Aircraft control surface actuation systems and methods are described herein. An example control surface actuation system includes an interface cable, a test interface, and a controller. The test interface is to be disposed in an electrical equipment (EE) bay of an aircraft and operatively coupled to an actuator associated with a control surface of the aircraft. The interface cable is to be connected between the test interface and the controller, and the controller is to transmit a signal via the interface cable to the test interface to control the actuator.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft control surface actuation systems and methods


    Contributors:

    Publication date :

    2019-08-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT CONTROL SURFACE ACTUATION SYSTEMS AND METHODS

    PORTER JOHN W / BEASLEY AMBER / PARTEL PETER | European Patent Office | 2019

    Free access

    AIRCRAFT CONTROL SURFACE ACTUATION MECHANISM

    BALSIGER DERICK S | European Patent Office | 2023

    Free access

    AIRCRAFT CONTROL SURFACE ACTUATION MECHANISM

    BALSIGER DERICK S | European Patent Office | 2023

    Free access

    AIRCRAFT CONTROL SURFACE ACTUATION MECHANISM

    BALSIGER DERICK S | European Patent Office | 2023

    Free access

    SPOILER ACTUATION SYSTEMS AND METHODS FOR AIRCRAFT

    HUYNH NEAL V | European Patent Office | 2024

    Free access