A method and system for generating a set of values for respective ones of a set of parameters used in determining rotor blade profiles for a corotating coaxial rotor system. The method comprises establishing a ratio of respective desired thrusts of an upper rotor and a lower rotor of the corotating coaxial rotor system based on a desired performance of the corotating coaxial rotor system; and determining the set of values of the set of parameters from the desired thrusts ratio based on an equal rotation speed condition between the upper rotor and the lower rotor of the corotating coaxial rotor system, wherein the set of parameters includes torques of the upper rotor and the lower rotor.


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    Titel :

    AERODYNAMIC OPTIMIZATION OF THE SIZING AND BLADE DESIGNS OF COROTATING COAXIAL ROTORS


    Weitere Titelangaben:

    AERODYNAMISCHE OPTIMIERUNG DER GRÖSSENBESTIMMUNG UND SCHAUFELKONSTRUKTIONEN VON GLEICHDREHENDEN KOAXIALEN ROTOREN
    OPTIMISATION AÉRODYNAMIQUE DES CONCEPTIONS DE DIMENSIONNEMENT ET DE PALE DE ROTORS COAXIAUX EN COROTATION


    Beteiligte:
    CHAN KEEN IAN (Autor:in)

    Erscheinungsdatum :

    2024-03-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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    CHAN KEEN IAN | Europäisches Patentamt | 2022

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