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1. 发明申请

US20130126673A1 RAIL SYSTEM AND METHOD AND SYSTEM FOR MOUNTING A COMPONENT IN AN AIRCRAFT 有权
公开(公告)号：US20130126673A1
公开(公告)日：2013-05-23
申请号：US13643701
申请日：2011-04-26
申请人： Sebastian Umlauft , Ralf Koblitz , Niklas Halfmann , Dieter Krause , Christoph Blees
发明人： Sebastian Umlauft , Ralf Koblitz , Niklas Halfmann , Dieter Krause , Christoph Blees
IPC分类号： B64F5/00
CPC分类号： B64F5/0009 , B64C1/20 , B64F5/10 , B64F5/50
摘要： A rail system for use when assembling a component in an aircraft comprises a first rail element having a securing device which is designed to be complementary to a first securing device provided in the region of a floor of an aircraft fuselage element and is adapted to cooperate with the first securing device in order to releasably secure the first rail element in the region of the floor of the aircraft fuselage element, wherein a section of the first rail element projects beyond an edge of the floor of the aircraft fuselage element in the connected state of the first rail element and the aircraft fuselage element. The first rail element furthermore comprises a guide device, which is designed to be complementary to a first guide device provided on an assembly aid, which is to be introduced into the aircraft fuselage element, and is adapted to cooperate with the first guide device to enable a guided displacement of the assembly aid to be introduced into the aircraft fuselage element relative to the rail system. The rail system furthermore comprises a second rail element having a securing device which is designed to be complementary to a second securing device provided in the region of the floor of the aircraft fuselage element and is adapted to cooperate with the second securing device in order to releasably secure the second rail element in the region of the floor of the aircraft fuselage element, wherein a section of the second rail element projects beyond an edge of the floor of the aircraft fuselage element in the connected state of the second rail element and the aircraft fuselage element. The second rail element furthermore comprises a guide device, which is designed to be complementary to a second guide device provided on an assembly aid, which is to be introduced into the aircraft fuselage element, and is adapted to cooperate with the second guide device to enable a guided displacement of the assembly aid to be introduced into the aircraft fuselage element relative to the rail system.

2. 发明申请

US20110309214A1 APPARATUS FOR AFFIXING AN OBJECT TO A RAIL 有权
标题翻译：装备对象的装置
公开(公告)号：US20110309214A1
公开(公告)日：2011-12-22
申请号：US13163535
申请日：2011-06-17
申请人： Christoph BLEES , Dieter KRAUSE , Ralf KOBLITZ , Oliver GEHLEN , Dirk HUMFELDT , Mark HERZOG
发明人： Christoph BLEES , Dieter KRAUSE , Ralf KOBLITZ , Oliver GEHLEN , Dirk HUMFELDT , Mark HERZOG
IPC分类号： F16M11/04 , F16M13/02
CPC分类号： B64C1/20 , B64D9/00
摘要： An apparatus for affixing an object to a rail includes, but is not limited to at least one base body, at least one locking body and at least one operating element. The locking body is held so as to be movable relative to the base body and is connected to the operating element by way of at least one bearing. The operating element is arranged so as to be rotatable in the base body, includes, but is not limited to a cam that acts on the base body, and when rotated moves the locking body towards the base body. In this way apparatus is created which makes possible the manual affixing and undoing, without the need for tools, of an object on and from a rail, for example, if needed, in order to reposition displaceable monuments in a cabin of an aircraft.
摘要翻译：用于将物体固定到轨道的装置包括但不限于至少一个基体，至少一个锁定体和至少一个操作元件。锁定体被保持为能够相对于基体移动，并且通过至少一个轴承连接到操作元件。操作元件布置成可在基体中旋转，包括但不限于作用在基体上的凸轮，并且当旋转时使锁定体向基体移动。以这种方式，创建了使得可能的手段，例如，如果需要，手动地将轨道上的对象手动附加和拆除，而不需要工具，以便重新定位飞机的机舱中的可移动纪念碑。

3. 发明授权

US08899545B2 Apparatus for affixing an object to a rail 有权
标题翻译：用于将物体固定在轨道上的装置
公开(公告)号：US08899545B2
公开(公告)日：2014-12-02
申请号：US13163535
申请日：2011-06-17
申请人： Christoph Blees , Dieter Krause , Ralf Koblitz , Oliver Gehlen , Dirk Humfeldt , Mark Herzog
发明人： Christoph Blees , Dieter Krause , Ralf Koblitz , Oliver Gehlen , Dirk Humfeldt , Mark Herzog
IPC分类号： A47B97/00 , B65D63/00 , B64D9/00 , B64C1/20
CPC分类号： B64C1/20 , B64D9/00
摘要： An apparatus for affixing an object to a rail includes, but is not limited to at least one base body, at least one locking body and at least one operating element. The locking body is held so as to be movable relative to the base body and is connected to the operating element by way of at least one bearing. The operating element is arranged so as to be rotatable in the base body, includes, but is not limited to a cam that acts on the base body, and when rotated moves the locking body towards the base body. In this way apparatus is created which makes possible the manual affixing and undoing, without the need for tools, of an object on and from a rail, for example, if needed, in order to reposition displaceable monuments in a cabin of an aircraft.
摘要翻译：用于将物体固定到轨道的装置包括但不限于至少一个基体，至少一个锁定体和至少一个操作元件。锁定体被保持为能够相对于基体移动，并且通过至少一个轴承连接到操作元件。操作元件布置成可在基体中旋转，包括但不限于作用在基体上的凸轮，并且当旋转时使锁定体向基体移动。以这种方式，创建了使得可能的手段，例如，如果需要，手动地将轨道上的对象手动附加和拆除，而不需要工具，以便重新定位飞机的机舱中的可移动纪念碑。

4. 发明授权

US08661685B2 Preassembly and integration of aircraft cabins 有权
标题翻译：飞机舱的组装和整合
公开(公告)号：US08661685B2
公开(公告)日：2014-03-04
申请号：US13058365
申请日：2009-08-03
申请人： Christoph Blees , Niklas Halfmann , Dieter Krause , Marcus Gehm
发明人： Christoph Blees , Niklas Halfmann , Dieter Krause , Marcus Gehm
IPC分类号： B21D53/88
CPC分类号： B64F5/00 , B64F5/10 , Y10T16/364 , Y10T16/379 , Y10T29/49616 , Y10T29/49622 , Y10T29/49828 , Y10T29/53539 , Y10T29/53548
摘要： According to an exemplary embodiment of the invention, pre-assembly and integration of part of an aircraft cabin takes place outside the aircraft structure by means of an assembly device. After pre-assembly, the part of the aircraft cabin is slid into the open section of the aircraft structure where it is installed.
摘要翻译：根据本发明的示例性实施例，飞机机舱的一部分的预组装和集成通过组装装置发生在飞行器结构外部。在预组装之后，飞机机舱的一部分滑入安装在其上的飞机结构的开口部分。

5. 发明申请

US20110138603A1 PREASSEMBLY AND INTEGRATION OF AIRCRAFT CABINS 有权
标题翻译：飞机舱的组合和整合
公开(公告)号：US20110138603A1
公开(公告)日：2011-06-16
申请号：US13058365
申请日：2009-08-03
申请人： Christoph Blees , Niklas Halfmann , Dieter Krause , Marcus Gehm
发明人： Christoph Blees , Niklas Halfmann , Dieter Krause , Marcus Gehm
IPC分类号： B64F5/00 , B23P19/00 , B23P11/00
CPC分类号： B64F5/00 , B64F5/10 , Y10T16/364 , Y10T16/379 , Y10T29/49616 , Y10T29/49622 , Y10T29/49828 , Y10T29/53539 , Y10T29/53548
摘要： According to an exemplary embodiment of the invention, pre-assembly and integration of part of an aircraft cabin takes place outside the aircraft structure by means of an assembly device. After pre-assembly, the part of the aircraft cabin is slid into the open section of the aircraft structure where it is installed.
摘要翻译：根据本发明的示例性实施例，飞机机舱的一部分的预组装和集成通过组装装置发生在飞行器结构外部。在预组装之后，飞机机舱的一部分滑入安装在其上的飞机结构的开口部分。

6. 发明授权

US09174748B2 Rail system and method and system for mounting a component in an aircraft 有权
公开(公告)号：US09174748B2
公开(公告)日：2015-11-03
申请号：US13643701
申请日：2011-04-26
申请人： Sebastian Umlauft , Ralf Koblitz , Niklas Halfmann , Dieter Krause , Christoph Blees
发明人： Sebastian Umlauft , Ralf Koblitz , Niklas Halfmann , Dieter Krause , Christoph Blees
IPC分类号： B64F5/00 , B64C1/20
CPC分类号： B64F5/0009 , B64C1/20 , B64F5/10 , B64F5/50
摘要： A rail system for use when assembling a component in an aircraft comprises a first rail element having a securing device which is designed to be complementary to a first securing device provided in the region of a floor of an aircraft fuselage element and is adapted to cooperate with the first securing device in order to releasably secure the first rail element in the region of the floor of the aircraft fuselage element, wherein a section of the first rail element projects beyond an edge of the floor of the aircraft fuselage element in the connected state of the first rail element and the aircraft fuselage element. The first rail element furthermore comprises a guide device, which is designed to be complementary to a first guide device provided on an assembly aid, which is to be introduced into the aircraft fuselage element, and is adapted to cooperate with the first guide device to enable a guided displacement of the assembly aid to be introduced into the aircraft fuselage element relative to the rail system. The rail system furthermore comprises a second rail element having a securing device which is designed to be complementary to a second securing device provided in the region of the floor of the aircraft fuselage element and is adapted to cooperate with the second securing device in order to releasably secure the second rail element in the region of the floor of the aircraft fuselage element, wherein a section of the second rail element projects beyond an edge of the floor of the aircraft fuselage element in the connected state of the second rail element and the aircraft fuselage element. The second rail element furthermore comprises a guide device, which is designed to be complementary to a second guide device provided on an assembly aid, which is to be introduced into the aircraft fuselage element, and is adapted to cooperate with the second guide device to enable a guided displacement of the assembly aid to be introduced into the aircraft fuselage element relative to the rail system.

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