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Civil airliner with main deck and lower deck

机译:带有主甲板和下甲板的民用客机

摘要

In a commercial aircraft with a main deck (2) and a lower deck (5, 6), at least one passenger cabin (16, 16) is also provided on the lower deck. The fuselage diameter lies on the order of a wide-body aircraft, and an energy-absorbing deformation structure (22, 23, 24) is arranged underneath the lower deck cabin. The invention proposes to arrange the wings (7) on the aircraft fuselage in accordance with the shoulder wing configuration, and to arrange the landing gear (10) outside on the fuselage such that the landing gear bays are spaced apart from one another by a certain distance that is defined by the positioning of the bottom longeron spars (9). This may provide that the lower deck volume situated underneath the main deck can be optimally utilized for payloads. The lower deck areas may also be interconnected in such a way that a significant useful width of the passage between the landing gear bays is achieved.
机译:在具有主甲板(2)和下甲板(5、6)的商用飞机中,在下甲板上还设有至少一个客舱(16、16)。机身直径约为宽体飞机的高度,下甲板机舱下方布置了一个能量吸收变形结构(22、23、24)。本发明提出根据肩部机翼构造将机翼(7)布置在飞机机身上,并且将起落架(10)布置在机身外侧,使得起落架舱彼此隔开一定距离。距离由底部纵梁(9)的位置确定。这可以规定,位于主甲板下面的下甲板容积可以被最佳地用于有效载荷。下甲板区域也可以以使得起落架舱之间的通道的有效有用宽度大的方式相互连接。

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