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AIRCRAFT SUBASSEMBLY, HAVING MAIN-LANDING-GEAR ASSEMBLY AND SPONSON, HOUSING MAIN-LANDING-GEAR ASSEMBLY

机译:飞机子组件,具有主登陆齿轮组件和Sponson,外壳主落齿轮组件

摘要

An aircraft subassembly (100) comprises a fuselage structure (102), comprising a first side (108) and a second side (114). The aircraft subassembly (100) further comprises a main-landing-gear system (104), having a single pair of wheels (107). 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).
机译:飞机子组件(100)包括机身结构(102),包括第一侧(108)和第二侧(114)。该飞机子组件(100)还包括主着陆齿轮系统(104),具有一对车轮(107)。主落地齿轮系统(104)另外包括Sponson(130),从机身结构(102)向外延伸并向外延伸。 Sponson(130)包括中心部分(131)和第一主着陆齿轮门(140),第一主着陆齿轮门(140)可相对于中央部分(131)可包括在内,包合地,关闭位置和打开位置。 Sponson(130)还包括第二主落地 - 齿轮门(142),其可相对于中心部分(131)移动,包括在内,包括关闭位置和打开位置。主落地齿轮系统(104)还包括第一主着陆齿轮组件(106),连接到第一轮(110)和第二主落地齿轮组件(112),连接到第二轮(116)。

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