A system, including: a linear actuator axially arranged in a first propeller and rotatably secured thereto, a first linking mechanism connecting a rod of the linear actuator to a second propeller to change a setting of blades thereof, and including an intermediate bearing between the propellers, which is capable of transmitting translation of the rod of the linear actuator and disconnecting a rotatable link to the first propeller to make it possible to change the setting of the blades of the second propeller rotated in an opposite direction to the first propeller, and a second linking mechanism combined with blades of the first propeller to change a setting thereof.


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    Titel :

    System for changing the pitch of the contra-rotating propellers of a turboshaft engine


    Beteiligte:

    Erscheinungsdatum :

    06.11.2018


    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 / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



    System for changing the pitch of the contra-rotating propellers of a turboshaft engine

    CHARIER GILLES ALAIN / BALK WOUTER | Europäisches Patentamt | 2016

    Freier Zugriff

    Contra-rotating propellers

    Savikurki, J. | Tema Archiv | 1988


    Contra-rotating propellers

    Manen, J. D. / Sentić, A. | TIBKAT | 1956


    Contra-rotating propellers

    Taylor, J.L. | Engineering Index Backfile | 1941


    Contra-rotating propellers1

    van Manen, J.D. / Sentić, A. | IOS Press | 1956