A method and apparatus applicable to jet engines is presented for improving operating efficiency over broad ranges of flight conditions and for reducing engine noise output in take-off and landing by controlling the airflow entering and exiting the engines. A turbojet engine apparatus is described which operates efficiently at both subsonic and supersonic speeds and a method is described which enables a turbofan with an associated satellite turbojet or turbofan to operate more efficiently at both subsonic and supersonic speeds. In both cases, take-off and landing noise is reduced substantially. The apparatus consists essentially of arranging for two separate portions of an engine to act upon one airstream or, alternately, to operate on independent airstreams.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Dual Cycle Aircraft Turbine Engine


    Beteiligte:
    M. R. Nichols (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Dual cycle aircraft turbine engine

    Nichols, M. R. | NTRS | 1977


    Dual Cycle Aircraft Turbine Engine

    M. R. Nichols | NTIS | 1973


    Turbine engine assembly and dual fuel aircraft system

    WOLLENWEBER GARY CRAIG | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft turbine engine

    SERVANT REGIS EUGENE HENRI / DESOMBRE DIDIER GABRIEL BERTRAND / JACQUEMARD CHRISTOPHE PAUL | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT TURBINE ENGINE

    SERVANT REGIS EUGENE HENRI / DESOMBRE DIDIER GABRIEL BERTRAND / JACQUEMARD CHRISTOPHE PAUL | Europäisches Patentamt | 2022

    Freier Zugriff