公开(公告)号：US20170129585A1

公开(公告)日：2017-05-11

申请号：US15344724

申请日：2016-11-07

申请人： Airbus Operations GmbH

发明人： Johann Konrad Erben

IPC分类号： B64C1/14 ,  E05B83/42 ,  E05C9/00 ,  E05C19/12 ,  E05B79/10 ,  E05B17/20 ,  E05C3/12

CPC分类号： B64C1/1461 ,  B64C1/143 ,  E05B15/0086 ,  E05B17/2007 ,  E05B17/2034 ,  E05B79/10 ,  E05B83/42 ,  E05C3/02 ,  E05C3/12 ,  E05C9/00 ,  E05C19/12

摘要： A door assembly, particularly for doors of passenger aircraft, includes a door frame, a door having a door body hingedly installed in the door frame, at least one hooking pintle attached to the door frame or an edge of the door body extending along a pintle axis, and at least one door latch connected to an edge of the door body or the door frame, respectively, the door latch having a substantially C-shaped latch body configured to rotate around an axis parallel to the pintle axis of the hooking pintle. The door assembly further includes a bistable latch and hook mechanism configured to catch the door latch in hooking engagement with the hooking pintle and to retain the door latch in a direction perpendicular to the door body in an overcenter position.

公开(公告)号：US10538304B2

公开(公告)日：2020-01-21

申请号：US15344724

申请日：2016-11-07

申请人： Airbus Operations GmbH

发明人： Johann Konrad Erben

IPC分类号： B64C1/14 ,  E05B17/20 ,  E05B79/10 ,  E05B83/42 ,  E05C3/12 ,  E05C9/00 ,  E05C19/12

摘要： A door assembly, particularly for doors of passenger aircraft, includes a door frame, a door having a door body hingedly installed in the door frame, at least one hooking pintle attached to the door frame or an edge of the door body extending along a pintle axis, and at least one door latch connected to an edge of the door body or the door frame, respectively, the door latch having a substantially C-shaped latch body configured to rotate around an axis parallel to the pintle axis of the hooking pintle. The door assembly further includes a bistable latch and hook mechanism configured to catch the door latch in hooking engagement with the hooking pintle and to retain the door latch in a direction perpendicular to the door body in an overcenter position.

公开(公告)号：US20130306793A1

公开(公告)日：2013-11-21

申请号：US13954240

申请日：2013-07-30

申请人： Airbus Operations GmbH

发明人： Johann Konrad Erben ,  Sten Kramer

IPC分类号： B64C1/22 ,  B64D11/00

CPC分类号： B64C1/22 ,  B64C1/00 ,  B64C2001/0027 ,  B64D11/00

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.

摘要翻译： 飞机机身的机身部分包括具有封闭横截面的墙壁，第一机舱地板，第二机舱地板和货舱底板。 第一个客舱地板，第二个客舱地板和货舱底板彼此垂直间隔开并连接到墙壁上。 第一乘客区域布置在第一机舱地板的上方，第二乘客区域布置在第二机舱地板的上方，货物区域布置在货舱底板的上方。 货物区域的尺寸设计为：至少提供四个乘客座位，最多可提供1立方米的货物舱。 以这种方式，可以以面向需求的方式设计现有的飞行器机身，使得其可容纳两个或更多个乘客区域。