The disclosure relates to an aircraft subassembly having a main-landing-gear system and a sponson. The aircraft subassembly (100) comprises a fuselage structure (102) and a main-landing-gear system (104). The main-landing-gear system (104) additionally comprises a sponson (130), connected to and extending outward from the fuselage structure (102). The sponson (130) comprises a central portion (131) and a first main-landing-gear door (140) that is moveable relative to the central portion (131) between, inclusively, a closed position and an open position. The sponson (130) further comprises a second main-landing-gear door (142) that is moveable relative to the central portion (131) between, inclusively, a closed position and an open position. The main-landing-gear system (104) further comprises a first main-landing-gear assembly (106), connected to the first wheel (110) and a second main-landing-gear assembly (112), connected to the second wheel (116).
本公开涉及具有主起落架组件和突出部的飞机子组件。飞机子组件(100)包括机身结构(102)。飞机子组件(100)还包括主起落架系统(104)。主起落架系统(104)另外包括连接到机身结构(102)并从机身结构(102)向外延伸的突出部(130)。突出部(130)包括:中央部(131);第一主起落架门(140),其相对于中央部(131)能在闭合位置和打开位置之间——包括闭合位置和打开位置——移动;以及第二主起落架门(142),其相对于中央部(131)能在闭合位置和打开位置之间——包括闭合位置和打开位置——移动。主起落架系统(104)还包括连接到第一轮(110)第一主起落架组件(106)以及连接到第二轮(116)的第二主起落架组件(112)。
Aircraft subassembly with main-landing-gear system and sponson
具有主起落架组件和突出部的飞机子组件
2021-06-22
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2021
|European Patent Office | 2024
|European Patent Office | 2021
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