Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
【発明の名称】航空機のためのフライバイワイヤーフライトコントロールシステムおよび航空機上の複数個の飛行制御翼面の位置を制御する方法
Document Type and Number:
Japanese Patent JP3384833
Kind Code:
B2
Abstract:
A redundant, multi-channel fly-by-wire control system for use in an aircraft is disclosed. The system includes a left flight control channel (60), a center flight control channel (80) and a right flight control channel (90). Each control channel is capable of flying the aircraft in the event the other two channels fail. Included within each control channel is an actuator controller electronics unit (ACE (62, 82, 92)), which transmits a series of pilot control transducer signals to a set of primary flight computers (64, 84, and 94). The primary flight computers combine the pilot control transducer signals with data obtained from an air data and inertial reference unit (145) to generate a set of flight surface commands. Each ACE selects a set of flight surface commands to control the movement of a set of flight control surfaces on the aircraft.

Inventors:
Henning booth
Application Number:
JP12863993A
Publication Date:
March 10, 2003
Filing Date:
May 31, 1993
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
The Boeing Company
International Classes:
B64C13/00; B64C13/50; G05D1/00; (IPC1-7): B64C13/50
Other References:
【文献】冨尾 武 外7名,ヘリコプタ搭載型フライ・バイ・ワイヤ(FBW)操縦システムの開発,川崎重工技報,日本,川崎重工業株式会社 明石技術研究所,1992年 4月20日,第113号,P88-P95
【文献】L.J.HARTMAN 外2名,Testing of the Advanced Digital Optical Flight Control System(ADOCS),AMERICANHELICOPTER SOCIETY 43rd Annual Forum Proceedings,米国,American Hlicopter Societry,1987年 5月18日,Volume I,P173-P188
【文献】W.L.Ballauer 外3名,Testing of the V-22 Flight Control System,AMERICAN HELICOPTER SOCIETY 46th Annual Forum Proceeding,米国,American Helicopter Society,1990年 5月21日,Volume II,P1147-P1160
Attorney, Agent or Firm:
Fukami Hisaro (3 outside)



 
Previous Patent: 両軸受リール

Next Patent: ターンオン制御回路