FUSELAGE OF UNMANNED AERIAL VEHICLE AND UNMANNED AERIAL VEHICLE

WIPO Patent Application WO/2018/152911

A1

An unmanned aerial vehicle (100) and a fuselage (10), the fuselage (10) comprising an upper shell (11) and a lower shell (12). The upper shell (11) comprises an upper shell groove (112) arranged at the periphery of the upper shell (11), the lower shell (12) may match the upper shell (11), and the lower shell (12) comprises a lug (122) arranged at the periphery of the lower shell (12). When the lower shell (12) is matched with the upper shell (11), the lug (122) may extend into the upper shell groove (112) to match therewith. The unmanned aerial vehicle (100) comprises a fuselage (10) and a plurality of machine arms (30). The plurality of machine arms (30) are fixedly connected to the fuselage (10) and are radially arranged outwards from the fuselage (10). When the lower shell (12) is matched with the upper shell (11), the lug (122) may extend into the upper shell groove (112) to be matched therewith. In practical use, water droplets may be prevented from entering the fuselage (10) from the matching gap between the lower shell (12) and the upper shell (11), thus enhancing the protective performance of the fuselage (10).

ZHANG YONGSHENG (CN)
QIU LI (CN)
CHEN XIANGYU (CN)
LIU YUCHENG (CN)
LIANG GUIBIN (CN)

PCT/CN2017/077744

August 30, 2018

March 22, 2017

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SZ DJI TECHNOLOGY CO LTD (CN)

B64C1/00

CN105799909A	2016-07-27
CN106081052A	2016-11-09
CN205524925U	2016-08-31
US20120267472A1	2012-10-25
CN205738053U	2016-11-30

SHENZHEN SCIENBIZIP INTELLECTUAL PROPERTY AGENCY CO.,LTD. (CN)

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