Antriebssystem, Antriebssteuerungsvorrichtung und Antriebssteuerungsprogramm

Details

Veröffentlichungs-Nr.

EP4733196

Anmeldetag

4. April 2024

Veröffentlichung

26. Dezember 2024

Rechtsraum

EP

IPC

B64D31/16, B64D27/30

Abstract

In an inverter device (80), an inverter high-voltage unit (86) is accommodated in an inverter housing (90). The inverter housing (90) includes an inverter opening portion (92) and an inverter lid portion (95). The inverter lid portion (95) covers the inverter opening portion (92) to hide the inverter high-voltage unit (86). When a control mode of a flight control device (40) is set to an interlock mode, power supply from a battery (31) to a motor (61) is cut off as the inverter lid portion (95) is opened. When the control mode is set to an interlock release mode, the power supply from the battery (31) to the motor (61) is not cut off even when the inverter lid portion (95) is opened. The control mode is set to the interlock release mode when the eVTOL (10) is in flight.

Anmelder

Firma

DENSO CORPORATION

Land

🇯🇵 Japan

Fachgebiete