Title:
UNMANNED AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2023/007910
Kind Code:
A1
Abstract:
The present invention provides an unmanned aircraft with deployable wings and in which an increase in the weight of the unmanned aircraft is suppressed. Provided is an unmanned aircraft 100 comprising: an aircraft body 101; a plurality of upward-facing rotors 104A, 104B; and left and right wing sections 105 connected to the aircraft body 101, wherein the wing sections 105 can be switched between a first hanging state in which the wing sections 105 extend downward from the aircraft body 101 and a second deployed state in which the wing sections 105 extend out laterally from the aircraft body 101, and the wing sections 105 are configured to switch from the first hanging state to the second deployed state due to the force of air received when the unmanned aircraft 100 moves forward.
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Inventors:
FUKUDOME SHIGERU (JP)
OGURA SHINSUKE (JP)
OGURA SHINSUKE (JP)
Application Number:
PCT/JP2022/020517
Publication Date:
February 02, 2023
Filing Date:
May 17, 2022
Export Citation:
Assignee:
ACSL LTD (JP)
International Classes:
B64C25/22; B64C27/08; B64C27/26; B64C39/02
Domestic Patent References:
| WO2018236295A1 | 2018-12-27 |
Foreign References:
| CN110418753A | 2019-11-05 | |||
| CN107585300A | 2018-01-16 | |||
| JP2020037396A | 2020-03-12 |
Attorney, Agent or Firm:
TANAKA Shinichiro et al. (JP)
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