Title:
飛行体
Document Type and Number:
Japanese Patent JP7420110
Kind Code:
B2
Abstract:
To provide an air vehicle configured to stabilize the power output of a fuel cell by securing the generated water discharge property of the fuel cell. An air vehicle, wherein the air vehicle comprises two or more fuel cells; wherein each fuel cell comprises an anode outlet manifold; and wherein each fuel cell is disposed in the air vehicle so that water discharge directions of the anode outlet manifolds are different from each other.
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Inventors:
Hiroki Okabe
Tomohiko Kaneko
Tomohiro Shinagawa
Yoshihiro Shinozaki
Tomohiko Kaneko
Tomohiro Shinagawa
Yoshihiro Shinozaki
Application Number:
JP2021073155A
Publication Date:
January 23, 2024
Filing Date:
April 23, 2021
Export Citation:
Assignee:
Toyota Motor Corporation
International Classes:
B64D37/30; B64C29/00; B64D27/24; H01M8/00; H01M8/04537; H01M8/04746
Domestic Patent References:
| JP2020205203A | ||||
| JP2016096058A | ||||
| JP2014108723A | ||||
| JP2007157655A |
Foreign References:
| WO2020079419A1 | ||||
| CN105416596A | ||||
| US20170054163 |
Attorney, Agent or Firm:
Tatsuto Kishimoto
Akihiko Yamashita
Noriaki Yamamoto
Akihiko Yamashita
Noriaki Yamamoto
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