Title:
エンジン搭載自立型飛行装置
Document Type and Number:
Japanese Patent JP6707761
Kind Code:
B2
Abstract:
An autonomous flying device achieving a large payload and a long continuous flight time and also accurately adjust position and orientation while flying. The device includes: a main rotor and the like that provide main thrust; a sub rotor and the like that controls the orientation; an engine that generates energy for rotating the main rotor and the like and the sub rotor and the like; and an arithmetic control device that controls rotation of the sub rotor and the like. Also, the main rotor and the like are rotated by being drivingly connected to the engine, whereas the sub rotor and the like are rotated by motors driven by electric power generated from generator and the like operated by the engine. Further, when orientation control to tilt the fuselage is performed, the arithmetic control device increases the output distribution ratio of the sub rotor to above the output distribution ratio of the sub rotor when hovering is performed.
Inventors:
Mitsuru Ishikawa
Hidetaka Kayanuma
Hidetaka Kayanuma
Application Number:
JP2017185764A
Publication Date:
June 10, 2020
Filing Date:
September 27, 2017
Export Citation:
Assignee:
Ishikawa Energy Research Co., Ltd.
International Classes:
B64D27/24; B64C27/08; B64C39/02; F02B75/28; F02B77/00
Domestic Patent References:
| JP2017154654A | ||||
| JP2016180336A | ||||
| JP2015137092A |
Foreign References:
| WO2017035593A1 | ||||
| US20170066531 | ||||
| US20170029131 | ||||
| CN107140192A | ||||
| KR1020170018671A |
Attorney, Agent or Firm:
Yoshitaka Okada
Takashi Okada
Shimo Shigeki
Takashi Okada
Shimo Shigeki