An auxiliary guide assembly is disclosed. The auxiliary guide assembly including a head (212) including a guiding surface (208A, 208B) and an overriding surface, a pinion (218), a hub (214) configured to receive the pinion, a union unit (216) configured to secure the pinion to the hub, the union unit rotationally coupled to the pinion and the head, a solenoid (220) coupled to the hub, the solenoid configured to receive a first electric polarity, a reciprocating rod (222) disposed through the solenoid, the reciprocating rod having a first rod end including a rack (224) operatively coupled to the pinion, and an armature (230) 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.


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    Title :

    LATCH SOLENOID ACTUATED FULLY AUTOMATIC AUXILIARY GUIDE ASSEMBLY


    Additional title:

    VERRIEGELUNGSMAGNETBETÄTIGTE VOLLAUTOMATISCHE HILFSFÜHRUNGSANORDNUNG
    ENSEMBLE DE GUIDAGE AUXILIAIRE ENTIÈREMENT AUTOMATIQUE ACTIONNÉ PAR SOLÉNOÏDE DE VERROUILLAGE



    Publication date :

    2024-09-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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