CN214776506U

CN214776506U - Plug mounting structure between wings of fixed-wing unmanned aerial vehicle

Info

Publication number: CN214776506U
Application number: CN202120410249.5U
Authority: CN
Inventors: 陶大俊; 刘克鹏; 王冬李; 王鹏
Original assignee: Wuhu Chuanglian Aviation Equipment Industry Research Institute Co ltd
Current assignee: Wuhu Chuanglian Aviation Equipment Industry Research Institute Co ltd
Priority date: 2021-02-25
Filing date: 2021-02-25
Publication date: 2021-11-19
Anticipated expiration: 2031-02-25

Abstract

The utility model discloses a plug mounting structure between fixed wing unmanned aerial vehicle wing, including unmanned aerial vehicle body link, wing body, the inside fixed symmetry erection bracing piece of unmanned aerial vehicle body link, one side fixed mounting drive structure of bracing piece, one side of drive structure is equipped with connection structure, fixed mounting fixed knot constructs on the connection structure, the utility model discloses a connection structure is connected wing body and unmanned aerial vehicle body link, fixes the coupling part through fixed knot structure, prevents that the wing from droing, drives through the drive structure, realizes the erection joint of plug.

Description

Plug mounting structure between wings of fixed-wing unmanned aerial vehicle

Technical Field

The utility model relates to a plug mounting structure, especially a plug mounting structure between fixed wing unmanned aerial vehicle wing.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

The existing fixed-wing unmanned aerial vehicle has the advantages that the wing size is large, the wing is not beneficial to storage and carrying, and the wing needs to be disassembled, so that the inter-wing plug mounting structure of the fixed-wing unmanned aerial vehicle is designed, and the wing is convenient to disassemble and install.

SUMMERY OF THE UTILITY MODEL

The to-be-solved technical problem of the utility model

An object of the utility model is to provide a plug mounting structure between fixed wing unmanned aerial vehicle wing to solve the problem that proposes in the above-mentioned background art, current fixed wing unmanned aerial vehicle's wing size is great, is unfavorable for accomodating and carrying, needs dismantle, has consequently designed a plug mounting structure between fixed wing unmanned aerial vehicle wing, is convenient for dismantle the installation.

Technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a plug mounting structure between fixed wing unmanned aerial vehicle wing, includes unmanned aerial vehicle body link, wing body, the inside fixed symmetry installation bracing piece of unmanned aerial vehicle body link and wing body, one side fixed mounting drive structure of bracing piece, one side of drive structure is equipped with connection structure, the last fixed mounting fixed knot of connection structure constructs.

Preferably, the driving structure comprises a first supporting plate, the first supporting plate is fixedly arranged at one side of the two supporting rods, one end of the electric telescopic rods is symmetrically and fixedly arranged at one side of the first supporting plate, and the other end of each electric telescopic rod is provided with a connecting structure.

Preferably, connection structure includes first spliced pole, first spliced pole fixed mounting be in electric telescopic handle's one end, the one end of first nut of screwed connection on the first spliced pole, the other end screwed connection second spliced pole of first nut, one side fixed mounting second backup pad of second spliced pole, the one side symmetry fixed mounting of second backup pad the bracing piece.

Preferably, fixed knot constructs including first fixed plate and second fixed plate, first fixed plate fixed mounting in the outer wall of first spliced pole, second fixed plate fixed mounting in the outer wall of second spliced pole, first fixed plate with the matching is equipped with a plurality of spiral holes on the second fixed plate, first fixed plate pass through screw and second nut with the second fixed plate is connected.

Preferably, a socket is fixedly arranged in the center of one side of the first supporting plate in a penetrating mode, a plug is fixedly arranged in the center of one side of the second supporting plate in a penetrating mode, and the plug is matched with the socket.

Advantageous effects

Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses a connection structure is connected the wing body with unmanned aerial vehicle body link, fixes coupling part through fixed knot structure, prevents that the wing from droing, drives through drive structure, realizes the demountable installation of plug and connects.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of the driving structure of the present invention;

fig. 3 is a schematic view of the connection structure and the fixing structure of the present invention.

In the figure: 1. the unmanned aerial vehicle body is connected with the end; 2. a wing body; 3. a support bar; 4. a drive structure; 41. a first support plate; 42. an electric telescopic rod; 5. a connecting structure; 51. a first connecting column; 52. a first nut; 53. a second support plate; 6. a fixed structure; 61. a first fixing plate; 62. a second fixing plate; 7. a socket; 8. and (4) a plug.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative efforts belong to the protection scope of the present invention.

In an embodiment, please refer to fig. 1-3, the present invention provides a technical solution: the utility model provides a plug mounting structure between fixed wing unmanned aerial vehicle wing, includes unmanned aerial vehicle body link 1, wing body 2, the inside fixed symmetry erection bracing piece 3 of unmanned aerial vehicle body link 1 and wing body 2, one side fixed mounting drive structure 4 of bracing piece 3, one side of drive structure 4 is equipped with connection structure 5, fixed mounting fixed knot constructs 6 on the connection structure 5.

In an embodiment, referring to fig. 2, the driving structure 4 includes a first supporting plate 41, the first supporting plate 41 is fixedly installed at one side of the two supporting rods 3, one side of the first supporting plate 41 is fixedly and symmetrically installed at one end of an electric telescopic rod 42, and the other end of each electric telescopic rod 42 is installed at a connecting structure 5.

In an embodiment, referring to fig. 2-3, the connecting structure 5 includes a first connecting column 51, the first connecting column 51 is fixedly installed at one end of the electric telescopic rod 42, the first connecting column 51 is spirally connected with one end of a first nut 52, the other end of the first nut 52 is spirally connected with a second connecting column, a second supporting plate 53 is fixedly installed at one side of the second connecting column, and the supporting rods 3 are symmetrically and fixedly installed at one side of the second supporting plate 53.

In an embodiment, referring to fig. 3, the fixing structure 6 includes a first fixing plate 61 and a second fixing plate 62, the first fixing plate 61 is fixedly installed on an outer wall of the first connecting column 51, the second fixing plate 62 is fixedly installed on an outer wall of the second connecting column, a plurality of spiral holes are formed in the first fixing plate 61 and the second fixing plate 62 in a matching manner, the first fixing plate 61 is connected with the second fixing plate 62 through a screw and a second nut, and the fixing structure 6 is used for fixing the first connecting column 51 after being connected with the second connecting column in a spiral manner.

In an embodiment, referring to fig. 2, a socket 7 is fixedly installed in the center of one side of the first support plate 41, a plug 8 is fixedly installed in the center of one side of the second support plate 53, the plug 8 is matched with the socket 7, and the plug 8 is moved toward the socket 7 by driving the electric telescopic rod 42 until connection.

The working principle is as follows: the utility model discloses a first nut 52 carries out screwed connection with first spliced pole 51 and second spliced pole, and the rethread screw is connected first fixed plate 61 and second fixed plate 62 with the nut, fixes, places wing body 2 and drops, then drives wing body 2 through control electric telescopic handle 42 and removes, is connected with socket 8 up to plug 7.

The above description is only for the specific embodiments of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art can easily think of the changes or substitutions within the technical scope of the present invention, and all should fall within the protection scope of the present invention.

Claims

1. The utility model provides a plug mounting structure between fixed wing unmanned aerial vehicle wing, includes unmanned aerial vehicle body link (1), wing body (2), its characterized in that: the utility model discloses an unmanned aerial vehicle wing, including unmanned aerial vehicle body link (1) and the inside fixed symmetry erection bracing piece (3) of wing body (2), one side fixed mounting drive structure (4) of bracing piece (3), one side of drive structure (4) is equipped with connection structure (5), fixed mounting fixed knot constructs (6) on connection structure (5).

2. The wing plug mounting structure of a fixed wing drone of claim 1, wherein: drive structure (4) are including first backup pad (41), first backup pad (41) fixed mounting is two one side of bracing piece (3), the one end of one side fixed symmetry installation electric telescopic handle (42) of first backup pad (41), every other end installation connection structure (5) of electric telescopic handle (42).

3. The wing plug mounting structure of a fixed wing drone of claim 2, wherein: connection structure (5) include first spliced pole (51), first spliced pole (51) fixed mounting be in the one end of electric telescopic handle (42), the one end of first nut (52) of screwed connection is gone up in first spliced pole (51), the other end screwed connection second spliced pole of first nut (52), one side fixed mounting second backup pad (53) of second spliced pole, the one side symmetry fixed mounting of second backup pad (53) bracing piece (3).

4. The wing plug mounting structure of a fixed wing drone of claim 3, wherein: fixed knot constructs (6) including first fixed plate (61) and second fixed plate (62), first fixed plate (61) fixed mounting be in the outer wall of first spliced pole (51), second fixed plate (62) fixed mounting be in the outer wall of second spliced pole, first fixed plate (61) with the matching is equipped with a plurality of spiral holes on second fixed plate (62), first fixed plate (61) pass through screw and second nut with second fixed plate (62) are connected.

5. The wing plug mounting structure of a fixed wing drone of claim 4, wherein: the fixed installation socket (7) that runs through in one side center of first backup pad (41), the fixed installation plug (8) that runs through in one side center of second backup pad (53), plug (8) with socket (7) phase-match.