A dual redundant actuation control system for controlling a plurality of actuators for positioning a plurality of moveable aircraft components. The actuation control system includes a component controller. The component controller includes two component control channels. Each of the plurality of actuators is electrically connected to each of the two component control channels such that either of the two component control channels may control any or all of the plurality of actuators.
申请公布号
US8583294(B2)
申请公布日期
2013.11.12
申请号
US201113083826
申请日期
2011.04.11
申请人
VILLANO WILLIAM E.;GIBBONS KEVIN;JONES TEDDY L.;RECCK FRANCIS W.;HAMILTON SUNDSTRAND CORPORATION
发明人
VILLANO WILLIAM E.;GIBBONS KEVIN;JONES TEDDY L.;RECCK FRANCIS W.