A turboprop including a propeller including a blade extending in a direction, which also includes a root, a leading edge, a trailing edge, and a wing tip, and an inner air stream channel, wherein the inner air stream channel includes an inlet located at the root of the blade and an outlet leading to the trailing edge of the blade transversely directed in relation to the main elongation direction, such that an inner stream of air flowing in the inner air stream channel by entering via the inlet adjacent to the root of the blade is discharged via the outlet adjacent to the trailing edge of the blade by forming a stream of blown air that moves away from the trailing edge in a direction which is transverse to the main elongation direction and which has a component in the direction of a skeleton line of the blade at the trailing edge.


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    Titel :

    Turboprop



    Erscheinungsdatum :

    2019-12-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    TURBOPROP

    FORESTO PAUL ANTOINE / BINDER ANTHONY / COUILLEAUX ALEXANDRE GERARD FRANCOIS et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Turboprop

    PAUL ANTOINE FORESTO / ANTHONY BINDER / ALEXANDRE GERARD FRANCOIS COUILLEAUX et al. | Europäisches Patentamt | 2017

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    Online Contents | 2001


    Turboprop Operations

    George, F. | British Library Online Contents | 1996


    TURBOPROP TRIUMPH

    Online Contents | 2012