A fitting for use with an ejection seat system of an aircraft includes a fitting bar configured to extend across a top of a catapult of the ejection seat system and defining an angled slot configured to receive a portion of a gas port of the ejection seat system. The fitting further includes a first leg and a second leg coupled to and extending away from the fitting bar and configured to be pivotally coupled to a smokestack structure of the ejection seat system.


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    Title :

    SPACE SAVER FITTING FOR EJECTION SEAT CATAPULT


    Contributors:

    Publication date :

    2022-03-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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