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Rotorcraft fuselage structure incorporating a load-bearing middle floor interposed between a cabin space and an equipment space
Rotorcraft fuselage structure incorporating a load-bearing middle floor interposed between a cabin space and an equipment space
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机译：旋翼飞机机身结构，在机舱空间和设备空间之间插入了承重中层
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摘要
A fuselage structure for a rotorcraft (1), the structure comprising load-bearing members including middle frames (9a, 9b) carrying a top floor (12a) and a middle floor (12b). The middle floor (12b) internally partitions the fuselage into two compartments (6, 7), including a cabin-forming top compartment (6) and a bottom compartment (7) having an open bottom (23) leading to the outside via the bottom face of the fuselage. The middle floor (12b) provides a loading plane in the top compartment (6) having a false-floor (27) made up of interchangeable slabs (28) fitted out in a variety of ways. The middle floor (12b) also forms an anchor member from which equipment (16, 17) for suspending can be suspended, which equipment is accessible from outside the fuselage through said open bottom (23).
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机译：用于旋翼飞机的机身结构（ 1 ），该结构包括带有中间框架（ 9 a， 9 < / B> b ）带有顶层（ 12 a ）和中层（ 12 ） b ）。中层（ 12 b ）在内部将机身分成两个舱（ 6、7 ），其中包括形成机舱的顶部舱（< B> 6 ）和底部舱室（ 7 ），底部舱室（ 23 ）穿过机身的底面通向外部。中层（ 12 b ）在顶部隔层（ 6 ）中提供一个带有假地板（ 27 < / B>）由以各种方式装配的可互换平板（ 28 ）组成。中层（ 12 b ）还形成了一个锚定构件，可以从该锚定构件上悬挂用于悬挂的设备（ 16、17 ），该设备是可从机身外部通过所述开口底部（ 23 ）进行操作。
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