Title:
CONTROL DEVICE, OPERATION MANAGEMENT SYSTEM, AND CONTROL PROGRAM
Document Type and Number:
WIPO Patent Application WO/2024/080060
Kind Code:
A1
Abstract:
A control device (60) controls flight of an eVTOL comprising: rotating blades (13) which are driven by a drive apparatus (15) and which generate a rotational lifting force; a fixed blade for generating a glide lifting force; and a lifting force adjusting mechanism for adjusting the glide lifting force. The control device (60) comprises: a rotating blade control unit (621) for adjusting the rotational lifting force by controlling the drive of the rotating blades (13); and a fixed blade control unit (622) for adjusting the glide lifting force by controlling the drive of the lifting force adjusting mechanism. If an abnormality of the drive apparatus (15) is predicted or detected when an electric powered aircraft is flying, lifting force adjustment control is executed, in which the rotating blade control unit (621) reduces the rotational lifting force and the fixed blade control unit (622) increases the glide lifting force.
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Inventors:
YOSHIDA SHUHEI (JP)
NAKAMURA MASAYA (JP)
NAKAMURA MASAYA (JP)
Application Number:
PCT/JP2023/033286
Publication Date:
April 18, 2024
Filing Date:
September 13, 2023
Export Citation:
Assignee:
DENSO CORP (JP)
International Classes:
B64C13/00; B64C27/26; B64D27/24
Foreign References:
| US20150041583A1 | 2015-02-12 | |||
| EP3828083A1 | 2021-06-02 | |||
| US4106730A | 1978-08-15 | |||
| US20170057630A1 | 2017-03-02 | |||
| US10807707B1 | 2020-10-20 | |||
| JP2003509276A | 2003-03-11 |
Attorney, Agent or Firm:
YAHAGI Kazuyuki et al. (JP)
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