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11. 发明申请

US20110133027A1 AIRCRAFT HAVING A FORCE TRANSMISSION ELEMENT BETWEEN A CABIN STRUCTURAL ELEMENT AND A PRIMARY STRUCTURE 有权
标题翻译：具有舱室结构元件与主要结构之间的强制传动元件的飞机
公开(公告)号：US20110133027A1
公开(公告)日：2011-06-09
申请号：US12936714
申请日：2009-03-20
申请人： Ulrike Graeber , Peter Grosse-Plankermann , Martin Pätz , Holger Becker
发明人： Ulrike Graeber , Peter Grosse-Plankermann , Martin Pätz , Holger Becker
IPC分类号： B64D11/00 , B64C1/06 , B23P11/00
CPC分类号： B64C1/068 , B64C1/066 , B64C1/1484 , Y10T29/49826
摘要： The invention relates to an aircraft comprising a force transmission element which detachably connects a cabin structural segment to an aircraft primary structure and which comprises a cabin bearing element and a structure bearing element, the cabin bearing element being connected to the cabin structural segment and the structure bearing element being connected to the aircraft primary structure. The force transmission element is designed in such a manner that a force transmission can take place between the cabin structural segment and the aircraft primary structure with at least one degree of freedom of movement.
摘要翻译：本发明涉及一种飞行器，其包括力传递元件，该力传递元件将舱室结构段可拆卸地连接到飞机初级结构，其包括舱室轴承元件和结构轴承元件，所述舱室轴承元件连接到舱室结构段和结构轴承元件连接到飞机初级结构。力传递元件被设计成使得能够以至少一个移动自由度在机舱结构段和飞机初级结构之间发生力传递。

12. 发明申请

US20090250554A1 SELF-SUPPORTING CABIN STRUCTURE 有权
标题翻译：自支撑舱结构
公开(公告)号：US20090250554A1
公开(公告)日：2009-10-08
申请号：US12420761
申请日：2009-04-08
申请人： Ulrike GRAEBER , Peter GROSSE-PLANKERMANN , Martin PAETZ
发明人： Ulrike GRAEBER , Peter GROSSE-PLANKERMANN , Martin PAETZ
IPC分类号： B64C1/00 , B64C1/06 , B64C1/18 , B23P11/00
CPC分类号： B64C1/068 , B64C1/06 , B64C1/066 , B64C2211/00 , B64D2011/0046 , Y02T50/46 , Y10T29/49826
摘要： A cabin structural unit for attaching cabin installation elements is provided for an aircraft. The cabin structural unit is set up in such a way that a cabin installation element is attachable. The cabin structural unit is implemented as self-supporting and fastenable to an aircraft structure.
摘要翻译：为飞机提供了一个用于安装机舱安装元件的舱室结构单元。机舱结构单元设置成可以安装机舱安装元件。机舱结构单元实现为自支撑并且可紧固到飞行器结构。

13. 发明授权

US09623914B2 Covering system for an interior space of a vehicle, a method for covering a region of an interior space of a vehicle, and a vehicle with an interior space, which is covered by the covering system in at least some regions 有权
公开(公告)号：US09623914B2
公开(公告)日：2017-04-18
申请号：US13599932
申请日：2012-08-30
申请人： Peter Grosse-Plankermann , Dieter Plehn
发明人： Peter Grosse-Plankermann , Dieter Plehn
IPC分类号： B62D25/20 , B64C1/18
CPC分类号： B62D25/20 , B64C1/18
摘要： A covering system for an interior space of a vehicle comprises at least one surface element and at least one sealing element. The surface element comprises an upper surface and at least one bounding edge extending at an angle to the upper surface. The surface element furthermore comprises at least one recess, which runs at least adjacent to the bounding edge. The sealing element has an extent corresponding at least partly with the at least one bounding edge, and a shape corresponding at least partly with the recess of the surface element.

14. 发明申请

US20130249178A1 SEAT BENCH TRANSPORT DEVICE 有权
标题翻译：座椅运输设备
公开(公告)号：US20130249178A1
公开(公告)日：2013-09-26
申请号：US13613861
申请日：2012-09-13
申请人： Peter GROSSE-PLANKERMANN , Thomas Bardenhagen , Uwe Pietz
发明人： Peter GROSSE-PLANKERMANN , Thomas Bardenhagen , Uwe Pietz
IPC分类号： B62B3/02
CPC分类号： B62B3/02 , B62B3/04 , B62B3/10 , B62B3/16 , B62B2202/32 , B62B2203/44 , B62B2206/02 , B64F5/50
摘要： Disclosed is a seat bench transport device according to the invention for transporting a bench of seats for a vehicle, comprising a chassis, a retaining rail pair that is arranged on the chassis and includes two retaining rails extending parallel to one another for accommodating seat bench feet, the lengthwise sides of these rails that face one another being open at least in sections and the lengthwise sides thereof that face away from one another each having at least one locking section, and a displacement mechanism for moving the retaining rails transversely relative to one another.
摘要翻译：公开了根据本发明的用于运输用于车辆的座椅台座的座椅台架运输装置，包括底盘，保持轨道对，其布置在底盘上并且包括彼此平行延伸的两个保持轨道，用于容纳座椅脚相互面对的这些轨道的长度方向至少部分开放，并且其长度方向彼此面对，每个具有至少一个锁定部分，以及用于相对于彼此横向地移动保持轨道的位移机构。

15. 发明授权

US08430362B2 Aircraft having a force transmission element between a cabin structural element and a primary structure 有权
标题翻译：飞机在机舱结构元件和主结构之间具有力传递元件
公开(公告)号：US08430362B2
公开(公告)日：2013-04-30
申请号：US12936714
申请日：2009-03-20
申请人： Ulrike Graeber , Peter Grosse-Plankermann , Martin Pätz , Holger Becker
发明人： Ulrike Graeber , Peter Grosse-Plankermann , Martin Pätz , Holger Becker
IPC分类号： G05D1/12
CPC分类号： B64C1/068 , B64C1/066 , B64C1/1484 , Y10T29/49826
摘要： The invention relates to an aircraft comprising a force transmission element which detachably connects a cabin structural segment to an aircraft primary structure and which comprises a cabin bearing element and a structure bearing element, the cabin bearing element being connected to the cabin structural segment and the structure bearing element being connected to the aircraft primary structure. The force transmission element is designed in such a manner that a force transmission can take place between the cabin structural segment and the aircraft primary structure with at least one degree of freedom of movement.
摘要翻译：本发明涉及一种飞行器，其包括力传递元件，该力传递元件将舱室结构段可拆卸地连接到飞机初级结构，其包括舱室轴承元件和结构轴承元件，所述舱室轴承元件连接到舱室结构段和结构轴承元件连接到飞机初级结构。力传递元件被设计成使得能够以至少一个移动自由度在机舱结构段和飞机初级结构之间发生力传递。

16. 发明申请

US20120312921A1 System component module and method for mounting a system component module 有权
标题翻译：用于安装系统组件模块的系统组件模块和方法
公开(公告)号：US20120312921A1
公开(公告)日：2012-12-13
申请号：US13526107
申请日：2012-06-18
申请人： Peter Grosse-Plankermann , Thomas Fink , Peter Kiron , Martin Paetz
发明人： Peter Grosse-Plankermann , Thomas Fink , Peter Kiron , Martin Paetz
IPC分类号： B64D13/00 , B64D11/00
CPC分类号： B64D11/003 , B64D11/00 , B64D13/00 , B64D2011/0038 , B64D2013/003 , Y02T50/44 , Y02T50/46
摘要： A system component module (100) to be mounted in an aircraft cabin (22) comprises a support (28), to which a PSU duct (34) as well as an individual air supply system (72) are attached. A fastening device (112) is designed to fasten the system component module (100) to a bottom panel (32) of a luggage compartment (26) in the aircraft cabin (22).
摘要翻译：要安装在飞机机舱（22）中的系统组件模块（100）包括支撑件（28），PSU导管（34）以及单独的空气供应系统（72）附接到该支撑件。紧固装置（112）被设计成将系统部件模块（100）紧固到飞机机舱（22）中的行李箱（26）的底板（32）上。

17. 发明申请

US20120145828A1 SYSTEM AND METHOD FOR MANUFACTURING A VEHICLE CABIN 有权
标题翻译：制造车厢的系统和方法
公开(公告)号：US20120145828A1
公开(公告)日：2012-06-14
申请号：US13314788
申请日：2011-12-08
申请人： Peter GROSSE-PLANKERMANN , Martin PÄTZ , Philipp JUNGE
发明人： Peter GROSSE-PLANKERMANN , Martin PÄTZ , Philipp JUNGE
IPC分类号： B64D11/00 , B23P17/04 , B23P19/00 , B64F5/00
CPC分类号： B64D11/00 , B64C2211/00 , B64D11/003 , B64F5/10 , Y10T29/49826 , Y10T29/53
摘要： A system for manufacturing a vehicle cabin includes, but is not limited to at least one first installation component, at least one first surface element, and at least one guide element. The first surface element is slidably arranged on the first installation component with the guide element to form a cabin module, and the guide element is lockable in at least one assembly position and at least one operating position. The resultant cabin module in the assembly position includes, but is not limited to outer dimensions enabling incorporation into a fuselage section of a vehicle, so that the cabin module in the operating position can make up at least a section of the cabin in the fuselage section of the vehicle.
摘要翻译：用于制造车厢的系统包括但不限于至少一个第一安装部件，至少一个第一表面元件和至少一个引导元件。第一表面元件可滑动地布置在具有引导元件的第一安装部件上以形成舱模块，并且引导元件可锁定在至少一个组装位置和至少一个操作位置。在组装位置中的合成舱模块包括但不限于外部尺寸，使得能够结合到车辆的机身部分中，使得处于操作位置的舱模块可以组装在机身部分中的舱室的至少一部分的车辆。

18. 发明申请

US20120129438A1 Ventilation system and aircraft air-conditioning system 有权
标题翻译：通风系统和飞机空调系统
公开(公告)号：US20120129438A1
公开(公告)日：2012-05-24
申请号：US13302719
申请日：2011-11-22
申请人： Peter Grosse-Plankermann , Martin Paetz , Thomas Fink
发明人： Peter Grosse-Plankermann , Martin Paetz , Thomas Fink
IPC分类号： B64D13/00 , B60H1/24
CPC分类号： B64D13/00 , B64D2013/003
摘要： A ventilation system (10) for installation in an aircraft passenger cabin comprises an air supply pipe (12), which has a plurality of air outlet openings (14) disposed in a distributed manner along its longitudinal axis (L). An air chamber housing (16) is connectable to the air supply pipe (12) at various positions along the longitudinal axis (L) of the air supply pipe, such that air-conditioning air flowing through the air supply pipe (12) is supplyable, through an air outlet opening provided in the air supply pipe (12), into the air chamber housing (16). A connection device (34) is designed to connect the air chamber housing (16) to an air supply device (36) for supplying air-conditioning air into the aircraft passenger cabin.
摘要翻译：用于安装在飞机乘客舱中的通风系统（10）包括一个空气供应管（12），该供气管具有沿其纵向轴线（L）以分布方式设置的多个空气出口开口（14）。在空气供给管的纵向轴线（L）的各个位置处，空气室壳体（16）可连接到空气供给管（12），使得流过供气管（12）的空调空气可供应通过设置在供气管（12）中的出气口，进入空气室壳体（16）。连接装置（34）被设计成将空气室壳体（16）连接到用于将空调空气供应到飞机乘客舱中的空气供应装置（36）。

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