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commercial aircraft with one main floor and one lower floor

机译:一楼一低层的商用飞机

摘要

COMMERCIAL AIRCRAFT WITH A MAIN FLOOR AND A LOWER FLOOR. In a commercial aircraft with a main floor (2) and a lower floor (5, 6), at least one passenger cabin (16, 16) is also provided on the lower floor. The fuselage diameter is in the order of a wide body aircraft, and an energy absorbing strain structure (22, 23, 24) is arranged below the lower deck cabin. The invention proposes to arrange the wings (7) in the aircraft fuselage according to the semi-high wing configuration, and to arrange the landing gear (10) around the fuselage such that the landing gear compartments are separated from each other by a certain distance that is defined by the position of the lower lengths (9). This may provide that the lower floor volume below the main floor can be optimally used for payloads. The lower deck areas may also be interconnected such that a significant useful width of passage between the landing gear compartments is obtained.
机译:商用飞机的主楼层和低楼层。在具有主地板(2)和下地板(5、6)的商用飞机中,在下地板上还设有至少一个客舱(16、16)。机身直径为宽体飞机的数量级,并且在下甲板机舱下方布置了能量吸收应变结构(22、23、24)。本发明提出根据半高机翼配置将机翼(7)布置在飞机机身中,并且将起落架(10)围绕机身布置,使得起落架舱彼此隔开一定距离。由较低长度(9)的位置定义。这可以提供主地板下方的下部地板体积可以最佳地用于有效载荷。下甲板区域也可以相互连接,从而在起落架舱之间获得相当大的有用的通道宽度。

著录项

  • 公开/公告号BRPI0512353A

    专利类型

  • 公开/公告日2008-03-04

    原文格式PDF

  • 申请/专利权人 AIRBUS DEUTSCHLAND GMBH;

    申请/专利号BR2005PI12353

  • 发明设计人 WILFRIED SPRENGER;

    申请日2005-07-08

  • 分类号B64C1;B64C11;B64C25;B64C25/12;B64D11;B64D25;

  • 国家 BR

  • 入库时间 2022-08-21 20:08:45

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