Invention Grant
- Patent Title: Flight control system and method of separating control lever linkage
- Patent Title (中): 飞行控制系统和分离控制杆联动方法
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Application No.: US12674509Application Date: 2008-06-25
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Publication No.: US08352098B2Publication Date: 2013-01-08
- Inventor: Masahiko Sataka
- Applicant: Masahiko Sataka
- Applicant Address: JP Tokyo
- Assignee: Mitsubishi Heavy Industries, Ltd.
- Current Assignee: Mitsubishi Heavy Industries, Ltd.
- Current Assignee Address: JP Tokyo
- Agency: Wenderoth, Lind & Ponack, L.L.P.
- Priority: JP2008-039342 20080220
- International Application: PCT/JP2008/061533 WO 20080625
- International Announcement: WO2009/104288 WO 20090827
- Main IPC: G05D1/00
- IPC: G05D1/00 ; G06F7/00

Abstract:
A flight control system according to the present invention includes a first sensor, a flight control computer, a link mechanism, a separation unit, and a second sensor detecting a force transmitted from the first control lever to the link mechanism. The first sensor detects a force applied from an outside to a first control lever. The flight control computer determines whether or not sticking arises in the first control lever on the basis of the force detected by the first sensor and the force detected by the second sensor, and outputs a separation command to the separation unit when determining that the sticking arises. The separation unit disconnects the link mechanism on the basis of the separation command to separate a connection between the first control lever and the second control lever.
Public/Granted literature
- US20100305780A1 FLIGHT CONTROL SYSTEM AND METHOD OF SEPARATING CONTROL LEVER LINKAGE Public/Granted day:2010-12-02
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