CONTROL DEVICE OF ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT

Title:

CONTROL DEVICE OF ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT

Document Type and Number:

WIPO Patent Application WO/2021/039469

Kind Code:

A1

Abstract:

A control device (19) controls an electric drive system (10) including a drive motor (12) which is mounted in an electric vertical takeoff and landing aircraft (100) having a rotor blade (30) and which rotationally drives the rotor blade. The control device controls the electric drive system to selectively operate in one of at least two types of operating modes including a normal mode and a function testing mode. In the normal mode, the control device controls the drive motor in accordance with a command from an airframe control device (50) which controls flight of the electric vertical takeoff and landing aircraft. In the function testing mode, the control device controls the drive motor in accordance with a command transmitted from the exterior in accordance with a function testing program, or in accordance with a function testing program pre-configured in the control device itself.

More Like This:

WO/2023/060678	AIRCRAFT AND COAXIAL DUAL-ROTOR ASSEMBLY
WO/2021/039502	OPERATION CONFIRMATION DEVICE FOR ELECTRICAL VERTICAL TAKE-OFF/LANDING AIRCRAFT

Inventors:

HASHIMOTO MARIKO (JP)
IWAKAWA AKIRA (JP)
SUGITA SYUN (JP)
TAKEMURA YUUICHI (JP)

Application Number:

PCT/JP2020/031007

Publication Date:

March 04, 2021

Filing Date:

August 17, 2020

Export Citation:

Click for automatic bibliography generation Help

Assignee:

DENSO CORP (JP)

International Classes:

B64C27/22; B64C27/72; B64C29/00; B64D27/24; B64F5/60; H02P5/46

Foreign References:

US20160246304A1	2016-08-25
JP2006082775A	2006-03-30

Other References: