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1. 发明授权

US09387920B2 Self-supporting cabin structure 有权
标题翻译：自支撑舱结构
公开(公告)号：US09387920B2
公开(公告)日：2016-07-12
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： B04C1/00 , B64C1/06 , B64D11/00
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。

2. 发明授权

US08991757B2 Self-supporting cabin structural segment 有权
标题翻译：自支撑舱结构段
公开(公告)号：US08991757B2
公开(公告)日：2015-03-31
申请号：US13479538
申请日：2012-05-24
申请人： Peter Grosse-Plankermann , Martin Paetz , Markus Goslar
发明人： Peter Grosse-Plankermann , Martin Paetz , Markus Goslar
IPC分类号： B64C1/00 , B64C1/06 , B64C1/14
CPC分类号： B64C1/066 , B64C1/1461 , B64C2211/00 , Y10T29/49622
摘要： A cabin structural segment is provided for an aircraft that includes, but is not limited to a fuselage structure and a floor structure. The fuselage structure defines an interior and separating it from an environment. The fuselage structure includes, but is not limited to an opening for a door. It is possible to provide via the opening a connection between the interior and the environment. The cabin structural segment is designed to be self-supporting. The cabin structural segment is fastenable exclusively to the floor structure. The cabin structural segment is constructed in such a way that the one cabin structural segment frames the opening.
摘要翻译：为飞行器提供舱室结构段，其包括但不限于机身结构和地板结构。机身结构定义了一个内部，并将其与环境分开。机身结构包括但不限于门的开口。可以经由开口提供内部和环境之间的连接。机舱结构段设计为自支撑。车厢结构部分专门用于地板结构。机舱结构段以这样的方式构造，使得一个机舱结构段框架开口。

3. 发明授权

US09656754B2 Ventilation system and aircraft air-conditioning system 有权
公开(公告)号：US09656754B2
公开(公告)日：2017-05-23
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
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.

4. 发明授权

US09156554B2 System component module and method for mounting in an aircraft cabin 有权
标题翻译：系统组件模块和安装在飞机机舱中的方法
公开(公告)号：US09156554B2
公开(公告)日：2015-10-13
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： B64D11/00 , B64D13/00
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。

5. 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。

6. 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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