A propulsion system includes a source of compressed fluid, at least one thruster in fluid communication with the source, at least one turbine in fluid communication with the source and coupled to a propeller, and an apparatus for selectively providing the compressed fluid to one or both of the at least one thruster and the at least one turbine.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    COMBINATION COMPRESSED-FLUID EJECTOR AND PROPELLER PROPULSION SYSTEM


    Beteiligte:
    EVULET ANDREI (Autor:in)

    Erscheinungsdatum :

    04.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



    COMBINATION COMPRESSED-FLUID EJECTOR AND PROPELLER PROPULSION SYSTEM

    EVULET ANDREI | Europäisches Patentamt | 2021

    Freier Zugriff

    Combination compressed-fluid ejector and propeller propulsion system

    EVULET ANDREI | Europäisches Patentamt | 2020

    Freier Zugriff

    Combination Compressed-Fluid Ejector and Propeller Propulsion System

    EVULET ANDREI | Europäisches Patentamt | 2025

    Freier Zugriff

    COMBINATION COMPRESSED-FLUID EJECTOR AND PROPELLER PROPULSION SYSTEM

    EVULET ANDREI | Europäisches Patentamt | 2019

    Freier Zugriff

    COMBINATION COMPRESSED-FLUID EJECTOR AND PROPELLER PROPULSION SYSTEM

    EVULET ANDREI | Europäisches Patentamt | 2022

    Freier Zugriff