Title:
UNMANNED AERIAL VEHICLE
Document Type and Number:
WIPO Patent Application WO/2019/024806
Kind Code:
A1
Abstract:
Disclosed is an unmanned aerial vehicle, comprising a fuselage (1), a shell assembly (3) and a functional component. The fuselage comprises a fuselage body (10). The shell assembly (3) is connected at a front end of the fuselage body. The functional component is mounted at a rear end of the fuselage body. An upper end face of the functional component is a first circular arc face. An upper end face of the shell assembly (3) is a second circular arc face. The first circular arc face is adjacent to the second circular arc face, and the first circular arc face and the second circular arc face constitute a streamlined curved face. Such a design can solve the problems of existing unmanned aerial vehicles having low working efficiency and consuming a large amount of energy caused by the irrational layout of the unmanned aerial vehicles.
Inventors:
XIAO DINGFENG (CN)
XU ZHIQIN (CN)
XU ZHIQIN (CN)
Application Number:
PCT/CN2018/097543
Publication Date:
February 07, 2019
Filing Date:
July 27, 2018
Export Citation:
Assignee:
GUANGZHOU XAIRCRAFT TECH CO LTD (CN)
International Classes:
B64C1/06; B64C27/08
Domestic Patent References:
| WO2016112124A2 | 2016-07-14 |
Foreign References:
| CN105752340A | 2016-07-13 | |||
| KR101727019B1 | 2017-04-14 | |||
| CN205971857U | 2017-02-22 | |||
| CN105799938A | 2016-07-27 | |||
| CN207060377U | 2018-03-02 |
Other References:
See also references of EP 3663189A4
Attorney, Agent or Firm:
KANGXIN PARTNERS, P.C. (CN)
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