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An unmanned aerial vehicle whose wings are reliably connected to the fuselage

A drone and fuselage technology, applied in the field of drones, can solve problems such as troublesome installation and easy damage to wing wiring, and achieve the effects of easy installation, high reliability, and good sealing

Active Publication Date: 2018-06-22
TIANXUN INNOVATION BEIJING TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The invention aims at the problem of troublesome connection and installation of the wing and the fuselage, and easy damage to the internal wiring of the wing, and provides a UAV with reliable connection of the wing and the fuselage

Method used

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  • An unmanned aerial vehicle whose wings are reliably connected to the fuselage
  • An unmanned aerial vehicle whose wings are reliably connected to the fuselage
  • An unmanned aerial vehicle whose wings are reliably connected to the fuselage

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Embodiment Construction

[0018] In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0019] In describing the present invention, it is to be understood that the terms "radial", "axial", "upper", "lower", "top", "bottom", "inner", "outer" etc. indicate orientation Or the positional relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, and does not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation , and therefore cannot be const...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle whose wings are reliably connected to the fuselage. The plate has a first mounting hole and a second mounting hole, and the wing floor has a third mounting hole opposite to the first mounting hole and the second mounting hole; the drone also includes a steering gear mounting frame and the socket mounting frame; the steering gear mounting frame has a limit fixing part and a pin mounting part, the limit fixing part passes through the third mounting hole, and is tightly connected with the wing rib from the outside of the wing; the pin faces the fuselage fixed on the pin installation part; the socket is installed on the socket mounting frame; the socket mounting frame is tightly connected with the rib plate of the fuselage, and the socket is located in the first mounting hole; when the wing is connected to the fuselage, the pin is inserted into the socket , and the limiting and fixing part is inserted into the second mounting hole. The wing and the fuselage of the invention are connected and installed conveniently, and the wires will not be pulled when disassembled.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle whose wings are reliably connected to a fuselage. Background technique [0002] The fuselage and wings of the fixed-wing drone are separated, the power supply for the entire drone is set in the fuselage, and the steering gear is set in the wing. In order to facilitate transportation and packing, the wing and the fuselage are detachable. However, since the wires connecting the power supply in the fuselage need to pass through the wings to the wingtips, the general method is that the power supply on the fuselage side is connected with wires. Jack, the steering gear on the wing side is connected with a plug by a wire, and the connection end faces of the wing and the fuselage all have connection holes that allow the fixed carbon tube to be inserted. When connecting the fuselage to the wing, insert the wing and the fuselage from both ends o...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/06B64C1/26B64C3/18B64C11/44
CPCB64C1/064B64C1/26B64C3/187B64C11/44B64U10/25
Inventor 王川杨威马聪
Owner TIANXUN INNOVATION BEIJING TECH CO LTD