A system for monitoring for pushrod faults in an aircraft includes a pushrod; a sensor (36) mounted on the pushrod (34), the sensor (36) wirelessly transmitting measured pushrod load data; a receiver (44) receiving the measured pushrod load data; a model (42) receiving flight data and generating a modeled pushrod load profile; and a fault detector (46) comparing measured pushrod load data to the modeled pushrod load profile to detect a pushrod fault.
申请公布号
WO2011163316(A2)
申请公布日期
2011.12.29
申请号
WO2011US41374
申请日期
2011.06.22
申请人
SIKORSKY AIRCRAFT CORPORATION;ISOM, JOSHUA D.;DAVIS, MARK W.;WELSH, WILLIAM A.;MORRIS, BRIAN EDWARD;CYCON, JAMES PETER
发明人
ISOM, JOSHUA D.;DAVIS, MARK W.;WELSH, WILLIAM A.;MORRIS, BRIAN EDWARD;CYCON, JAMES PETER