The invention provides a high-altitude propeller rapid iterative generation method. The method comprises the steps of: 1, determining the diameter of a propeller; 2, determining the width and the thickness of a propeller blade; 3, selecting a high-altitude propeller airfoil; 4, determining the number of blades of the high-altitude propeller; 5, determining the torsion angle of the propeller blade;and 6, determining final parameters of the propeller. According to the invention, research is carried out for characteristics of high-altitude propellers, on the basis of analyzing the influence of each design parameter of the propeller on the performance of the propeller, the environmental factor of a 20km height stratosphere is combined to serve as a variable directly related to the Mach numberof the propeller tip and the local sound velocity, and the rapid and effective method for generating the high-altitude propeller is provided based on a propeller lath theory.

    本发明提出一种高空螺旋桨快速迭代生成方法,其包括步骤:第一步:确定螺旋桨直径;第二步:确定螺旋桨桨叶宽度与桨叶厚度;第三步:选取高空螺旋桨翼型;第四步:确定高空螺旋桨桨叶数;第五步:确定螺旋桨桨叶扭转角;第六步:确定螺旋桨最终参数。本发明针对高空螺旋桨的特性展开研究,在分析螺旋桨各设计参数对螺旋桨性能影响的基础上,结合20km高度平流层的环境因素,将作为一个直接相关于桨尖马赫数与当地声速的变量,基于螺旋桨片条理论,提出一种快速有效的高空螺旋桨的生成方法。


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    Titel :

    High-altitude propeller rapid iterative generation method


    Weitere Titelangaben:

    一种高空螺旋桨快速迭代生成方法


    Beteiligte:
    WANG CHAOLUN (Autor:in) / HAN CHAO (Autor:in) / ZHENG RISHENG (Autor:in)

    Erscheinungsdatum :

    2020-04-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge



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