Aviation accessory cleaning device capable of being adjusted at multiple angles
By designing a multi-angle adjustable aircraft parts cleaning device, the problem of existing devices being unable to clean thoroughly has been solved, achieving comprehensive cleaning of aircraft parts and improving their safety.
Patent Information
- Application Number
- CN202422978959.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-03
- Publication Date
- 2025-11-11
- Estimated Expiration
- 2034-12-03
AI Technical Summary
Existing aircraft parts cleaning equipment cannot fully cover all surfaces and internal crevices of the object being cleaned, resulting in compromised cleaning effectiveness.
A multi-angle adjustable aviation parts cleaning device was designed. By setting up an electric telescopic rod, a drive motor, an arc-shaped slider and a limiting component, the part carrier frame can be adjusted and fixed at multiple angles, ensuring that ultrasonic cleaning covers all surfaces.
It enables comprehensive cleaning of aircraft parts, avoids interference with the cleaning effect, and improves cleaning safety and efficiency.
Smart Images

Figure CN223530976U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of cleaning devices, specifically a multi-angle adjustable cleaning device for aviation parts. Background Technology
[0002] Aviation parts cleaning equipment generally refers to equipment used to clean various aviation materials and components. These devices need to efficiently and precisely remove dirt, grease, oxides and other contaminants to ensure the performance and safety of aviation parts. They are important devices in the production or maintenance of aviation parts. Existing aviation parts cleaning equipment is mainly based on ultrasonic cleaning devices, which can complete the cleaning of aviation parts with extremely high efficiency.
[0003] However, current cleaning devices still have some shortcomings. For example, existing cleaning devices are not convenient for multi-angle adjustment of aviation parts. Because aviation parts are often complex in shape and precise in structure, the ultrasonic waves generated by the cleaning device cannot fully cover all surfaces and internal gaps of the object being cleaned, which interferes with the cleaning effect of the device and results in certain defects in its use.
[0004] Therefore, there is an urgent need to improve this shortcoming. This utility model is to study and improve the existing structure to provide a multi-angle adjustable aviation parts cleaning device. Utility Model Content
[0005] The purpose of this invention is to provide a multi-angle adjustable aircraft parts cleaning device to solve the problems mentioned in the background art.
[0006] To achieve the above objectives, this utility model provides the following technical solution: a multi-angle adjustable aviation parts cleaning device, comprising an ultrasonic cleaning chamber and a parts carrier frame. The ultrasonic cleaning chamber has symmetrically fixedly mounted carrier plates on both sides, and an electric telescopic rod is fixedly connected to the top of the carrier plates. A connecting assembly is fixedly connected to the extended end of the electric telescopic rod, and a motor bracket is fixedly mounted on the top of the connecting assembly. A drive motor is mounted on the top of the motor bracket. The parts carrier frame is rotatably connected to the inner side of the connecting assembly, and arc-shaped sliders are symmetrically mounted on both sides of the parts carrier frame. A limit component is movably mounted on the inner surface of the parts carrier frame.
[0007] Furthermore, the connecting assembly includes a support bracket, a T-shaped slide bar, a connecting plate, and a drive shaft. The T-shaped slide bars are symmetrically installed on the left and right sides of the support bracket, and the connecting plates are symmetrically fixedly installed on the front and rear sides of the support bracket. The bottom of the connecting plate is fixedly connected to the extension end of the electric telescopic rod, and the drive shaft is rotatably connected inside the support bracket.
[0008] Furthermore, the side of the support bracket is fixedly connected to the inner side of the T-shaped slide bar, and the support bracket and the ultrasonic cleaning box form a sliding structure through the T-shaped slide bar.
[0009] Furthermore, one end of the drive shaft is fixedly connected to the outside of the accessory support frame, and the other end of the drive shaft is rotatably connected to the inside of the support bracket, and the accessory support frame and the support bracket form a rotating structure through the drive shaft.
[0010] Furthermore, the limiting component includes an L-shaped limiting frame, a threaded extension rod, a threaded connecting cylinder, a limiting telescopic rod, and a positioning mechanism. The threaded extension rod is fixedly connected to the outer side of the L-shaped limiting frame, and the threaded connecting cylinder is movably connected to the outer side of the threaded extension rod. The end of the threaded connecting cylinder is rotatably connected to the inside of the accessory support frame. Simultaneously, limiting telescopic rods are symmetrically installed on the outer side of the L-shaped limiting frame, and the positioning mechanism is movably connected to the inner surface of the L-shaped limiting frame.
[0011] Furthermore, the positioning mechanism includes a positioning plate, a connecting seat, a threaded adjusting rod, and a guide slider. The connecting seat is fixedly installed on the top of the positioning plate, and the threaded adjusting rod is rotatably connected inside the connecting seat. The side of the threaded adjusting rod is threadedly connected to the inside of the L-shaped limiting frame. Meanwhile, guide sliders are symmetrically installed on the front and rear sides of the positioning plate.
[0012] Furthermore, the side of the positioning plate is fixedly connected to the inner side of the guide slider, and the positioning plate forms a sliding structure with the L-shaped limiting structure through the guide slider.
[0013] This invention provides a multi-angle adjustable aircraft parts cleaning device, which has the following advantages:
[0014] 1. This utility model uses a fastening band to enable the drive motor to rotate the drive shaft inside the support bracket during operation. Then, with the cooperation of the arc-shaped slider, the drive shaft can rotate the accessory support frame along the inner surface of the support bracket. This achieves the purpose of multi-angle adjustment of the cleaning angle of the aviation accessories placed in the accessory support frame, thereby avoiding the situation where the ultrasonic waves generated during the operation of the cleaning device cannot fully cover all surfaces and internal gaps of the object to be cleaned, thus interfering with the cleaning effect of the cleaning device.
[0015] 2. This utility model, through the setting of a threaded extension rod and a threaded connecting cylinder, allows the threaded extension rod to extend and retract along the inside of the threaded connecting cylinder when the operator rotates the threaded connecting cylinder on the inner surface of the accessory carrier frame. This achieves the purpose of quickly adjusting the position of the L-shaped limiting frame. Then, with the cooperation of the guide slider, the positioning plate can be quickly raised and lowered along the inner surface of the L-shaped limiting frame when the operator rotates the threaded adjustment rod. This achieves the purpose of quickly fixing the aviation accessories to be cleaned, thereby avoiding the situation where the aviation accessories move and collide with the accessory carrier frame when the accessory carrier frame is rotated, thus improving the cleaning safety of the cleaning device. Attached Figure Description
[0016] Figure 1 This is a frontal three-dimensional structural diagram of a multi-angle adjustable aviation parts cleaning device according to the present invention;
[0017] Figure 2 This is a three-dimensional structural diagram of the support bracket-part support frame of the multi-angle adjustable aviation parts cleaning device of this utility model.
[0018] Figure 3 This is a three-dimensional structural diagram of the L-shaped limiting frame-positioning plate of the multi-angle adjustable aviation parts cleaning device of this utility model.
[0019] In the diagram: 1. Ultrasonic cleaning box; 2. Support plate; 3. Electric telescopic rod; 4. Connecting assembly; 41. Support bracket; 42. T-shaped slide bar; 43. Connecting plate; 44. Drive shaft; 5. Motor bracket; 6. Drive motor; 7. Accessory support frame; 8. Arc-shaped slider; 9. Limiting assembly; 91. L-shaped limit frame; 92. Threaded extension rod; 93. Threaded connecting cylinder; 94. Limiting telescopic rod; 95. Positioning mechanism; 951. Positioning plate; 952. Connecting seat; 953. Threaded adjusting rod; 954. Guide slider. Detailed Implementation
[0020] The embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are for illustrative purposes only and should not be construed as limiting the scope of this utility model.
[0021] like Figure 1 and Figure 2As shown, a multi-angle adjustable aviation parts cleaning device includes an ultrasonic cleaning chamber 1 and a parts support frame 7. Support plates 2 are symmetrically fixedly installed on both sides of the ultrasonic cleaning chamber 1, and an electric telescopic rod 3 is fixedly connected to the top of the support plate 2. A connecting assembly 4 is fixedly connected to the extended end of the electric telescopic rod 3. The connecting assembly 4 includes a support bracket 41, T-shaped slide bars 42, a connecting plate 43, and a drive shaft 44. T-shaped slide bars 42 are symmetrically installed on the left and right sides of the support bracket 41. The sides of the support bracket 41 are fixedly connected to the inner sides of the T-shaped slide bars 42. The support bracket 41 and the ultrasonic cleaning chamber 1 form a sliding structure through the T-shaped slide bars 42. This sliding structure of the support bracket 41 and the ultrasonic cleaning chamber 1 allows for smoother and more stable movement of the support bracket 41 along the inner surface of the ultrasonic cleaning chamber 1. Furthermore, the front and rear sides of the support bracket 41... A connecting plate 43 is fixedly installed, and the bottom of the connecting plate 43 is fixedly connected to the extension end of the electric telescopic rod 3. At the same time, a drive shaft 44 is rotatably connected inside the support bracket 41. The end of the drive shaft 44 is fixedly connected to the outside of the accessory support frame 7, and the other end of the drive shaft 44 is rotatably connected to the inside of the support bracket 41. The accessory support frame 7 and the support bracket 41 form a rotating structure through the drive shaft 44. By setting the accessory support frame 7 and the support bracket 41 into a rotating structure, the accessory support frame 7 can easily rotate along the inner surface of the support bracket 41 to achieve multi-angle adjustment of the aviation accessories. A motor bracket 5 is fixedly installed on the top of the connecting component 4, and a drive motor 6 is installed on the top of the motor bracket 5. The accessory support frame 7 is rotatably connected to the inside of the connecting component 4, and arc-shaped sliders 8 are symmetrically installed on both sides of the accessory support frame 7.
[0022] like Figures 1-3As shown, the ultrasonic cleaning box 1 has symmetrically fixedly installed support plates 2 on both sides, and an electric telescopic rod 3 is fixedly connected to the top of the support plate 2. The extension end of the electric telescopic rod 3 is fixedly connected to a connecting assembly 4. The accessory support frame 7 is rotatably connected to the inner side of the connecting assembly 4. Arc-shaped sliders 8 are symmetrically installed on both sides of the accessory support frame 7. A limiting assembly 9 is movably installed on the inner surface of the accessory support frame 7. The limiting assembly 9 includes an L-shaped limiting frame 91, a threaded extension rod 92, a threaded connecting cylinder 93, a limiting telescopic rod 94, and a positioning mechanism 95. The threaded extension rod 92 is fixedly connected to the outer side of the L-shaped limiting frame 91, and the threaded connecting cylinder 93 is movably connected to the outer side of the threaded extension rod 92. The end of the threaded connecting cylinder 93 is rotatably connected to the inside of the accessory support frame 7. At the same time, the limiting telescopic rods 94 are symmetrically installed on the front and rear sides of the outer side of the L-shaped limiting frame 91. A positioning mechanism 95 is movably connected to the inner surface of the L-shaped limiting frame 91. The positioning mechanism 95 includes a positioning plate 951, a connecting seat 952, a threaded adjusting rod 953, and a guide slider 954. The connecting seat 952 is fixedly installed on the top of the positioning plate 951, and the threaded adjusting rod 953 is rotatably connected inside the connecting seat 952. The side of the threaded adjusting rod 953 is threadedly connected to the inside of the L-shaped limiting frame 91. Meanwhile, the guide sliders 954 are symmetrically installed on the front and rear sides of the positioning plate 951. The side of the positioning plate 951 is fixedly connected to the inner side of the guide slider 954. The positioning plate 951 and the L-shaped limiting frame 91 form a sliding structure through the guide sliders 954. By setting the positioning plate 951 and the L-shaped limiting frame 91 into a sliding structure, the positioning plate 951 moves more smoothly and stably when it moves up and down along the inner surface of the L-shaped limiting frame 91.
[0023] In summary, this multi-angle adjustable aircraft parts cleaning device is first based on... Figures 1 to 3As shown in the diagram, the operator places the aircraft parts to be cleaned into the parts carrier frame 7, then grasps the threaded connecting cylinder 93 and rotates it inside the parts carrier frame 7, causing the threaded extension rod 92 to extend outward along the inside of the threaded connecting cylinder 93. At this time, through the connection of the limiting telescopic rod 94, the L-shaped limiting frame 91 moves from the bottom of the parts carrier frame 7 towards the center. When the inner surface of the L-shaped limiting frame 91 is in contact with the side of the aircraft parts, the rotation of the threaded connecting cylinder 93 stops. Next, the operator grasps the threaded adjusting rod 953 and rotates it inside the connecting seat 952. At this time, through the sliding of the guide slider 954, the positioning plate 951 moves downward along the inner surface of the L-shaped limiting frame 91, thereby allowing the limiting assembly 9 to automatically complete the multi-directional fixing of the aircraft parts. Then, the operator opens the electric telescopic rod 3 on the top of the carrier plate 2 through the controller. When the electric telescopic rod 3 starts to run, through the connection of the connecting plate 43 and the sliding of the T-shaped slide bar 42, the carrier bracket 41 moves along the super The inner surface of the ultrasonic cleaning chamber 1 moves downward. When the component carrier frame 7 immerses the aviation components in the cleaning fluid, the operator opens the ultrasonic cleaning chamber 1 via the controller. This allows the ultrasonic waves generated by the ultrasonic cleaning chamber 1 to automatically clean the aviation components inside the component carrier frame 7. Since the ultrasonic cleaning chamber 1 uses U or HU series ultrasonic cleaning heads, the cleaning efficiency of the ultrasonic cleaning chamber 1 is more efficient. When the operator needs to adjust the cleaning angle of the aviation components, the operator opens the drive motor 6 on the top of the motor bracket 5 via the controller. When the drive motor 6 starts running, it drives the drive shaft 44 to rotate inside the carrier bracket 41 through the fastening belt. At this time, the drive shaft 44 drives the component carrier frame 7 to rotate along the inner surface of the carrier bracket 41 through the guide sliding of the arc-shaped slider 8. This achieves the purpose of quickly adjusting the cleaning angle of the aviation components, so that the ultrasonic waves generated by the cleaning device can more comprehensively cover the aviation components inside the component carrier frame 7.
[0024] The embodiments of this utility model are given for illustrative and descriptive purposes only, and are not intended to be exhaustive or to limit the utility model to the forms disclosed. Many modifications and variations will be apparent to those skilled in the art. The embodiments were chosen and described in order to better illustrate the principles and practical applications of this utility model, and to enable those skilled in the art to understand this utility model and design various embodiments with various modifications suitable for a particular purpose.
Claims
1. A multi-angle adjustable aircraft parts cleaning device, comprising an ultrasonic cleaning chamber (1) and a parts carrier frame (7), characterized in that, The ultrasonic cleaning box (1) has a support plate (2) fixedly installed on both sides, and an electric telescopic rod (3) is fixedly connected to the top of the support plate (2). The extension end of the electric telescopic rod (3) is fixedly connected to a connecting component (4). A motor bracket (5) is fixedly installed on the top of the connecting component (4), and a drive motor (6) is installed on the top of the motor bracket (5). The accessory support frame (7) is rotatably connected to the inside of the connecting component (4). Arc-shaped sliders (8) are symmetrically installed on both sides of the accessory support frame (7), and a limit component (9) is movably installed on the inner surface of the accessory support frame (7).
2. The multi-angle adjustable aircraft parts cleaning device according to claim 1, characterized in that, The connecting assembly (4) includes a support bracket (41), a T-shaped slide bar (42), a connecting plate (43), and a drive shaft (44). The T-shaped slide bars (42) are symmetrically installed on the left and right sides of the support bracket (41), and the connecting plate (43) is symmetrically fixedly installed on the front and rear sides of the support bracket (41). The bottom of the connecting plate (43) is fixedly connected to the extension end of the electric telescopic rod (3), and the drive shaft (44) is rotatably connected inside the support bracket (41).
3. The multi-angle adjustable aircraft parts cleaning device according to claim 2, characterized in that, The side of the support bracket (41) is fixedly connected to the inner side of the T-shaped slide bar (42), and the support bracket (41) and the ultrasonic cleaning box (1) form a sliding structure through the T-shaped slide bar (42).
4. The multi-angle adjustable aircraft parts cleaning device according to claim 2, characterized in that, The end of the drive shaft (44) is fixedly connected to the outside of the accessory support frame (7), and the other end of the drive shaft (44) is rotatably connected to the inside of the support bracket (41). The accessory support frame (7) and the support bracket (41) form a rotating structure through the drive shaft (44).
5. The multi-angle adjustable aircraft parts cleaning device according to claim 1, characterized in that, The limiting component (9) includes an L-shaped limiting frame (91), a threaded extension rod (92), a threaded connecting cylinder (93), a limiting telescopic rod (94), and a positioning mechanism (95). The L-shaped limiting frame (91) is fixedly connected to the outer side of the threaded extension rod (92), and the threaded connecting cylinder (93) is movably connected to the outer side of the threaded extension rod (92). The end of the threaded connecting cylinder (93) is rotatably connected to the inside of the accessory support frame (7). At the same time, the limiting telescopic rod (94) is symmetrically installed on the outer side of the L-shaped limiting frame (91). The positioning mechanism (95) is movably connected to the inner surface of the L-shaped limiting frame (91).
6. The multi-angle adjustable aircraft parts cleaning device according to claim 5, characterized in that, The positioning mechanism (95) includes a positioning plate (951), a connecting seat (952), a threaded adjusting rod (953), and a guide slider (954). The top of the positioning plate (951) is fixedly installed with the connecting seat (952), and the threaded adjusting rod (953) is rotatably connected inside the connecting seat (952). The side of the threaded adjusting rod (953) is threadedly connected to the inside of the L-shaped limit frame (91). Meanwhile, the guide slider (954) is symmetrically installed on the front and rear sides of the positioning plate (951).
7. The multi-angle adjustable aircraft parts cleaning device according to claim 6, characterized in that, The side of the positioning plate (951) is fixedly connected to the inner side of the guide slider (954), and the positioning plate (951) and the L-shaped limit frame (91) form a sliding structure through the guide slider (954).