An assembly is provided for an aircraft propulsion system. This assembly includes a center body, a scarfed inlet structure and an inlet passage. The scarfed inlet structure extends circumferentially about the center body. The inlet passage is radially between and formed by at least the center body and the scarfed inlet structure. A first component of the assembly is configured to rotate about an axis relative to a second component of the assembly between: (A) a first position where a metering portion of the inlet passage has a first area; and (B) a second position where the metering portion has a second area. The first component is one of the center body or the scarfed inlet structure, and the second component is the other one of the center body or the scarfed inlet structure.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft propulsion system with variable area inlet assembly


    Beteiligte:

    Erscheinungsdatum :

    2023-05-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET ASSEMBLY

    GORMLEY TIMOTHY | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET ASSEMBLY

    GORMLEY TIMOTHY | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET ASSEMBLY

    GORMLEY TIMOTHY | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET

    GHANDOUR IMAD / GORMLEY TIMOTHY | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft propulsion system with variable area inlet

    GORMLEY TIMOTHY | Europäisches Patentamt | 2023

    Freier Zugriff