The present invention belongs to the field of aircraft engines, and particularly, it belongs to the technical field of nacelle architecture of turbo-propeller engines. In particular, an object of the present invention is to provide an improved engine air intake of a nacelle for a turbo-propeller engine of an aircraft.


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    Title :

    NACELLE FOR TURBO-PROPELLER ENGINES


    Additional title:

    GONDEL FÜR TURBOPROPELLERMOTOREN
    NACELLE POUR TURBOPROPULSEURS


    Contributors:

    Publication date :

    2025-06-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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