An assembly for an aircraft includes a variable area inlet (72) for an aircraft propulsion system (20). The variable area inlet (72) includes an inlet structure (74), an inlet door (76), an inner inlet passage (78) and an outer inlet passage (80). The inlet door (76) is configured to move outward from a closed position to an open position. The inlet door (76) is configured to close the outer inlet passage (80) when the inlet door (76) is in the closed position. The inlet door (76) is configured to open the outer inlet passage (80) when the inlet door (76) is in the open position. The inner inlet passage (78) extends into the variable area inlet (72) from a leading edge (86) of the inlet structure (74). The outer inlet passage (80) extends into the inlet structure (74) to the inner inlet passage (78).


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    Title :

    AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET


    Additional title:

    FLUGZEUGANTRIEBSSYSTEM MIT EINLASS MIT VARIABLEM BEREICH
    SYSTÈME DE PROPULSION D'AÉRONEF AVEC ENTRÉE À SECTION VARIABLE


    Contributors:

    Publication date :

    2024-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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