An anterior part of a nacelle of an aircraft propulsion unit. A rigidifying frame annular about a longitudinal axis of extension of the nacelle is at the rear end of the anterior part. An annular shield is in front of the rigidifying frame and connects an internal peripheral edge of the rigidifying frame to an internal structure. The shield has a portion extending towards the external panel beyond the internal peripheral edge of the rigidifying frame, the portion forming a non-zero angle with respect to the rigidifying frame to form a free space with respect to the rigidifying frame behind the portion. The shield can thus deform in the event of an impact of a foreign object entering through the air inlet lip, without the rigidifying frame itself being deformed, thereby absorbing all or some of the impact energy. A nacelle can have such an anterior part, and an aircraft can have such a nacelle.


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    Title :

    PARTIE ANTÉRIEURE DE NACELLE D'UN ENSEMBLE PROPULSIF D AÉRONEF COMPORTANT UN BOUCLIER EN AVANT DE SON CADRE DE RIGIDIFICATION


    Additional title:

    FORWARD SECTION OF NACELLE OF AN AIRCRAFT PROPULSION ASSEMBLY COMPRISING A SHIELD IN FRONT OF ITS STIFFENING FRAME
    VORDERER TEIL DER GONDEL EINER FLUGZEUG-ANTRIEBSGRUPPE MIT EINEM SCHUTZSCHILD VOR SEINEN VERSTEIFUNGSRAHMEN


    Contributors:

    Publication date :

    2022-06-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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