An auxiliary guide assembly is disclosed. The auxiliary guide assembly including a head including a guiding surface and an overriding surface, a pinion, a hub configured to receive the pinion, a union unit configured to secure the pinion to the hub, the union unit rotationally coupled to the pinion and the head, a solenoid coupled to the hub, the solenoid configured to receive a first electric polarity, a reciprocating rod disposed through the solenoid, the reciprocating rod having a first rod end including a rack operatively coupled to the pinion, and an armature adjacent the solenoid and configured to engage the reciprocating rod, the armature moves in a first direction in response to the solenoid receiving the first electric polarity, the armature moving the reciprocating rod in the first direction, and the head rotates in a second direction in response to the reciprocating rod moving in the first direction.
LATCH SOLENOID ACTUATED FULLY AUTOMATIC AUXILIARY GUIDE ASSEMBLY
26.09.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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