An aircraft windscreen (100) includes: a main body; and a dovetail shaped portion (120) formed in the main body at a periphery thereof. Suitably, the windscreen (100) is secured within an opening (192) of an aircraft frame or body (190). In this regard, the aircraft has: a body (190) constructed of a first material and including an opening (192) therein; a windscreen (100) constructed of a second material and arranged within the opening (192) of the body (190); and a retaining member (400) attached to the body (190) and/or fuselage (300) by a set of fasteners (402) so as to secure the windscreen (100) thereto. Suitably, the retaining member (400) cooperates with the body and/or fuselage (300) to form a channel (200) in which a dovetailed shaped portion (120) formed at a periphery of the windscreen (100) is seated so as to be retained without through holes being formed in the windscreen (100).


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    Title :

    DOVETAIL AIRCRAFT WINDSCREEN


    Contributors:
    WALL JOHN (author)

    Publication date :

    2018-07-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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