A method for manufacturing a propeller reduction gear, which includes measuring manufacturing defects of the casing; calculating a first angular play induced at each intermediate gear by the measured manufacturing defects; estimating a second angular play induced at each intermediate gear by deformations of the casing when the reduction gear transmits a threshold torque; calculating a total angular play from the first angular play and the second angular play; and selecting two intermediate gears with a phase difference that compensates for the total angular play.


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    Title :

    PROCÉDÉ DE FABRICATION D'UN RÉDUCTEUR D'HÉLICE


    Additional title:

    METHOD FOR MANUFACTURING A PROPELLER REDUCTION GEAR
    VERFAHREN ZUR HERSTELLUNG EINES PROPELLERUNTERSETZUNGSGETRIEBES


    Contributors:

    Publication date :

    2018-11-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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