The invention relates to a turboprop (TP) comprising a propeller (2) comprising a blade extending in a direction (α), and which comprises a root (35), a leading edge (31), a trailing edge (32), and a wing tip (36), and an inner air stream channel (4), wherein said inner air stream channel (4) comprises an inlet (41) located at the root (35) of the blade (3) and an outlet (42) leading to the trailing edge (32) of the blade (3) and which is transversely directed in relation to the main elongation direction (α), such that an inner stream of air (51) flowing in the inner air stream channel (4) by entering via the inlet (41) adjacent to the root (35) of the blade (3) is discharged via the outlet (42) adjacent to the trailing edge (32) of the blade (3) by forming a stream of blown air (52) that moves away from the trailing edge (32) in a direction which is transverse to the main elongation direction (α) and which has a component in the direction of a skeleton line of the blade (3) at the trailing edge (32).


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    Titel :

    Turboprop



    Erscheinungsdatum :

    2017-10-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    TURBOPROP

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

    Freier Zugriff

    Turboprop

    FORESTO PAUL ANTOINE / BINDER ANTHONY / COUILLEAUX ALEXANDRE GERARD FRANCOIS et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Turboprop Operations

    George, F. | British Library Online Contents | 1996


    Turboprop troubles

    Online Contents | 2001


    Turboprop airplane

    Fox, W.W. | Engineering Index Backfile | 1952