ball sleeve and the ball head.

[0010] The present invention is further configured such that a support screw is provided on the support rod, and the support rod is threadedly connected to the ball head through the support screw, which facilitates the connection between the support rod and the ball head.

[0011] The present invention is further configured such that a moving screw is rotatably provided in the moving groove, and a moving motor is provided at one end of the moving screw. The moving screw is threadedly connected to the moving block. The moving motor drives the moving screw to rotate, thereby driving the moving block and the clamping frame to move.

[0012] The present invention is further configured such that clamping cylinders are symmetrically arranged on the clamping frame, and a clamping plate is provided at the output end of the clamping cylinder. The clamping plate is moved by the clamping cylinder, which facilitates the clamping and support of aircraft parts.

[0013] The present invention is further configured such that the clamping plate is provided with a clamping block and the clamping frame is provided with a clamping groove, thereby restricting the movement direction of the clamping plate through the cooperation of the clamping block and the clamping groove.

[0014] The present invention is further provided with a limiting spring between the limiting plate and the limiting groove, and a limiting handle is provided at one end of the limiting plate to facilitate moving the position of the limiting plate.

[0015] (III) Beneficial Effects

[0016] Compared with the prior art, this utility model provides a horizontal support device for aircraft components, which has the following advantages:

[0017] 1. The ball head and plumb bob are connected. Under the gravity of the plumb bob, the support plate is brought into a horizontal position. The relative position of the ball head and the ball sleeve is fixed by fastening bolts. The support plate is horizontally supported by the support bolts, so that the support plate is in a horizontal support position, which facilitates the horizontal support of aircraft parts.

[0018] 2. The moving screw is driven to rotate by the moving motor, which in turn moves the moving block in the moving slot to adjust the position of the clamping frame. The clamping plate is moved by the clamping cylinder to facilitate the clamping and fixing of aircraft parts.

[0019] 3. The position of the snap-fit ​​block is fixed by the engagement of the limiting rod on the limiting plate with the limiting hole on the connecting block, and the position of the clamping frame is fixed by the snap-fit ​​block, which facilitates the connection and fixation of the moving block and the clamping frame, and improves the convenience of clamping frame installation and disassembly. Attached Figure Description

[0020] Figure 1This is a schematic diagram of the overall structure of a horizontal support device for an aircraft component according to the present invention.

[0021] Figure 2 This is a cross-sectional structural diagram of the support platform and support plate in this utility model;

[0022] Figure 3 This is a schematic diagram of the cooperative structure of the support plate, the moving groove, the moving block and the moving screw in this utility model;

[0023] Figure 4 This is a schematic diagram of the cooperative structure of the clamping frame, clamping cylinder and clamping plate in this utility model;

[0024] Figure 5 This is a cross-sectional structural diagram of the connecting device in this utility model.

[0025] In the diagram: 1. Support platform; 2. Support plate; 3. Ball head; 4. Ball sleeve; 5. Support rod; 6. Plumb bob; 7. Support bolt; 8. Moving groove; 9. Moving block; 10. Clamping frame; 11. Connecting block; 12. Snap-fit ​​block; 13. Limiting groove; 14. Limiting plate; 15. Limiting rod; 16. Limiting hole; 17. Ball bearing; 18. Fastening bolt; 19. Support screw; 20. Moving screw; 21. Moving motor; 22. Clamping cylinder; 23. Clamping plate; 24. Clamping block; 25. Clamping groove; 26. Limiting spring; 27. Limiting handle. Detailed Implementation

[0026] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0027] It should be noted that, unless otherwise specified, all technical and scientific terms used in this application have the same meaning as commonly understood by one of ordinary skill in the art to which this application pertains.

[0028] In this utility model, unless otherwise stated, the orientations used, such as "up" and "down", usually refer to the direction shown in the accompanying drawings, or to the vertical, perpendicular, or gravitational direction; similarly, for ease of understanding and description, "left" and "right" usually refer to the left and right shown in the accompanying drawings; "inner" and "outer" refer to the inner and outer contours of each component itself, but the above directional terms are not used to limit this utility model.

[0029] Please see Figures 1-5A horizontal support device for aircraft components includes a support platform 1 and a support plate 2. The support plate 2 has a ball head 3 at its bottom, a ball sleeve 4 on the support platform 1, a support rod 5 at the bottom of the ball head 3, a plumb bob 6 at the bottom of the support rod 5, and multiple support bolts 7 on the support platform 1. The support plate 2 has symmetrically arranged moving grooves 8, and a moving block 9 is slidably arranged on the moving grooves 8. The moving block 9 has a connecting device and a clamping frame 10. The connecting device includes a connecting block 11, which is set on the moving block 9. A snap-fit ​​block 12 is rotatably arranged on the connecting block 11. A limiting groove 13 is provided on the snap-fit ​​block 12, and a limiting plate 14 is slidably arranged on the limiting groove 13. Limiting rods 15 are symmetrically arranged on the limiting plate 14. A limiting hole 16 that cooperates with the limiting rod 15 is provided on the connecting block 11. Multiple balls 17 are rotatably arranged on the side wall of the ball sleeve 4. Fastening bolts 18 are symmetrically threaded on the ball sleeve 4. A support screw 19 is provided on the support rod 5, and the support rod 5 is threadedly connected to the ball head 3 through the support screw 19.

[0030] In this embodiment, during the leveling of the support plate 2, the plumb bob 6 and the support rod 5 are mounted on the ball head 3 via the support screw 19, causing the ball head 3 to rotate within the ball sleeve 4. The ball bearing 17 improves the ease of rotation, adjusting the level of the support plate 2. After adjustment, the support height of the support bolt 7 is adjusted to ensure the support plate 2 is at a horizontal level. The relative positions of the ball sleeve 4 and the ball head 3 are fixed by the fastening bolt 18. The clamping frame 10 is mounted on the moving block 9 and sleeved on the connecting block 11. At this time, the limiting spring 26 is in a compressed state, and the rotation is engaged. When the limiting rod 15 on the snap-fit ​​block 12 is aligned with the limiting hole 16 of the connecting block 11, the limiting plate 14, under the elastic force of the limiting spring 26, drives the limiting rod 15 into the limiting hole 16, fixing the position of the snap-fit ​​block 12. The position of the clamping frame 10 is fixed by the snap-fit ​​block 12. When disassembling the clamping frame 10, pull the limiting handle 27 upward. The limiting handle 27 drives the limiting plate 14 to compress the limiting spring 26, causing the limiting rod 15 to leave the limiting hole 16. Rotate the snap-fit ​​block 12. When the snap-fit ​​block 12 is aligned with the connecting block 11, the clamping frame 10 can be disassembled.

[0031] Please see Figures 3-4 As one embodiment of the clamping frame 10: a moving screw 20 is rotatably provided in the moving groove 8, a moving motor 21 is provided at one end of the moving screw 20, the moving screw 20 is threadedly connected to the moving block 9, clamping cylinders 22 are symmetrically provided on the clamping frame 10, a clamping plate 23 is provided at the output end of the clamping cylinder 22, a clamping block 24 is provided on the clamping plate 23, a clamping groove 25 is provided on the clamping frame 10, a limiting spring 26 is provided between the limiting plate 14 and the limiting groove 13, and a limiting handle 27 is provided at one end of the limiting plate 14.

[0032] More specifically, when clamping aircraft parts, the moving motor 21 is started, which drives the moving screw 20 to rotate, thereby causing the moving block 9 to move in opposite directions within the moving groove 8, adjusting the position of the clamping frame 10, and activating the clamping cylinder 22. The clamping cylinder 22 drives the clamping plate 23 to clamp and fix the parts. Through the cooperation of the clamping block 24 and the clamping groove 25, the movement direction of the clamping plate 23 is restricted, improving the practicality of the clamping plate 23.

[0033] In summary, during the use or operation of the overall equipment: When leveling the support plate 2, the plumb bob 6 and support rod 5 are installed on the ball head 3 via the support screw 19, causing the ball head 3 to rotate within the ball sleeve 4. The ball bearing 17 improves the ease of rotation, adjusting the level of the support plate 2. After adjustment, the support height of the support bolt 7 is adjusted to ensure the support plate 2 is at a horizontal level. The relative positions of the ball sleeve 4 and ball head 3 are fixed by the fastening bolt 18. The clamping frame 10 is then installed on the moving block 9, and the clamping frame 10 is fitted onto the connecting block 11. At this time, the limit spring 26 is in a compressed state. Rotate the locking block 12. When the limiting rod 15 on the locking block 12 is aligned with the limiting hole 16 of the connecting block 11, the limiting plate 14, under the elastic force of the limiting spring 26, drives the limiting rod 15 into the limiting hole 16, fixing the position of the locking block 12. The position of the clamping frame 10 is fixed by the locking block 12. When disassembling the clamping frame 10, pull the limiting handle 27 upward. The limiting handle 27 drives the limiting plate 14 to compress the limiting spring 26, causing the limiting rod 15 to leave the limiting hole 16. Rotate the locking block 12. When the locking block 12 is aligned with the connecting block 11, the clamping frame 10 can be disassembled.

[0034] When clamping aircraft parts, the moving motor 21 is started, which drives the moving screw 20 to rotate, thereby causing the moving block 9 to move in opposite directions within the moving groove 8. The position of the clamping frame 10 is adjusted, and the clamping cylinder 22 is started. The clamping cylinder 22 drives the clamping plate 23 to clamp and fix the parts. Through the cooperation of the clamping block 24 and the clamping groove 25, the movement direction of the clamping plate 23 is restricted, which improves the practicality of the clamping plate 23.

[0035] In all the solutions mentioned above, the connection between two components can be selected according to the actual situation, such as welding, bolt and nut connection, bolt or screw connection, or other known connection methods, which will not be elaborated here. For all the fixed connections mentioned above, welding is preferred. Although the embodiments of this utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of this utility model. The scope of this utility model is defined by the appended claims and their equivalents.

[0036] In all the solutions mentioned above, those involving the operation of electrical components, unless otherwise specified, are controlled by a controller. Since the devices matched with the controllers are common devices, their control principles and circuit connections are existing, well-known, and mature technologies, and their electrical connection relationships and specific circuit structures will not be elaborated here.

[0037] Of all the solutions mentioned above, those involving motors can be combined with reducers if necessary. The connection structure and working principle between the motor and the reducer are existing known technologies, and this utility model will not elaborate on them.

Claims

1. An aircraft component horizontal support device comprising a support table (1) and a support plate (2), characterized in that: The bottom of the support plate (2) is provided with a ball head (3), the support table (1) is provided with a ball sleeve (4), the bottom of the ball head (3) is provided with a support rod (5), the bottom of the support rod (5) is provided with a plumb bob (6), the support table (1) is provided with a plurality of support bolts (7), the support plate (2) is provided with a plurality of moving grooves (8) symmetrically, the moving grooves (8) are provided with moving blocks (9) slidingly, the moving blocks (9) are provided with connecting devices and clamping frames (10), the connecting devices comprise connecting blocks (11), the connecting blocks (11) are arranged on the moving blocks (9), the connecting blocks (11) are provided with clamping blocks (12) rotatably, the clamping blocks (12) are provided with limiting grooves (13), the limiting grooves (13) are provided with limiting plates (14) slidingly, the limiting plates (14) are provided with limiting rods (15) symmetrically, the connecting blocks (11) are provided with limiting holes (16) matched with the limiting rods (15).

2. An aircraft component horizontal support apparatus as claimed in claim 1, wherein: The sidewall of the ball sleeve (4) is provided with a plurality of rolling balls (17) rotatably.

3. An aircraft part horizontal support apparatus as claimed in claim 1, wherein: The ball sleeve (4) is provided with fastening bolts (18) symmetrically and threadedly.

4. An aircraft part horizontal support apparatus as defined in claim 1, wherein: The support rod (5) is provided with a support screw rod (19), and the support rod (5) is threadedly connected with the ball head (3) through the support screw rod (19).

5. An aircraft part horizontal support apparatus as defined in claim 1, wherein: The moving grooves (8) are provided with moving screw rods (20) rotatably, one end of the moving screw rod (20) is provided with a moving motor (21), and the moving screw rod (20) is threadedly connected with the moving block (9).

6. An aircraft part horizontal support apparatus as defined in claim 1, wherein: The clamping frames (10) are provided with clamping cylinders (22) symmetrically, and the output ends of the clamping cylinders (22) are provided with clamping plates (23).

7. An aircraft component horizontal support apparatus as claimed in claim 6, characterised in that: The clamping plates (23) are provided with clamping blocks (24), and the clamping frames (10) are provided with clamping grooves (25).

8. An aircraft part horizontal support apparatus as defined in claim 1, wherein: Limiting springs (26) are arranged between the limiting plates (14) and the limiting grooves (13), and one end of the limiting plate (14) is provided with a limiting handle (27).

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