专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US09266601B2 Method and system for emergency ventilation of an aircraft cabin in the case of a leak in the area of an air mixer 有权
标题翻译：在空气混合器区域发生泄漏的情况下，飞机机舱应急通风的方法和系统
公开(公告)号：US09266601B2
公开(公告)日：2016-02-23
申请号：US13126544
申请日：2009-09-08
申请人： Frank Klimpel , Rüdiger Schmidt
发明人： Frank Klimpel , Rüdiger Schmidt
IPC分类号： B64D13/00 , B64C1/18 , B64D13/02 , B64C1/00
CPC分类号： B64C1/18 , B64C2001/009 , B64D13/02 , Y02T50/44
摘要： In a method for emergency ventilation of an aircraft cabin, a leak is detected in the area of an air mixer of an aircraft air conditioning system. An emergency air flap, which in a closed position prevents an air exchange between an aircraft area adjacent to the air mixer and the aircraft cabin, is controlled into an open position. Air from the aircraft area adjacent to the air mixer is conveyed through the open emergency air flap into the aircraft cabin.
摘要翻译：在飞机机舱的紧急通风方法中，在飞行器空调系统的空气混合器的区域中检测到泄漏。处于闭合位置的紧急空气挡板防止与空气混合器相邻的飞机区域与飞机机舱之间的空气交换被控制到打开位置。来自与空气混合器相邻的飞机区域的空气通过开放的紧急空气挡板输送到飞机机舱中。

2. 发明授权

US08272930B2 Air system 有权
标题翻译：空气系统
公开(公告)号：US08272930B2
公开(公告)日：2012-09-25
申请号：US11795778
申请日：2006-01-24
申请人： Frank Klimpel , Torge Pfafferott
发明人： Frank Klimpel , Torge Pfafferott
IPC分类号： B64D11/00 , B64D13/02
CPC分类号： B64D13/02 , B64D13/06 , B64D2013/0618 , B64D2013/0644 , B64D2013/0688 , Y02T50/56
摘要： An air system for pressurizing and air conditioning a cockpit and cabin space of a plane comprises a compressor (3) for compressing an air mass flow, wherein the air mass flow to be compressed is extracted through a ram air duct (13, 14) from the environment of the plane and supplied through a heat exchanger (15, 18) to at least one zone (10A-D) to be pressurized and air conditioned.
摘要翻译：用于对飞机的驾驶舱和客舱空间进行加压和空调的空气系统包括用于压缩空气质量流的压缩机（3），其中待压缩的空气质量流量通过冲压空气管道（13,14）从平面的环境并通过热交换器（15,18）供应到至少一个区域（10A-D），以被加压和空调。

3. 发明申请

US20090291625A1 Air System 有权
标题翻译：空气系统
公开(公告)号：US20090291625A1
公开(公告)日：2009-11-26
申请号：US11795778
申请日：2006-01-24
申请人： Frank Klimpel , Torge Pfafferott
发明人： Frank Klimpel , Torge Pfafferott
IPC分类号： B64D13/02 , F25B29/00
CPC分类号： B64D13/02 , B64D13/06 , B64D2013/0618 , B64D2013/0644 , B64D2013/0688 , Y02T50/56
摘要： An air system for pressurizing and air conditioning a cockpit and cabin space of a plane comprises a compressor (3) for compressing an air mass flow, wherein the air mass flow to be compressed is extracted through a ram air duct (13, 14) from the environment of the plane and supplied through a heat exchanger (15, 18) to at least one zone (10A-D) to be pressurized and air conditioned.
摘要翻译：用于对飞机的驾驶舱和客舱空间进行加压和空调的空气系统包括用于压缩空气质量流的压缩机（3），其中待压缩的空气质量流量通过冲压空气管道（13,14）从平面的环境并通过热交换器（15,18）供应到至少一个区域（10A-D），以被加压和空调。

4. 发明申请

US20120003908A1 Method And System For Emergency Ventilation Of An Aircraft Cabin In The Case Of A Leak In The Area Of An Air Mixer 有权
标题翻译：在空气混合器区域泄漏的情况下，飞机机舱紧急通风的方法和系统
公开(公告)号：US20120003908A1
公开(公告)日：2012-01-05
申请号：US13126544
申请日：2009-09-08
申请人： Frank Klimpel , Rudiger Schmidt
发明人： Frank Klimpel , Rudiger Schmidt
IPC分类号： B64D13/00
CPC分类号： B64C1/18 , B64C2001/009 , B64D13/02 , Y02T50/44
摘要： In a method for emergency ventilation of an aircraft cabin (12) a leak is detected in the area of an air mixer (24) of an aircraft air conditioning system (16). An emergency air flap (38), which in a closed position prevents an air exchange between an aircraft area (40) adjacent to the air mixer (24) and the aircraft cabin (12), is controlled into an open position. Finally, air from the aircraft area (40) adjacent to the air mixer (24) is conveyed through the open emergency air flap (38) into the aircraft cabin (12).
摘要翻译：在飞机机舱（12）的紧急通风的方法中，在飞行器空调系统（16）的空气混合器（24）的区域中检测到泄漏。处于关闭位置的紧急空气挡板（38）防止与空气混合器（24）相邻的飞行器区域（40）和飞机机舱（12）之间的空气交换被控制在打开位置。最后，邻近空气混合器（24）的飞机区域（40）的空气通过开放的紧急空气挡板（38）输送到飞机机舱（12）中。

5. 发明授权

US08360358B2 Ram air duct flap arrangement and ram air duct 有权
标题翻译：拉姆空气管道挡板装置和冲压空气管道
公开(公告)号：US08360358B2
公开(公告)日：2013-01-29
申请号：US12894488
申请日：2010-09-30
申请人： Frank Klimpel
发明人： Frank Klimpel
IPC分类号： B64D33/02
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： A ram air duct flap arrangement (22) comprises at least one ram air duct flap (24, 26) which is designed to close, in a closed position, a ram air inlet (14) or a ram air outlet (18) of a ram air duct (10) and, at least partly open, in an open position, the ram air inlet (14) or the ram air outlet (18) of the ram air duct (10). Furthermore, the ram air duct flap arrangement (22) comprises an actuator (32) for actuating the ram air duct flap (24, 26) between its closed position and its open position. A pressure control device (42) is designed to control a pressure (pi), which, when the ram air duct flap arrangement (22) is mounted in an aircraft, acts on an inner surface (44) of the ram air duct flap (24, 26) facing an interior of the aircraft, in such a way that it corresponds substantially to a pressure (pa) which, when the ram air duct flap arrangement (22) is mounted in an aircraft, acts on an outer surface (38) of the ram air duct flap (24, 26) facing the external environment.
摘要翻译：冲压空气管道翼片装置（22）包括至少一个冲压空气管道挡板（24,26），其设计成在关闭位置关闭压头空气入口（14）或冲压空气出口（18）冲压空气管道（10），并且在打开位置至少部分地打开冲压空气管道（10）的冲压空气入口（14）或冲压空气出口（18）。此外，冲压空气管道翼片装置（22）包括致动器（32），用于在其关闭位置和其打开位置之间致动冲压空气管道挡板（24,26）。压力控制装置（42）被设计成控制压力（pi），当压头空气管道挡板装置（22）安装在飞行器中时，该压力作用在冲压空气管道挡板的内表面（44）上 24,26）面向飞行器的内部，使得其基本上对应于当冲压空气管道翼片装置（22）安装在飞行器中时的压力（pa），其作用在外表面（38 ）的冲击空气管道翼片（24,26）面向外部环境。

6. 发明授权

US08087255B2 Air-conditioning system for aircraft 有权
标题翻译：飞机空调系统
公开(公告)号：US08087255B2
公开(公告)日：2012-01-03
申请号：US12295963
申请日：2007-04-05
申请人： Frank Klimpel
发明人： Frank Klimpel
IPC分类号： F25D17/06
CPC分类号： B64D13/06 , B64D2013/0618 , Y02T50/44 , Y02T50/56
摘要： Air-conditioning system (10) for aircraft, in particular for commercial aircraft, with a bleed air source (12), a bleed air line (22-30) comprising a main valve (16), and an air-conditioning unit (32), wherein a mass air flow conveyed from the bleed air source (12) through the bleed air line (22-30) to the air-conditioning unit (32) can be controlled by means of the main valve (16). According to the invention it is envisaged that a by-pass line (36-50, 58, 60) comprising a by-pass valve (34) and by-passing at least a part (22-26, 16) of the bleed air line, is present between the bleed air source (12) and the air-conditioning unit (32).
摘要翻译：用于飞机的空调系统（10），特别是商用飞机，具有放气源（12），包括主阀（16）和空调单元（32）的排气管线（22-30）），其中通过所述主阀（16）可以控制从所述排气源（12）通过所述排气管线（22-30）输送到所述空调单元（32）的质量空气流。根据本发明，设想包括旁通阀（34）并绕过排气的至少一部分（22-26,16）的旁路管线（36-50,58,60）存在于排气源（12）和空调单元（32）之间。

7. 发明授权

US07727057B2 Device and process for heating an aircraft cabin 有权
标题翻译：用于加热飞机机舱的装置和过程
公开(公告)号：US07727057B2
公开(公告)日：2010-06-01
申请号：US10582594
申请日：2004-12-30
申请人： Jens Beier , Frank Klimpel
发明人： Jens Beier , Frank Klimpel
IPC分类号： B64D13/08 , B64D13/02 , B64D13/00
CPC分类号： B64D13/00 , B64D13/08 , Y02T50/44
摘要： The invention relates to a device (10) for heating an aircraft cabin and comprises a first hot air supply line (12) that leads to an air conditioning unit (14), a flow control valve (16) that is disposed in the first hot air supply line (12) upstream from the air conditioning unit (14), and a second hot air supply line (18) that branches off from the first hot air supply line (12) between the flow control valve (16) and the air conditioning unit (14) and bypasses the air conditioning unit (14). In order to assure air conditioning of the aircraft cabin in the event of a failure of the air conditioning unit (14) a third hot air supply line (20) branches off from the first hot air supply line (12) upstream from the flow control valve (16), which third hot air supply line (20) connects the first hot air supply line (12) to the second hot air supply line (18). Further a first close off mechanism is disposed in the second hot air supply line (18) upstream from the junction with the third hot air supply line (20), which first close off mechanism in its closed position prevents a flow from the second hot air supply line (18) back into the first hot air supply line (12). Finally a second close off mechanism is disposed in the third hot air supply line (20) upstream from the junction with the second hot air supply line (18).
摘要翻译：本发明涉及一种用于加热飞行器机舱的装置（10），包括通向空调单元（14）的第一热空气供应管线（12），设置在第一热的流量控制阀（16）空调装置（14）上游的空气供给管线（12）和从流量控制阀（16）与空气之间的第一热风供给管线（12）分支的第二热风供给管线空调单元（14）并绕过空调单元（14）。为了在空调单元（14）发生故障的情况下确保飞机机舱的空调，第三热空气供应管线（20）从流动控制上游的第一热空气供应管线（12）分支阀（16），其中第三热风供应管线（20）将第一热风供应管线（12）连接到第二热空气供应管线（18）。此外，在与第三热风供应管线（20）的连接处的上游的第二热风供应管线（18）中设置有第一关闭机构，其中第一关闭机构处于其关闭位置，防止来自第二热空气供应管线（18）回到第一热空气供应管线（12）中。最后，在与第二热风供应管线（18）的连接处的上游的第三热风供应管线（20）中设置第二关闭机构。

8. 发明申请

US20090301110A1 Air-Conditioning System For Aircraft 有权
标题翻译：飞机空调系统
公开(公告)号：US20090301110A1
公开(公告)日：2009-12-10
申请号：US12295963
申请日：2007-04-05
申请人： Frank Klimpel
发明人： Frank Klimpel
IPC分类号： F25D17/04 , F25D9/00 , F28B9/00
CPC分类号： B64D13/06 , B64D2013/0618 , Y02T50/44 , Y02T50/56
摘要： Air-conditioning system (10) for aircraft, in particular for commercial aircraft, with a bleed air source (12), a bleed air line (22-30) comprising a main valve (16), and an air-conditioning unit (32), wherein a mass air flow conveyed from the bleed air source (12) through the bleed air line (22-30) to the air-conditioning unit (32) can be controlled by means of the main valve (16). According to the invention it is envisaged that a by-pass line (36-50, 58, 60) comprising a by-pass valve (34) and by-passing at least a part (22-26, 16) of the bleed air line, is present between the bleed air source (12) and the air-conditioning unit (32).
摘要翻译：用于飞机的空调系统（10），特别是商用飞机，具有放气源（12），包括主阀（16）和空调单元（32）的排气管线（22-30）），其中通过所述主阀（16）可以控制从所述排气源（12）通过所述排气管线（22-30）输送到所述空调单元（32）的质量空气流。根据本发明，设想包括旁通阀（34）并绕过排气的至少一部分（22-26,16）的旁路管线（36-50,58,60）存在于排气源（12）和空调单元（32）之间。

9. 发明申请

US20070144729A1 Device and process for heating an aircraft cabin 有权
标题翻译：用于加热飞机机舱的装置和过程
公开(公告)号：US20070144729A1
公开(公告)日：2007-06-28
申请号：US10582594
申请日：2004-12-30
申请人： Jens Beier , Frank Klimpel
发明人： Jens Beier , Frank Klimpel
IPC分类号： F25B9/00 , F24F11/00
CPC分类号： B64D13/00 , B64D13/08 , Y02T50/44
摘要： The invention relates to a device (10) for heating an aircraft cabin and comprises a first hot air supply line (12) that leads to an air conditioning unit (14), a flow control valve (16) that is disposed in the first hot air supply line (12) upstream from the air conditioning unit (14), and a second hot air supply line (18) that branches off from the first hot air supply line (12) between the flow control valve (16) and the air conditioning unit (14) and bypasses the air conditioning unit (14). In order to assure air conditioning of the aircraft cabin in the event of a failure of the air conditioning unit (14) a third hot air supply line (20) branches off from the first hot air supply line (12) upstream from the flow control valve (16), which third hot air supply line (20) connects the first hot air supply line (12) to the second hot air supply line (18). Further a first close off mechanism is disposed in the second hot air supply line (18) upstream from the junction with the third hot air supply line (20), which first close off mechanism in its closed position prevents a flow from the second hot air supply line (18) back into the first hot air supply line (12). Finally a second close off mechanism is disposed in the third hot air supply line (20) upstream from the junction with the second hot air supply line (18).
摘要翻译：本发明涉及一种用于加热飞行器机舱的装置（10），包括通向空调单元（14）的第一热空气供应管线（12），设置在第一热的流量控制阀（16）空调装置（14）上游的空气供给管线（12）和从流量控制阀（16）与空气之间的第一热风供给管线（12）分支的第二热风供给管线空调单元（14）并绕过空调单元（14）。为了在空调单元（14）发生故障的情况下确保飞机机舱的空调，第三热空气供应管线（20）从流动控制上游的第一热空气供应管线（12）分支阀（16），其中第三热风供应管线（20）将第一热风供应管线（12）连接到第二热空气供应管线（18）。此外，在与第三热风供应管线（20）的连接处的上游的第二热风供应管线（18）中设置有第一关闭机构，其中第一关闭机构处于其关闭位置，防止来自第二热空气供应管线（18）回到第一热空气供应管线（12）中。最后，在与第二热风供应管线（18）的连接处的上游的第三热风供应管线（20）中设置第二关闭机构。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式