Wing assembly tool for unmanned aerial vehicle

Abstract

The utility model discloses an unmanned aerial vehicle wing assembly tool which comprises a movable supporting mechanism, a lifting mechanism and an assembly platform, the lifting mechanism is arranged at the top of the supporting mechanism, and the assembly platform is installed at the top of the lifting mechanism so that the assembly platform can be driven by the lifting mechanism to move up and down. A positioning support used for supporting a wing plate and a positioning supporting plate used for placing a wing seat are arranged on the assembling platform in the first direction, the positioning support is provided with a limiting structure used for limiting relative movement of the wing plate in the second direction, and the second direction is perpendicular to the first direction. The positioning support plate is provided with a convex structure matched with the concave part structure of the wing seat, the positioning support plate is provided with an assembling through hole, and the assembling through hole is communicated with the gear mounting hole of the wing seat. The problems that existing unmanned aerial vehicle wing assembling is low in assembling efficiency and poor in assembling precision are solved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle assembly, in particular to an unmanned aerial vehicle wing assembly tool. Background Art

[0002] In the assembly of UAV wings, the wing panels and wing seats need to be assembled, and multiple gears need to be assembled to the wing seats. Due to the large number of gears and manual assembly, the assembly efficiency is low and the assembly error is large. Utility Model Content

[0003] In view of the defects existing in the above prior art, the utility model provides a UAV wing assembly tool to improve the assembly efficiency and assembly accuracy of the UAV wing assembly.

[0004] The utility model is implemented by the following technical solutions:

[0005] A wing assembly tool for an unmanned aerial vehicle comprises a movable supporting mechanism, a lifting mechanism and an assembly platform, wherein the lifting mechanism is arranged on the top of the supporting mechanism, and the assembly platform is installed on the top of the lifting mechanism so as to drive the assembly platform to move up and down through the lifting mechanism, and a positioning support for supporting a wing panel and a positioning support plate for placing a wing seat are provided on the assembly platform in a first direction, the positioning support is provided with a limiting structure for limiting the relative movement of the wing panel in a second direction, the second direction is perpendicular to the first direction, the positioning support plate is provided with a protruding structure for cooperating with a recessed structure of the wing seat, and the positioning support plate is provided with an assembly through hole, and the assembly through hole is communicated with the gear mounting hole of the wing seat.

[0006] Furthermore, the limiting structure includes: two baffles respectively arranged at both ends of the positioning support and a limiting portion arranged in the middle of the positioning support, and the limiting portion and the adjacent baffles jointly limit the relative movement of the wing panel in the second direction.

[0007] Furthermore, the upper surface of the positioning support is formed with a curved surface that matches the wing panel.

[0008] Furthermore, the positioning support includes a front positioning support arranged at the front end of the assembly platform and a rear positioning support arranged at the rear end of the assembly platform.

[0009] Furthermore, the lifting mechanism includes a lifting rod and an operating rod for driving the lifting rod to move up and down.

[0010] Furthermore, the supporting mechanism includes a supporting frame and a walking assembly arranged at the bottom of the supporting frame.

[0011] Furthermore, the walking assembly includes a support leg and a universal wheel, the support leg is arranged at the bottom of the support frame, and the universal wheel is rotatably mounted on the support leg.

[0012] Furthermore, the assembly platform is detachably connected to the top of the lifting mechanism.

[0013] Furthermore, the assembly platform is connected to the top of the lifting mechanism via fasteners.

[0014] Compared with the prior art, the beneficial effects of the present invention include at least:

[0015] The assembly platform of the utility model preliminarily positions the wing panel and the wing seat respectively by setting a positioning support and a positioning support plate, and limits the wing panel in the second direction by a limiting structure to prevent the wing panel from shifting during the assembly process. At the same time, the setting of the limiting structure can also effectively reduce the assembly error between the wing panel and the wing seat, avoiding the process of manual fine-tuning of the installation position of the wing panel, reducing labor costs, and improving assembly efficiency and assembly accuracy; the raised structure of the positioning support plate can quickly position the wing seat, and the setting of the assembly through hole facilitates the subsequent convenient installation of the wing seat gear, thereby improving assembly efficiency; when the wing assembly is completed, the assembly platform is driven by the lifting mechanism to rise to the general assembly equipment for subsequent assembly processes, without the need for manual transfer, reducing labor intensity, and having a high degree of automation, further improving assembly efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 This is a structural schematic diagram of a UAV wing assembly tooling according to an embodiment of the utility model;

[0017] Figure 2 It is a schematic diagram of assembling the wing of an embodiment of the utility model on an assembly platform;

[0018] Figure 3 It is a structural schematic diagram of an assembly platform of an embodiment of the utility model;

[0019] Figure 4 It is a structural schematic diagram of the wing of an embodiment of the utility model;

[0020] In the figure: 10, supporting mechanism; 101, supporting frame; 102, supporting leg; 103, universal wheel; 20, lifting mechanism; 201, lifting rod; 202, operating lever; 30, assembly platform; 301, front positioning support; 302, rear positioning support; 303, positioning support plate; 304, curved surface; 305, baffle; 306, limiting part; 307, raised structure; 308, assembly through hole; 309, fastener; 501, left wing panel; 502, right wing panel; 503, wing seat. DETAILED DESCRIPTION

[0021] Example embodiments will now be described more fully with reference to the accompanying drawings. However, example embodiments can be implemented in a variety of forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided to make the present invention more comprehensive and complete and to fully convey the concepts of example embodiments to those skilled in the art. The same reference numerals in the figures represent the same or similar structures, and thus their repeated description will be omitted.

[0022] The words expressing positions and directions described in the present utility model are all explained by taking the drawings as examples, but they can be changed as needed, and all the changes are included in the protection scope of the present utility model.

[0023] like Figure 1-3 As shown, the utility model provides a UAV wing assembly tool, including a movable supporting mechanism 10, a lifting mechanism 20 and an assembly platform 30, wherein the lifting mechanism 20 is arranged on the top of the supporting mechanism 10, and the assembly platform 30 is installed on the top of the lifting mechanism 20, so as to drive the assembly platform 30 to move up and down through the lifting mechanism 20, and the assembly platform 30 is provided with a positioning support for supporting the wing panel and a positioning support plate 303 for placing the wing seat 503 along a first direction, the positioning support is provided with a limiting structure for limiting the relative movement of the wing panel in a second direction, and the second direction is perpendicular to the first direction, and the positioning support plate 303 is provided with a protruding structure 307 for cooperating with the recessed structure of the wing seat 503, and the positioning support plate 303 is provided with an assembly through hole 308, and the assembly through hole 308 is connected with the gear mounting hole of the wing seat 503.

[0024] In this example, see Figure 4 The wing of the UAV includes a wing panel and a wing seat 503, wherein the wing panel includes a left wing panel 501 and a right wing panel 502, and the assembly process includes assembling and connecting the left wing panel 501, the right wing panel 502 and the wing seat 503, and installing gears on the wing seat 503. During assembly, the left wing panel 501 and the right wing panel 502 are placed on the positioning support, and the wing seat 503 is placed on the positioning support plate 303. Since the positioning support is provided with a limiting structure, on the one hand, the wing panel can be quickly positioned, and on the other hand, the wing panel can be prevented from being displaced in the second direction; the concave structure at the bottom of the wing seat 503 is combined with the convex structure 307 on the positioning support plate 303 to ensure that the wing seat 503 can be stably positioned on the positioning support plate 303, and the assembly through hole 308 on the positioning support plate 303 can facilitate the assembly of gears on the wing seat 503; after completing the assembly of the wing panel and the wing seat 503, the lifting mechanism 20 drives the assembly platform 30 to rise to the general assembly equipment for subsequent assembly.

[0025] The assembly platform 30 of the present invention preliminarily positions the wing panel and the wing seat 503 respectively by setting a positioning support and a positioning support plate 303, and limits the wing panel in the second direction by a limiting structure to prevent the wing panel from shifting during the assembly process. At the same time, the setting of the limiting structure can also effectively reduce the assembly error between the wing panel and the wing seat 503, avoiding the process of manual fine-tuning of the installation position of the wing panel, reducing labor costs, and improving assembly efficiency and assembly accuracy; the raised structure 307 of the positioning support plate 303 can quickly position the wing seat 503, and the setting of the assembly through hole 308 facilitates the subsequent convenient installation of the gear of the wing seat 503, thereby improving assembly efficiency; when the wing assembly is completed, the assembly platform 30 is driven by the lifting mechanism 20 to rise to the general assembly equipment for subsequent assembly processes, without the need for manual transfer, reducing labor intensity, and having a high degree of automation, further improving assembly efficiency.

[0026] As a preferred embodiment, the limiting structure includes: two baffles 305 respectively arranged at both ends of the positioning support and a limiting portion 306 arranged in the middle of the positioning support, and the limiting portion 306 and its adjacent baffles 305 jointly limit the relative movement of the wing panel in the second direction.

[0027] See also Figure 3 , the first direction of this embodiment is the direction indicated by X, and the second direction is the direction indicated by Y. The baffle 305 and the limiter 306 jointly limit the relative movement of the wing panel in the second direction to prevent the wing panel from shifting during the assembly process; wherein, the structure of the limiter 306 is changed accordingly according to the shape of the wing panel to limit the movement of the wing panel; preferably, the baffle 305, the limiter 306 and the positioning support are integrally formed, which has the characteristics of simple structure, simple processing, low production cost, etc.

[0028] As a preferred embodiment, the upper surface of the positioning support is formed with a curved surface 304 adapted to the wing panel. The setting of the curved surface 304 can make the wing panel and the positioning seat fit smoothly, avoid damage to the wing panel, and at the same time play a limiting role and improve the limiting effect.

[0029] As a preferred embodiment, the positioning support includes a front positioning support 301 disposed at the front end of the assembly platform 30 and a rear positioning support 302 disposed at the rear end of the assembly platform 30. Since the wing panel of this embodiment is relatively long, the front positioning support 301 and the rear positioning support 302 jointly support the wing panel, which plays a role in stably supporting the wing panel and is conducive to improving assembly accuracy.

[0030] As a preferred embodiment, the lifting mechanism 20 includes a lifting rod 201 and an operating rod 202 for driving the lifting rod 201 to lift. The lifting rod 201 of this embodiment adopts an existing scissor-type connecting rod structure, and the lifting rod 201 can be driven to perform telescopic movement by rotating the operating rod 202, which is easy to operate.

[0031] As a preferred embodiment, the support mechanism 10 includes a support frame 101 and a walking assembly disposed at the bottom of the support frame 101. The support frame 101 of this embodiment is preferably an aluminum profile structure with high strength; the walking assembly facilitates the movement of the support frame 101 and the transfer of the assembly tool.

[0032] As a preferred embodiment, the walking assembly includes a support leg 102 and a universal wheel 103, wherein the support leg 102 is arranged at the bottom of the support frame 101, and the universal wheel 103 is rotatably mounted on the support leg 102. The setting of the universal wheel 103 can change the walking direction of the support frame 101, and the movement is smoother and more labor-saving.

[0033] As a preferred embodiment, the assembly platform 30 is detachably connected to the top of the lifting mechanism 20. The assembly platform 30 is detachably connected to the lifting mechanism 20, which is convenient for disassembly at any time and has good flexibility.

[0034] As a preferred embodiment, the assembly platform 30 is connected to the top of the lifting mechanism 20 via a fastener 309. The fastener 309 of this embodiment is preferably a bolt, and of course, the fastener 309 can also be other components as long as the assembly platform 30 can be fastened to the lifting mechanism 20 and can be easily disassembled.

[0035] Although the embodiments of the present invention have been shown and described above, it is to be understood that the above embodiments are exemplary and are not to be construed as limitations on the present invention. A person skilled in the art may change, modify, substitute and modify the above embodiments within the scope of the invention without departing from the principles and purpose of the present invention. All such changes should fall within the scope of protection of the claims of the present invention.

Claims

1. A UAV wing assembly tool, characterized in that , comprising a movable supporting mechanism (10), a lifting mechanism (20) and an assembly platform (30), wherein the lifting mechanism (20) is arranged on the top of the supporting mechanism (10), and the assembly platform (30) is installed on the top of the lifting mechanism (20) so as to drive the assembly platform (30) to move up and down through the lifting mechanism (20), and the assembly platform (30) is provided with a positioning support for supporting the wing panel and a positioning support plate (303) for placing the wing seat (503) along a first direction, and the positioning support is provided with a limiting structure for limiting the relative movement of the wing panel in a second direction, and the second direction is perpendicular to the first direction, and the positioning support plate (303) is provided with a protruding structure (307) for matching with the concave structure of the wing seat (503), and the positioning support plate (303) is provided with an assembly through hole (308), and the assembly through hole (308) is connected with the gear mounting hole of the wing seat (503).

2. The UAV wing assembly tool according to claim 1, characterized in that: The limiting structure comprises: two baffles (305) respectively arranged at the two ends of the positioning support and a limiting portion (306) arranged in the middle of the positioning support, and the limiting portion (306) and the adjacent baffles (305) jointly limit the relative movement of the wing panel in the second direction.

3. The UAV wing assembly tool according to claim 2, characterized in that: The upper surface of the positioning support is formed with a curved surface (304) that matches the wing panel.

4. The UAV wing assembly tool according to claim 3, characterized in that: The positioning support comprises a front positioning support (301) arranged at the front end of the assembly platform (30) and a rear positioning support (302) arranged at the rear end of the assembly platform (30).

5. The UAV wing assembly tool according to claim 1, characterized in that: The lifting mechanism (20) comprises a lifting rod (201) and an operating rod (202) for driving the lifting rod (201) to move up and down.

6. The UAV wing assembly tool according to claim 1, characterized in that: The support mechanism (10) comprises a support frame (101) and a walking assembly arranged at the bottom of the support frame (101).

7. The UAV wing assembly tool according to claim 6, characterized in that: The walking assembly comprises a supporting leg (102) and a universal wheel (103); the supporting leg (102) is arranged at the bottom of the supporting frame (101); and the universal wheel (103) is rotatably mounted on the supporting leg (102).

8. The UAV wing assembly tool according to claim 1, characterized in that: The assembly platform (30) is detachably connected to the top of the lifting mechanism (20).

9. The UAV wing assembly tool according to claim 8, characterized in that: The assembly platform (30) is connected to the top of the lifting mechanism (20) via a fastener (309).

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