Title:
CONTROL DEVICE FOR ELECTRIC FLIGHT VEHICLE
Document Type and Number:
WIPO Patent Application WO/2023/100597
Kind Code:
A1
Abstract:
This flight control device carries out a flight-control process for causing an eVTOL to fly. The flight control device determines, in step S101 of the flight control process, whether the eVTOL is in the midst of landing. If the eVTOL is in the midst of landing, the flight control device (40) acquires, in step S102, the temperature of the drive battery as a battery temperature (Tbt). The flight control device (40) determines, in step S103, whether the battery temperature (Tbt) is lower than a takeoff-permitting temperature (TA). If the battery temperature (Tbt) is lower than the takeoff-permitting temperature (TA), the flight control device (40) proceeds to step S104 and prohibits the eVTOL from taking off. After that, the flight control device (40), in step S105, carries out a controlled temperature ramp-up. In the controlled temperature ramp-up, the temperature of the drive battery (31) is ramped up.
Inventors:
TAKEMURA YUICHI (JP)
FUKUSHI MASATO (JP)
FUKUSHI MASATO (JP)
Application Number:
PCT/JP2022/041383
Publication Date:
June 08, 2023
Filing Date:
November 07, 2022
Export Citation:
Assignee:
DENSO CORP (JP)
International Classes:
B64D27/24; B64C27/26; B64C39/02
Domestic Patent References:
| WO2020022266A1 | 2020-01-30 | |||
| WO2017206032A1 | 2017-12-07 |
Foreign References:
| JP2021090315A | 2021-06-10 | |||
| JP2020196440A | 2020-12-10 |
Attorney, Agent or Firm:
YAHAGI Kazuyuki et al. (JP)
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