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1. 发明申请

US20140151504A1 Aircraft fuselage structure and method 有权
标题翻译：飞机机身结构与方法
公开(公告)号：US20140151504A1
公开(公告)日：2014-06-05
申请号：US14084692
申请日：2013-11-20
申请人： AIRBUS OPERATIONS GMBH
发明人： Magdalena Boyen , Wolfgang Eilken , Wolfgang Schulze
IPC分类号： B64C1/06 , B64F5/00
CPC分类号： B64C1/069 , B64C1/061 , B64C1/068 , B64C2001/0081 , B64F5/10 , Y10T29/49622
摘要： An aircraft fuselage structure having a first fuselage barrel section and a second fuselage section barrel which are joined by tension fasteners extending through frame holes. A shank diameter of the fasteners is smaller than a respective frame hole diameter. A first positive locking element and a second positive locking element is provided forming a form-fit area with the first positive locking element in the circumferential direction. A method for producing such an aircraft fuselage section is also provided.
摘要翻译：具有第一机身筒部和第二机身部筒的飞机机身结构，其通过延伸穿过框架孔的张力紧固件连接。紧固件的柄直径小于相应的机架孔直径。提供了第一正锁定元件和第二正锁定元件，其在圆周方向上与第一正锁定元件形成形状配合区域。还提供了一种生产这种飞机机身部分的方法。

2. 发明授权

US09567057B2 Aircraft fuselage structure and method 有权
标题翻译：飞机机身结构与方法
公开(公告)号：US09567057B2
公开(公告)日：2017-02-14
申请号：US14084692
申请日：2013-11-20
申请人： Airbus Operations GmbH
发明人： Magdalena Boyen , Wolfgang Eilken , Wolfgang Schulze
IPC分类号： B64C1/06 , B64F5/00 , B64C1/00
CPC分类号： B64C1/069 , B64C1/061 , B64C1/068 , B64C2001/0081 , B64F5/10 , Y10T29/49622
摘要： An aircraft fuselage structure having a first fuselage barrel section and a second fuselage section barrel which are joined by tension fasteners extending through frame holes. A shank diameter of the fasteners is smaller than a respective frame hole diameter. A first positive locking element and a second positive locking element is provided forming a form-fit area with the first positive locking element in the circumferential direction. A method for producing such an aircraft fuselage section is also provided.
摘要翻译：具有第一机身筒部和第二机身部筒的飞机机身结构，其通过延伸穿过框架孔的张力紧固件连接。紧固件的柄直径小于相应的机架孔直径。提供了第一正锁定元件和第二正锁定元件，其在圆周方向上与第一正锁定元件形成形状配合区域。还提供了一种生产这种飞机机身部分的方法。

3. 发明授权

US09511845B2 Aircraft frame 有权
标题翻译：飞机架
公开(公告)号：US09511845B2
公开(公告)日：2016-12-06
申请号：US14163406
申请日：2014-01-24
申请人： Airbus Operations GmbH
发明人： Magdalena Boyen , Wolfgang Eilken , Wolfgang Schulze
IPC分类号： B64C1/06 , B29C67/00 , B64C1/10
CPC分类号： B64C1/061 , B29C64/00 , B29C67/0051 , B64C1/064 , B64C1/069 , B64C1/10 , Y10T29/49826
摘要： An aircraft frame includes a first partial aircraft frame configured to be attached to a first aircraft fuselage segment, and a second partial aircraft frame configured to be attached to a second aircraft fuselage segment. The first and second partial aircraft frames include corresponding first and second stringer coupling sections. The first partial aircraft frame and the second partial aircraft frame are configured to be attached to each other via a first web and a second web. The first stringer coupling section is located between the first inner flange and the first outer flange and the second stringer coupling section is located between the second inner flange and the second outer flange. The first stringer coupling section includes a first wall which extends from the first web into the first section of the first partial aircraft frame, and the second stringer coupling section comprises a second wall, which extends from the second web into the second section of the second partial aircraft frame.
摘要翻译：飞机框架包括构造成附接到第一飞行器机身段的第一部分飞机框架和被配置为附接到第二飞行器机身段的第二部分飞机框架。第一和第二部分飞行器架包括对应的第一和第二纵梁联接部分。第一部分飞行器架和第二部分飞行器架被构造成经由第一腹板和第二腹板相互连接。第一纵梁联接部分位于第一内凸缘和第一外凸缘之间，第二纵梁联接部分位于第二内凸缘和第二外凸缘之间。第一纵梁联接部分包括从第一腹板延伸到第一部分飞行器框架的第一部分中的第一壁，并且第二纵梁联接部分包括第二壁，第二壁从第二腹板延伸到第二部分的第二部分部分飞机架。

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