The invention describes a series of convertible aircraft (1, 1 ') having a core body (100) comprising a fuselage (2) defining a first axis (Y); the first, second, third, fourth, fifth and sixth rotors (20a, 20b, 21a, 21b, 22a, 22b) are rotatable about respective first, second, third, fourth, fifth and sixth axes (B, C, D, E, F, G), and wherein the first, second, third, fourth, fifth and sixth rotors (20a, 20b, 21a, 21b, 22a, 22b) are rotatable about respective first, second, third, fourth, fifth and sixth axes (B, C, D, E, F, G), a first thrust value, a second thrust value, a third thrust value, a fourth thrust value, a fifth thrust value and a sixth thrust value (T1, T2, T3, T4, T5, T6), which are independent of each other, respectively, and which can be operated independently of each other to generate a first thrust value, a second thrust value, a third thrust value, a fourth thrust value, a fifth thrust value and a sixth thrust value; the core body (100) comprises a respective half-wing (3) and first and second portions (11, 17) of the aerodynamic surface (9) and each module (110, 120, 130, 140) comprises a respective half-wing (3) and third and fourth portions (12, 18) of the aerodynamic surface (9).

    本发明描述了可转换的飞行器(1、1’)的系列,所述飞行器具有包括限定第一轴线(Y)的机身(2)的核心体(100);第一旋翼、第二旋翼、第三旋翼、第四旋翼、第五旋翼和第六旋翼(20a、20b、21a、21b、22a、22b)能围绕相应的第一轴线、第二轴线、第三轴线、第四轴线、第五轴线和第六轴线(B、C、D、E、F、G)旋转,并且能彼此独立地操作以相应地产生彼此独立的第一推力值、第二推力值、第三推力值、第四推力值、第五推力值和第六推力值(T1、T2、T3、T4、T5、T6);核心体(100)包括相应的半机翼(3)和空气动力学表面(9)的第一部分和第二部分(11、17)并且每个模块(110、120、130、140)包括相应的半机翼(3)和空气动力学表面(9)的第三部分和第四部分(12、18)。


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    Titel :

    Series of hovering convertible aircraft and method for constructing hovering convertible aircraft


    Weitere Titelangaben:

    能够悬停的可转换的飞行器的系列和用于构造能够悬停的可转换的飞行器的方法


    Beteiligte:

    Erscheinungsdatum :

    2024-02-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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