The invention describes a series of convertible aircraft (1, 1 ') having a core body (100) and 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 power source (81) and electric motors (72a, 72b, 73a, 73b, 74a, 74b) connected to the first, second, third, fourth, fifth and sixth rotors (20a, 20b, 21a, 21b, 22a, 22b); each aircraft (1, 1 ') of the series comprises a module (110, 120, 130, 140) associated with a respective architecture and interfacing with said core body (100).
本发明描述了可转换的飞行器(1、1’)的系列,所述飞行器具有核心体(100)和限定第一轴线(Y)的机身(2);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)包括电源(81)和与所述第一旋翼、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)连接的电动马达(72a、72b、73a、73b、74a、74b));该系列的每个飞行器(1、1’)包括与相应的架构相关联并与所述核心体(100)对接的模块(110、120、130、140)。
Series of hovering convertible aircraft and method for constructing hovering convertible aircraft
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
2024-01-26
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Series of hovering convertible aircraft and method for constructing hovering convertible aircraft
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