<p>The present invention provides a lock sensor for use in an actuator such as is used in aircraft landing gear systems. The lock sensor comprises at least one field emitting device (46) mounted on a locking actuator pressure vessel where the field emitting device (46) monitors the position of at least one target (48). The field emitting device (46) emits a field that when breached by the target sends a signal to indicate that the actuator is in a locked state.</p>
申请公布号
WO2006024145(A1)
申请公布日期
2006.03.09
申请号
WO2005CA01303
申请日期
2005.08.30
申请人
MESSIER-DOWTY INC.;ATAMAN, GARY, STEPHEN;COFFIN, MARK;SCHMIDT, ROBERT KYLE
发明人
ATAMAN, GARY, STEPHEN;COFFIN, MARK;SCHMIDT, ROBERT KYLE