Title:
SELF-CHARGING TAIL-SITTER UNMANNED AERIAL VEHICLE ADAPTED TO LAUNCHER
Document Type and Number:
WIPO Patent Application WO/2023/155498
Kind Code:
A1
Abstract:
A self-charging tail-sitter unmanned aerial vehicle adapted to a launcher. The structure of the unmanned aerial vehicle comprises: a head propeller (1), a propeller driving motor (2), foldable wings (6), a wing actuating motor (5), a fuselage (4), a rechargeable battery, and an electromagnetic induction power generation device; the head propeller (1) is located at the head end of the fuselage; the foldable wings (6) are located on the sidewall of the fuselage on two sides thereof; the propeller driving motor (2) provides a driving force for the head propeller (1); the wing actuating motor (5) provides a driving force for unfolding or folding of the foldable wings (6); the rechargeable battery provides electric energy for the propeller driving motor (2) and the wing actuating motor (5); the electromagnetic induction power generation device is used for charging the rechargeable battery.
Inventors:
CHI FENGHUA (CN)
WANG YONGHAI (CN)
CAO SU (CN)
XIAO ZHEN (CN)
LI BO (CN)
SUN JINGHUA (CN)
JI SHENXIN (CN)
ZHANG XIAONAN (CN)
GUO XIAOMING (CN)
CHEN ANHONG (CN)
YANG FEI (CN)
WANG YONGHAI (CN)
CAO SU (CN)
XIAO ZHEN (CN)
LI BO (CN)
SUN JINGHUA (CN)
JI SHENXIN (CN)
ZHANG XIAONAN (CN)
GUO XIAOMING (CN)
CHEN ANHONG (CN)
YANG FEI (CN)
Application Number:
PCT/CN2022/131303
Publication Date:
August 24, 2023
Filing Date:
November 11, 2022
Export Citation:
Assignee:
BEIJING INST OF NEARSPACE VEHICLE’S SYSTEMS ENGINEERING (CN)
International Classes:
B64C29/02; B60L53/12; B64C3/56; B64D27/24
Foreign References:
| CN114750947A | 2022-07-15 | |||
| CN112356692A | 2021-02-12 | |||
| CN205239894U | 2016-05-18 | |||
| CN112124569A | 2020-12-25 | |||
| CN204967309U | 2016-01-13 | |||
| JP2008018965A | 2008-01-31 |
Attorney, Agent or Firm:
PATENT AGENT OF CHINA AEROSPACE TECHNOLOGY (CN)
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