Title:
DRONE, DRONE CONTROL METHOD, AND DRONE CONTROL PROGRAM
Document Type and Number:
WIPO Patent Application WO/2020/090879
Kind Code:
A1
Abstract:
[Problem] To provide a drone that operates using a fuel cell as a power source and can remain highly safe even during autonomous flight. [Solution] The present invention comprises: a flight control unit 21 that generates thrust by operating a propulsion device 101 that generates airflow; a fuel cell power supply 502 capable of supplying power to the flight control unit; an openable/closable reaction gas outlet 616 for discharging reaction gas to the outside of the fuel cell power supply; and a reaction gas outlet control unit 300 that controls the opening and closing of the reaction gas outlet according to the operating state of the propulsion unit.
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Inventors:
WAKE CHIHIRO (JP)
YANAGISHITA HIROSHI (JP)
YANAGISHITA HIROSHI (JP)
Application Number:
PCT/JP2019/042548
Publication Date:
May 07, 2020
Filing Date:
October 30, 2019
Export Citation:
Assignee:
NILEWORKS INC (JP)
International Classes:
B64D33/00; B64C27/08; B64C39/02; B64D27/24; H01M8/00; H01M8/04; H01M8/0662; H01M8/10
Foreign References:
| JP2017114186A | 2017-06-29 | |||
| US20170240291A1 | 2017-08-24 | |||
| US20180273194A1 | 2018-09-27 | |||
| JP2017530042A | 2017-10-12 | |||
| KR20170014295A | 2017-02-08 | |||
| JP2011023258A | 2011-02-03 |
Attorney, Agent or Firm:
KASUKAWA Toshio (JP)
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