Auxiliary power unit inlet apparatus and methods are disclosed. An example apparatus includes an air inlet for an aircraft including a first air flow path and a second air flow path. The first air flow path is immediately adjacent the second air flow path. The first air flow path is at least partially separated from the second air flow path by a first panel. The example apparatus includes a door hingably coupled adjacent the air inlet. The door includes a second panel extending from an interior surface of the door to substantially prevent air from flowing across the interior surface between the first air flow path and the second air flow path.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Auxiliary power unit inlet apparatus and methods


    Beteiligte:
    TRETOW PAUL R (Autor:in) / CHAMBERS DAVID S (Autor:in) / WILLIE ROBERT H (Autor:in)

    Erscheinungsdatum :

    04.04.2017


    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



    Auxiliary power unit inlet apparatus and methods

    TRETOW PAUL R / CHAMBERS DAVID S / WILLIE ROBERT H | Europäisches Patentamt | 2020

    Freier Zugriff

    AUXILIARY POWER UNIT INLET APPARATUS AND METHODS

    TRETOW PAUL R / CHAMBERS DAVID S / WILLIE ROBERT H | Europäisches Patentamt | 2016

    Freier Zugriff

    AUXILIARY POWER UNIT INLET APPARATUS AND METHODS

    TRETOW PAUL R / CHAMBERS DAVID S / WILLIE ROBERT H | Europäisches Patentamt | 2017

    Freier Zugriff

    Auxiliary power unit inlet

    LIGHT STACEY H / VITALE JACK V | Europäisches Patentamt | 2020

    Freier Zugriff

    INLET SYSTEM FOR AUXILIARY POWER UNIT

    BOULDIN BRUCE / KOWAL ADAM | Europäisches Patentamt | 2024

    Freier Zugriff