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Title:
重量移動式同軸回転翼ヘリコプタ
Document Type and Number:
Japanese Patent JP7316977
Kind Code:
B2
Abstract:
A helicopter (100) includes a propulsion system (110), gimbal assembly (160), and a controller (182). The propulsion system (110) includes a first rotor assembly (115a) and a second rotor assembly (115b). The first rotor assembly (115a) comprises a first motor (120a) coupled to a first rotor (130a) and the second rotor assembly (115b) comprises a second motor (120b) coupled to a second rotor (130b). The second rotor (130b) is coaxial to the first rotor (130a) and is configured to be counter-rotating to the first rotor (130a). The gimbal assembly (160) couples a fuselage (180) of the helicopter (100) to the propulsion system (110). The controller (182) is communicably coupled to the gimbal assembly (160) and is configured to provide instructions to the gimbal assembly (160) in order to weight-shift the fuselage (180) of the helicopter (100), thereby controlling movements of the helicopter (100).

Inventors:
Dustin Eli Gamble
Application Number:
JP2020100694A
Publication Date:
July 28, 2023
Filing Date:
June 10, 2020
Export Citation:
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Assignee:
LOCKHEED MARTIN CORPORATION
International Classes:
B64C17/04; B64C25/34; B64C25/54; B64C25/64; B64C25/66; B64C27/10; B64C27/26
Domestic Patent References:
JP2015520697A
Attorney, Agent or Firm:
Shinichiro Tanaka
Hiroyuki Suda
Ichiro Kurasawa
Yasushi Yamamoto
Hiroko Suzuki
Fumitaka Tamaki