Title:
電動垂直離着陸機および電動垂直離着陸機の制御装置
Document Type and Number:
Japanese Patent JP7342523
Kind Code:
B2
Abstract:
To execute a functional test of an electric drive system at an operation site of an electric vertical take and landing aircraft.SOLUTION: A control device 50 for an electric vertical takeoff and landing aircraft 100, which comprises a plurality of electric drive systems 10 having a drive motor 12 for rotationally drives a rotor 30, controls respective drive motor speeds in a symmetrical system 19 which is an electric drive system existing at a symmetrical position with respect to a test target system 18 when viewing the electric vertical takeoff and landing aircraft in a vertical direction and the test target system so as to be equal to each other, and executes balance control processing for so controlling rotation directions of respective drive motors as to be directions opposite to each other when executing a functional involving rotationally rotating the rotor with respect to the test target system which is an electric drive system, which becomes a test target, of the plurality of electric drive systems.SELECTED DRAWING: Figure 4
Inventors:
Mariko Hashimoto
Teru Iwakawa
Shun Sugita
Yuichi Takemura
Teru Iwakawa
Shun Sugita
Yuichi Takemura
Application Number:
JP2019155475A
Publication Date:
September 12, 2023
Filing Date:
August 28, 2019
Export Citation:
Assignee:
株式会社デンソー
International Classes:
B64F5/60; B64C27/72; B64C29/00; B64D27/24
Domestic Patent References:
| JP200682775A |
Foreign References:
| US20160246304 |
Attorney, Agent or Firm:
Patent Attorney Corporation Meisei International Patent Office
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