A compact aircraft main landing gear module allowing modular installation. The module (1) comprises two main landing gears (2) and a landing gear bay (3) accommodating the landing gears (2). The compartment (3) has two side walls (40), a top wall (41), a front wall (42) and a rear wall (43). The top wall (41), the front wall (42) and the rear wall (43) together form a pressurized barrier between the compartment (3) and the pressurized chamber. By means of the landing gear module (1), it is now possible to assemble and test the main landing gear (2), one or more hatch doors, and the rectifier before they are mounted to the aircraft.
一种允许模块化安装的紧凑型飞行器主起落架模块。模块(1)包括两个主起落架(2)、以及容纳起落架(2)的起落架舱(3)。舱(3)具有两个侧壁(40)、顶壁(41)、前壁(42)和后壁(43)。顶壁(41)、前壁(42)和后壁(43)一起在舱(3)与加压腔室之间形成加压屏障。通过起落架模块(1),现在可以在主起落架(2)、一个或多个舱门、以及整流器安装到飞行器之前对它们进行组装和测试。
Compact aircraft main landing gear module allowing modular installation
允许模块化安装的紧凑型飞行器主起落架模块
2022-04-22
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
COMPACT AIRCRAFT MAIN LANDING GEAR MODULE ALLOWING MODULAR MOUNTING
European Patent Office | 2022
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