F - Mech Eng,Light,Heat,Weapons – 15 – B
Patent
F - Mech Eng,Light,Heat,Weapons
15
B
F15B 15/26 (2006.01) B64C 25/00 (2006.01) F15B 21/08 (2006.01) F16F 9/56 (2006.01) G01B 7/00 (2006.01) G01B 21/00 (2006.01)
Patent
CA 2576801
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.
La présente invention a trait à un capteur de verrou, à utiliser dans un actionneur, tel que ceux utilisés dans les trains d'atterrissage d'avion. Le capteur de verrou comprend au moins un dispositif émetteur de champ (46) fixé sur une cuve de pression d'un actionneur de blocage ; le dispositif émetteur de champ (46) surveille la position d'au moins une cible (48). Le dispositif émetteur de champ (46) émet un champ qui, lorsqu'il est rompu par la cible, envoie un signal pour indiquer que l'actionneur est verrouillé.
Ataman Gary Stephen
Coffin Mark
Schmidt Robert Kyle
Gowling Lafleur Henderson Llp
Messier-Dowty Inc.
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