Title:
【発明の名称】航空宇宙の制御と機能とのためのアクチュエータシステム
Document Type and Number:
Japanese Patent JP2003506254
Kind Code:
A
Abstract:
An actuator system (10, 100, 200) for use in an aircraft control or operating system, comprising a controller (12) operable in response to an input for generating a control signal, and an electrical actuator (20) responsive to the control signal for operating an aircraft flight control surface or other aircraft apparatus. A tab (24; 124) for aerodynamically assisting the electrical actuator is also provided in order to reduce the load on the electrical actuator in use.
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Inventors:
Atley, Andrew Edward
Chambers, Peter William
Blackwell, naijan
Weller, Bryan
Chambers, Peter William
Blackwell, naijan
Weller, Bryan
Application Number:
JP2001514189A
Publication Date:
February 18, 2003
Filing Date:
July 31, 2000
Export Citation:
Assignee:
BAE SYSTEMS plc
International Classes:
B64C9/10; B64C13/50; (IPC1-7): B64C13/50; B64C9/10
Attorney, Agent or Firm:
Takehiko Suzue (4 outside)