A variable area engine inlet of a helicopter is provided and includes first inlet portions disposed to face one another in opposite directions and at a distance from one another and second inlet portions extending between the first inlet portions and being disposed to face one another in opposite directions and at a distance from one another. The first and second inlet portions define a capture area and at least one or both of the first and second inlet portions include a movable portion disposed to occupy and move between first and second positions. The first position is associated with a non-constricted condition of the capture area and the second position is associated with a constricted condition of the capture area.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    VARIABLE GEOMETRY HELICOPTER ENGINE INLET


    Beteiligte:

    Erscheinungsdatum :

    2018-05-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Variable geometry helicopter engine inlet

    LAMB JR DONALD WILLIAM | Europäisches Patentamt | 2018

    Freier Zugriff

    Variable geometry helicopter engine inlet

    LAMB JR DONALD WILLIAM | Europäisches Patentamt | 2017

    Freier Zugriff

    Variable geometry helicopter engine inlet

    LAMB JR DONALD WILLIAM | Europäisches Patentamt | 2019

    Freier Zugriff

    Variable Engine Inlet Geometry Algorithm

    PARSONS THOMAS DEWEY | Europäisches Patentamt | 2020

    Freier Zugriff

    VARIABLE GEOMETRY ENGINE INLET FOR HIGH SPEED AIRCRAFT

    LAUDER TIMOTHY F | Europäisches Patentamt | 2021

    Freier Zugriff