The present invention relates to a thermal protection system (10) for an aircraft comprising a cockpit, the cockpit comprising a plurality of transparent surfaces (12, 14, 16), at least two transparent surfaces (14) being openable. The protection system (10) comprises: - a flexible thermal protector (22) that is able to be deployed from the cockpit via the openable transparent surfaces (14) and is configured to cover at least one transparent surface (12, 14, 16) on the outside of the aircraft and/or a front part (18) of the aircraft; - at least one securing device (14) that is able to be deployed from the cockpit via the openable transparent surfaces (14) and is configured to cooperate with an exterior surface of the aircraft in order to secure the thermal protector to the or each corresponding transparent surface (12, 14, 16) and/or to the front part (18) of the aircraft.


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    Title :

    SYSTÈME DE PROTECTION THERMIQUE POUR UN AÉRONEF, ET PROCÉDÉ DE FIXATION D'UN TEL SYSTÈME


    Additional title:

    THERMAL PROTECTION SYSTEM FOR AN AIRCRAFT, AND METHOD FOR SECURING SUCH A SYSTEM
    WÄRMESCHUTZSYSTEM FÜR EIN FLUGZEUG UND VERFAHREN ZUR SICHERUNG SOLCH EINES SYSTEMS


    Contributors:

    Publication date :

    2024-08-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    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 / B60J WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILAR DEVICES FOR VEHICLES , Fenster, Windschutzscheiben und bewegbare Dächer, Türen oder Ähnliches für Fahrzeuge



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