Inclined strut structure for transition support
The diagonal brace structure for aircraft wings addresses instability issues by using a yoke and interconnected mechanisms to stabilize angle adjustments, ensuring stable and precise wing positioning.
Patent Information
- Application Number
- CN202420751897.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-12
- Publication Date
- 2024-12-24
- Estimated Expiration
- 2034-04-12
AI Technical Summary
Existing transition brackets for aircraft wings are unstable during angle adjustments due to the tilting of the base plate, which is caused by a spring at the bottom end, leading to instability during wing installation and maintenance.
A diagonal brace structure with a yoke affixed to a base, featuring guide rails, hydraulic cylinders, universal wheels, and a mechanism of interconnected rods and screws to stabilize the adjustment process, ensuring the placement plate remains stable during angle adjustments.
The diagonal brace structure provides stable and controlled angle adjustments for aircraft wings, preventing shaking or tilting during movement, enhancing the stability and precision of wing installation and maintenance processes.
Smart Images

Figure CN222222553U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aircraft wing installation, in particular to a diagonal brace structure used for a transition bracket. Background Art
[0002] During the manufacturing and maintenance process of an aircraft, a transition bracket is needed to lift the aircraft's wings. Since the wings are installed at different angles, the angle of the wings driven by the bracket also needs to be adjusted during installation.
[0003] The existing patent document with application number 201821771166.3 provides a universal bracket for aircraft wings. The height adjustment screw of the height adjustment frame is mainly used for adjusting the height of the upper base plate, and the adjusting bolt is mainly used for adjusting different inclination angles. The utility model is suitable for supporting aircraft wings with different heights and inclination angles and has universality; although the above application has many beneficial effects, it still has the following shortcomings: when the wing is placed on the base plate, since the diagonal support part at the bottom end of the base plate is provided with a spring, the base plate of the entire bracket will tilt during the movement, which is very unstable.
[0004] Therefore, in order to solve the above problems, the utility model proposes a diagonal brace structure for a transition bracket. Summary of the invention
[0005] The purpose of the utility model is to provide a diagonal brace structure for a transition bracket to solve the problems raised in the above background technology.
[0006] The yoke is affixed to a base as claimed in claim 1, wherein the two guide rails are arranged on the upper and lower ends of the support rails and the two guide rails are rotatably connected to each other with a plurality of guide rails respectively.
[0007] Preferably, the first guide rod is slidably connected to the first hinge seat, and the linkage seat is slidably connected to the limit rod.
[0008] Preferably, a plurality of symmetrically arranged hydraulic cylinders are fixedly mounted on the top of the base, a plurality of symmetrically arranged universal wheels are provided at the bottom of the base, and the output ends of the plurality of hydraulic cylinders are fixedly connected to the bottom end of the mounting plate.
[0009] Preferably, the output end of the motor is fixedly connected to one side of the screw rod, and the screw rod is threadedly connected to the movable seat.
[0010] Preferably, the bottom end of the top rod is hinged to the second hinged seat, and the movable seat is rotatably connected to the connecting rod.
[0011] Compared with the prior art, the beneficial effects of the utility model are: a screw rod, a movable seat, a first hinged seat, a second hinged seat and a linkage seat, etc. are provided. When the angle of the placement plate needs to be adjusted, the screw rod only needs to drive the movable seat to move, and the various mechanisms will be linked. The linkage of the various mechanisms will drive the placement plate to complete the angle adjustment action. The adjustment process is very stable, and the placement plate will not shake or suddenly tilt even during the movement of the bracket. BRIEF DESCRIPTION OF THE DRAWINGS
[0012] Figure 1 This is a schematic diagram of the main structure of the utility model;
[0013] Figure 2 This is a schematic diagram of the bottom structure of the placement plate of the utility model;
[0014] Figure 3 It is a schematic diagram of the internal structure of the top rod of the utility model.
[0015] In the figure: 1. mounting plate; 2. base; 3. support plate; 4. placement plate; 5. mounting frame; 6. first guide rod; 7. first articulated seat; 8. push rod; 9. limit rod; 10. linkage seat; 11. vertical plate; 12. motor; 13. second guide rod; 14. screw rod; 15. moving seat; 16. connecting rod; 17. second articulated seat; 18. hydraulic cylinder; 19. universal wheel. DETAILED DESCRIPTION
[0016] 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.
[0017] See also Figure 1-3The utility model provides a technical solution: a diagonal brace structure for a transition bracket, including a mounting plate 1 and a base 2, the top of the mounting plate 1 is fixedly connected to a symmetrically arranged support plate 3, the two support plates 3 are rotatably connected to a placement plate 4, the bottom of the placement plate 4 is fixedly connected to a mounting frame 5, the inside of the mounting frame 5 is fixedly connected to a first guide rod 6, the inside of the mounting frame 5 is slidably connected to a first hinge seat 7, the first hinge seat 7 is hinged to a top rod 8, the inside of the top rod 8 is fixedly connected to a limit rod 9, and the inside of the top rod 8 corresponds to the position of the limit rod 9 A linkage seat 10 is slidably connected, a vertical plate 11 is fixedly connected to the top of the mounting plate 1, a motor 12 is fixedly installed on one side of the vertical plate 11, and a symmetrically arranged second guide rod 13 is fixedly connected to the other side of the vertical plate 11. A screw rod 14 is rotatably connected to the middle position of the two second guide rods 13 on one side of the vertical plate 11, and the two second guide rods 13 are slidably connected to a moving seat 15 together, a connecting rod 16 is fixedly connected to the linkage seat 10 at a position on one side of the top of the moving seat 15, and a second hinged seat 17 is fixedly connected to one side of the top of the mounting plate 1.
[0018] Furthermore, the first guide rod 6 is slidably connected to the first articulated seat 7 , and the linkage seat 10 is slidably connected to the limiting rod 9 . The first guide rod 6 is convenient for guiding the movement of the first articulated seat 7 , and the limiting rod 9 is convenient for guiding the linkage seat 10 .
[0019] Furthermore, a plurality of symmetrically arranged hydraulic cylinders 18 are fixedly mounted on the top of the base 2, a plurality of symmetrically arranged universal wheels 19 are provided at the bottom of the base 2, and the output ends of the plurality of hydraulic cylinders 18 are fixedly connected to the bottom end of the mounting plate 1, so that the hydraulic cylinders 18 can easily drive the mounting plate 1 to move upward.
[0020] Furthermore, the output end of the motor 12 is fixedly connected to one side of the screw rod 14 , and the screw rod 14 is threadedly connected to the moving seat 15 , so that the screw rod 14 can drive the moving seat 15 to move.
[0021] Furthermore, the bottom end of the top rod 8 is hinged to the second hinged seat 17 , and the movable seat 15 is rotatably connected to the connecting rod 16 , so that when the movable seat 15 moves, it is convenient to drive the linkage seat 10 to move through the connecting rod 16 .
[0022] Specifically, when using the utility model, the wing can be tied and fixed to the top of the placement plate 4. When the angle of the placement plate 4 needs to be adjusted, the motor 12 drives the screw rod 14 to rotate. The rotation of the screw rod 14 will drive the moving seat 15 to move in the direction of the top rod 8. The movement of the moving seat 15 is guided by the second guide rod 13. The movement of the moving seat 15 will act on the linkage seat 10 through the connecting rod 16. The linkage seat 10 will slide inside the top rod 8. The movement of the linkage seat 10 is guided by the limit rod 9. As the moving seat 15 moves, the top rod 8 will slowly rotate toward the top direction. The bottom end of the top rod 8 will rotate with the second hinge seat 17 as the center, and the top end of the top rod 8 will drive the first hinge seat 7 to move to one side. The movement of the first hinge seat 7 is guided by the first guide rod 6. The slow rotation and uprightness of the top rod 8 will cause the placement plate 4 to rotate and tilt with the two support plates 3 as the center.
[0023] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A diagonal brace structure for a transition bracket, characterized in that: The mounting plate (1) comprises a mounting plate (1) and a base (2), wherein the top of the mounting plate (1) is fixedly connected to a symmetrically arranged support plate (3), the two support plates (3) are rotatably connected to a placement plate (4), the bottom of the placement plate (4) is fixedly connected to a mounting frame (5), the interior of the mounting frame (5) is fixedly connected to a first guide rod (6), the interior of the mounting frame (5) is slidably connected to a first hinge seat (7), the first hinge seat (7) is hingedly connected to a top rod (8), the interior of the top rod (8) is fixedly connected to a limit rod (9), and the interior of the top rod (8) is slidably connected to a linkage seat (10) at a position corresponding to the limit rod (9). The top of the mounting plate (1) is fixedly connected to a vertical plate (11), one side of the vertical plate (11) is fixedly mounted with a motor (12), the other side of the vertical plate (11) is fixedly connected to a symmetrically arranged second guide rod (13), one side of the vertical plate (11) is rotatably connected to a screw rod (14) at a position corresponding to the middle of the two second guide rods (13), the two second guide rods (13) are slidably connected to a moving seat (15), the linkage seat (10) is fixedly connected to a connecting rod (16) at a position corresponding to the top side of the moving seat (15), and the top side of the mounting plate (1) is fixedly connected to a second hinge seat (17).
2. The diagonal brace structure for a transition bracket according to claim 1, characterized in that: The first guide rod (6) is slidably connected to the first hinge seat (7), and the linkage seat (10) is slidably connected to the limit rod (9).
3. The diagonal brace structure for a transition bracket according to claim 1, characterized in that: A plurality of symmetrically arranged hydraulic cylinders (18) are fixedly mounted on the top of the base (2), a plurality of symmetrically arranged universal wheels (19) are provided on the bottom of the base (2), and the output ends of the plurality of hydraulic cylinders (18) are fixedly connected to the bottom of the mounting plate (1).
4. The diagonal brace structure for a transition bracket according to claim 1, characterized in that: The output end of the motor (12) is fixedly connected to one side of the screw rod (14), and the screw rod (14) is threadedly connected to the moving seat (15).
5. The diagonal brace structure for a transition bracket according to claim 1, characterized in that: The bottom end of the top rod (8) is hinged to the second hinged seat (17), and the movable seat (15) is rotatably connected to the connecting rod (16).
Citation Information
Patent Citations
Universal support for aircraft wings
CN209126995U
