An approach to seeker windows for aircraft comprises a window layer comprising an IR transparent material, the window layer comprising a first side and a second side substantially opposite the first side; and a heating layer on the first side or the second side of the window layer, the heating layer configured to apply a heating profile to the window layer to reduce thermal shock imparted to the window layer when the seeker window is exposed to hypersonic flight conditions.


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    Titel :

    Aircraft seeker windows and aircraft window systems including the same


    Beteiligte:
    RISSER STEVEN M (Autor:in) / HEINTZ AMY MARIE (Autor:in) / THURSTON RACHEL M (Autor:in) / BARTHOLOMEW JOHN (Autor:in) / HOWARD ERICA (Autor:in) / RATEICK JR RICHARD G (Autor:in) / HAGGERTY IAN (Autor:in)

    Erscheinungsdatum :

    29.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / F41G Zielvorrichtungen für Waffen , WEAPON SIGHTS / H05B ELECTRIC HEATING , Elektrische Heizung



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