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Unmanned aerial vehicle

A technology of drones and airframes, applied in the field of drones, can solve problems such as poor connection stability, disconnection of the fuselage, and vibration of the functional head, so as to reduce the influence of connection stability, stabilize the connection, and improve work The effect of stability and security

Inactive Publication Date: 2019-04-12
成都纵横大鹏无人机科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The function realized by this connection method can be replaced and installed, and the connection stability is extremely poor. There is a large gap between the nose and the fuselage. Due to the influence of the mechanical power device, the functional nose of the UAV often vibrates greatly, which affects the normal operation of the functional equipment of the drone, and even disconnects from the fuselage.

Method used

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Examples

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Embodiment

[0032] Please refer to figure 1 As shown, the drone 100 provided in this embodiment includes a fuselage 110 , a power unit 120 , a functional nose 130 , side wings 140 , an empennage 150 and a rotor arm 160 . The functional nose 130 is detachably connected to one end of the fuselage 110, and the power unit 120 is arranged on the end of the fuselage 110 away from the functional nose 130. The walls are detachably attached. In this embodiment, there are also two rotor arms 160 , which are detachably connected to one wing 140 respectively, and the empennage 150 is detachably connected to the end of the fuselage 110 away from the first connecting end 111 . In this embodiment, the empennage 150 is arranged on the same side where the fuselage 110 is connected to the power plant 120. The empennage 150 includes a flat wing 151 and a vertical wing 152. The vertical wing 152 is detachably connected to the end of the fuselage 110 away from the first connecting end 111. , the flat wing 1...

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Abstract

The invention discloses an unmanned aerial vehicle and relates to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle comprises a fuselage, a power device and a functional nose, wherein the fuselage is provided with a first connecting end; a hinge seat and a plurality of lock catches are arranged on the side wall of the first connecting end; the functional nose is providedwith a second connecting end; a hinge hook and a plurality of lock hooks are arranged on the side wall of the second connecting end; the hinge hook is used for being matched with the hinge seat, so that the functional nose rotates around the hinge seat to the end wall of the second connecting end and is laminated with the end wall of the first connecting end; the lock catches are used for being detachably connected with the lock hooks; the power device is arranged at one end, away from the first connecting end, of the fuselage. The functional nose of the unmanned aerial vehicle is connected with the fuselage more stably; in addition, the influence of the power device on connection stability is reduced, and work stability and safety of the unmanned aerial vehicle are improved.

Description

technical field [0001] The present invention relates to the technical field of unmanned aerial vehicles, in particular, to an unmanned aerial vehicle. Background technique [0002] At present, the UAVs on the market are gradually becoming modularized. The UAVs are divided into multiple modules, and the modules are selectively replaced according to the specific functional purposes required. At present, the functional head and the fuselage of the UAV often adopt a plug-in connection method, and the detachable installation of the functional head is realized through the cooperation of the connector and the plug-in part. [0003] The function realized by this connection method can be replaced and installed, and the connection stability is extremely poor. There is a large gap between the nose and the fuselage. Due to the influence of the mechanical power device, the functional nose of the UAV often vibrates greatly, which affects the normal operation of the functional equipment o...

Claims

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Application Information

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IPC IPC(8): B64C1/00
CPCB64C1/00
Inventor 王利光田裕夫付鹏
Owner 成都纵横大鹏无人机科技有限公司
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