Described herein is a system that includes an actuator (102) with a movable input, a first summing mechanism (106) with an input (112B), a first output, and a second output (114A, 116A). The input of the first summing mechanism is movably driven by the movable input of the actuator (102) and the first output (116A) of the first summing mechanism is movably coupled to a first actuatable element (122A). The system also includes an end mechanism (108) with an input (114B) and a first output (116B). The input of the end mechanism is movably driven by the second output (114A) and the first output of the end mechanism is movably coupled to a second actuatable element (122B). The system further includes a sensor (104) that senses a position of the rotational input of the actuator (102). A status of the first and second actuatable elements (122A, 122B) is based on a sensed position of the movable input of the actuator (102).


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    Title :

    FOLDABLE WINGTIP WITH A LOCK ACTUATION SYSTEM FOR AN AIRCRAFT


    Additional title:

    KLAPPFLÜGELSPITZE MIT EINEM VERRIEGELUNGSBETÄTIGUNGSSYSTEM FÜR EIN FLUGZEUG
    EXTREMITÉ D'AILE PLIABLE AVEC UN SYSTÈME D'ACTIONNEMENT DE VERROUILLAGE POUR AÉRONEF


    Contributors:
    GOOD MARK S (author)

    Publication date :

    2019-08-07


    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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