发明名称 Active Control Column With Manually Activated Reversion to Passive Control Column
摘要 An active control column transitionable to a fully passive state for an aircraft and methods of use are provided. The control column includes a passive feedback arrangement, a stick and a ground lock mechanism is provided. The passive feedback arrangement is moveable relative to a mechanical ground to adjust a feedback profile provided to the stick. The stick is movable relative to the mechanical ground and the passive feedback arrangement. The ground lock mechanism has a locked state in which the passive feedback arrangement is maintained in a fixed position relative to the mechanical ground. This places the control column in a fully passive state. The ground lock mechanism also has a normal state in which the passive feedback arrangement is permitted to move relative to the mechanical ground such that active feedback can be provided to the stick.
申请公布号 US2012025031(A1) 申请公布日期 2012.02.02
申请号 US20100845246 申请日期 2010.07.28
申请人 STACHNIAK DARRYL S.;RUSAK THOMAS M.;WOODWARD MPC, INC. 发明人 STACHNIAK DARRYL S.;RUSAK THOMAS M.
分类号 B64C13/04;B23P17/00 主分类号 B64C13/04
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