The invention provides a variant aircraft verification machine based on a novel flexible composite material skin. A main body part of a machine body is in a spindle shape; the wing is a straight wing, the airfoil profile is improved NASA-0012, the wing carries a rigid aileron control surface and a flexible flap control surface, the rigid aileron control surface and the flexible flap control surface can be combined and can also be independently controlled to roll, and the flexible control surface part is of a corrugated dot matrix composite material skin structure; the empennage is inverted T-shaped; the undercarriage is of a front three-point type; the engine is composed of a brushless motor and a propeller.

    本发明提供一种基于新型柔性复合材料蒙皮的变体飞行器验证机,机身主体部分为纺锤形;机翼为平直翼,翼型为改进的NASA‑0012,机翼搭载刚性副翼舵面和柔性襟翼舵面,两者既可以组合打舵也可各自独立打舵实现滚转,柔性舵面部分的为波纹点阵复合材料蒙皮结构;尾翼为倒“T”型;起落架为前三点式;发动机由无刷电机和螺旋桨组成。


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    Title :

    Variant aircraft verification machine based on novel flexible composite material skin


    Additional title:

    一种基于新型柔性复合材料蒙皮的变体飞行器验证机


    Contributors:
    BAI JIANGBO (author) / LI SHAOLIN (author) / LU CHIYU (author) / DU WENYUAN (author) / LIU TIANWEI (author)

    Publication date :

    2023-06-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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