Title:
電気機械式アクチュエータを備える航空機操舵システム
Document Type and Number:
Japanese Patent JP6779183
Kind Code:
B2
Abstract:
An aircraft steering system (10A) includes: a first actuator (21) attached to a wing main body (11); a horn arm (13) configured to transmit an output of the first actuator (21) to a flight control surface (12); and a second actuator (22) that is a rotary actuator and attached to the flight control surface (12). At least one of the first actuator (21) and the second actuator (22) is an electromechanical actuator (EMA). A first end of the horn arm (13) is coupled to an output terminal (21a) of the first actuator (21), and a second end of the horn arm (13) is fixed to an output terminal (22a) of the second actuator (22). The second actuator (22) is attached to the flight control surface (12) such that a turning axis of the output terminal (22a) is parallel to or coincides with a fulcrum axis (hinge line) of the flight control surface (12).
Inventors:
Miyazone Kohei
Nishiyama Yoji
Hideyuki Sugiura
Nishiyama Yoji
Hideyuki Sugiura
Application Number:
JP2017139156A
Publication Date:
November 04, 2020
Filing Date:
July 18, 2017
Export Citation:
Assignee:
Kawasaki Heavy Industries, Ltd.
International Classes:
B64C13/50; F16H19/02; F16H21/12; F16H21/16
Domestic Patent References:
| JP2001074121A |
Foreign References:
| US20060255207 |
Attorney, Agent or Firm:
Patent business corporation Yuko patent office