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Fuselage Segment For A Fuselage Of An Aircraft, Aircraft Fuselage and Aircraft

机译:飞机机身的机身段,飞机机身和飞机

摘要

A fuselage segment for an aircraft fuselage includes a wall with a closed cross section, a first cabin floor, a second cabin floor, and a cargo hold floor. The first cabin floor, the second cabin floor, and the cargo hold floor are vertically spaced apart from each other and connected to the wall. A first passenger region is arranged above the first cabin floor, a second passenger region is arranged above the second cabin floor, and a cargo region is arranged above the cargo hold floor. The cargo region is dimensioned in such a manner that for at least four passenger seats a maximum of 1 m3 of cargo hold volume is provided. In this manner an existing aircraft fuselage can be designed in a demand-oriented manner so that it can accommodate two or more passenger regions.
机译:用于飞机机身的机身段包括具有闭合横截面的壁,第一机舱地板,第二机舱地板和货舱地板。第一机舱地板,第二机舱地板和货舱地板彼此垂直地间隔开并连接至墙壁。第一乘客区域布置在第一机舱地板上方,第二乘客区域布置在第二机舱地板上方,并且货物区域布置在货舱地板上方。货物区域的尺寸设计为,至少为四个乘客座位提供最大1 m 3 的货物容纳量。以这种方式,可以以需求为导向的方式设计现有的飞机机身,以使其可以容纳两个或更多个乘客区域。

著录项

  • 公开/公告号US2013306793A1

    专利类型

  • 公开/公告日2013-11-21

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号US201313954240

  • 发明设计人 JOHANN KONRAD ERBEN;STEN KRAMER;

    申请日2013-07-30

  • 分类号B64C1/22;B64D11/00;

  • 国家 US

  • 入库时间 2022-08-21 16:06:35

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