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Patent Searching and Data


Title:
AIRCRAFT STEERING SYSTEM PROVIDED WITH ELECTROMECHANICAL ACTUATOR
Document Type and Number:
WIPO Patent Application WO/2019/017325
Kind Code:
A1
Abstract:
This aircraft steering system (10A) is provided with: a first actuator (21) mounted to a wing main body (11); a horn arm (13) which transmits an output of the first actuator (21) to a steering surface (12); and a second actuator (22) which is a rotary type and mounted on the steering surface (12). At least one among the first actuator (21) and the second actuator (22) is an electromechanical actuator (EMA). The horn arm (13) has one end connected to an output end (21a) of the first actuator (21) and the other end fixed to an output end (22a) of the second actuator (22). The second actuator (22) is mounted on the steering surface (12) so that a rotation axis line of the output end (22a) is parallel or aligned with a support point axis line (a hinge line) of the steering surface (12).

Inventors:
MIYAZONO, Kohei
NISHIYAMA, Yoji
SUGIURA, Hideyuki
Application Number:
JP2018/026700
Publication Date:
January 24, 2019
Filing Date:
July 17, 2018
Export Citation:
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Assignee:
KAWASAKI JUKOGYO KABUSHIKI KAISHA (1-1 Higashikawasaki-cho 3-chome, Chuo-ku Kobe-sh, Hyogo 70, 〒6508670, JP)
International Classes:
B64C13/50; F16H19/02; F16H21/12; F16H21/16
Foreign References:
JP2001074121A2001-03-23
US20060255207A12006-11-16
Attorney, Agent or Firm:
PATENT CORPORATE BODY ARCO PATENT OFFICE (3rd Fl, Bo-eki Bldg. 123-1, Higashimachi, Chuo-ku, Kobe-sh, Hyogo 31, 〒6500031, JP)
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