CN CN214190098U

Vertical take-off and landing aircraft

Publication no.

CN214190098U
Priority date
2020-10-12
Filing date
2020-10-12
Published
2021-09-14
Granted
2021-09-14
Assignee
浙江吉利控股集团有限公司
Inventor

黄寅吉

Abstract

The utility model relates to the technical field of vertical take-off and landing aircraft, in particular to a vertical take-off and landing aircraft. The tail is arranged at the tail of the fuselage, the first wing and the second wing are respectively arranged on both sides of the fuselage; the …

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