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1. 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。

2. 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。

3. 发明授权

US08973867B2 Fresh air inlet for an aircraft 有权
标题翻译：飞机的新鲜空气进口
公开(公告)号：US08973867B2
公开(公告)日：2015-03-10
申请号：US12994911
申请日：2009-05-27
申请人： Johannes Eichholz , Jens Beier , Alexander Solntsev , Ruediger Schmidt
发明人： Johannes Eichholz , Jens Beier , Alexander Solntsev , Ruediger Schmidt
IPC分类号： B64D33/02 , B64C7/00 , B64D13/00
CPC分类号： B64D33/02 , B64C7/00 , B64D13/00 , B64D2033/022 , B64D2241/00 , Y02T50/44 , Y02T50/56
摘要： A fresh air inlet for an aircraft features a ram air inlet with a ram air inlet opening, a secondary air inlet opening separate from the ram air inlet and a movably mounted flap. The flap can be moved into a first or second position, and essentially covers the secondary air inlet opening in the first position and at least partially opens the secondary air inlet opening and extends away from the aircraft body in the second position to shield the ram air inlet opening from foreign matter in the air. The secondary air inlet reduces the pressure loss of the air inlet on the ground or during flight phases with relatively slow speed due to the enlarged cross-sectional surface. The ram air inlet can be optimized for cruising phases, and the energy expenditure for any downstream compressors and flow-induced noises can be considerably reduced.
摘要翻译：用于飞行器的新鲜空气入口具有冲压空气入口，其具有冲压空气入口开口，与冲压空气入口分开的二次空气入口和可移动安装的翼片。翼片可以移动到第一或第二位置，并且在第一位置基本上覆盖二次空气入口开口，并且至少部分地打开二次空气入口开口并在第二位置远离飞行器主体以屏蔽冲压空气入口从空气中的异物进入。二次空气入口由于横截面的扩大而减小了地面空气入口的压力损失或飞行阶段的相对较慢的压力损失。冲压进气口可以针对巡航阶段进行优化，任何下游压缩机和流量引起的噪声的能量消耗都可以大大降低。

4. 发明授权

US08502700B2 Apparatus and method for pressurising an aircraft cabin structure and measuring the amount of leakage of the aircraft cabin structure 有权
标题翻译：用于对飞机机舱结构加压并测量飞机机舱结构的泄漏量的装置和方法
公开(公告)号：US08502700B2
公开(公告)日：2013-08-06
申请号：US12745513
申请日：2007-11-29
申请人： Thomas Uhlendorf , Michael Bielenberg , Matthias Geske , Jens Beier , Juergen Hintze , Michael Diesing-Jester
发明人： Thomas Uhlendorf , Michael Bielenberg , Matthias Geske , Jens Beier , Juergen Hintze , Michael Diesing-Jester
IPC分类号： G08B21/00
CPC分类号： G01M3/3263 , B64F5/60
摘要： An apparatus for pressurizing an aircraft cabin structure and measuring the amount of leakage of the aircraft cabin structure comprises an air supply line which at a first end is connectable to a pressurized air source and which at a second end is connectable to the aircraft cabin structure so as to supply pressurized air from the pressurized air source into the aircraft cabin structure, an air supply valve disposed in the air supply fine, a pressure sensor for sensing the pressure inside the aircraft cabin structure and for providing signals indicative of the pressure inside the aircraft cabin structure, an air discharge line which at a first end is connectable to the aircraft cabin structure and which at a second end is connectable to an air discharge opening so as to discharge air from the inside of the cabin structure to the air discharge opening and an air discharge valve disposed in the air discharge line. An electronic control unit is adapted to control the air supply valve and the discharge valve in dependence on signals provided by the pressure sensor.
摘要翻译：用于对飞机机舱结构加压并测量飞机机舱结构的泄漏量的装置包括供气管线，其在第一端可连接到加压空气源，并且其第二端可连接到飞机机舱结构，因此为了将来自加压空气源的加压空气供应到飞机机舱结构中，设置在空气供应良好的空气供应阀，用于感测飞机机舱结构内的压力并用于提供指示飞机内的压力的信号的压力传感器舱室结构，空气排放管线，其第一端可连接到飞机机舱结构，并且在第二端可连接到排气口，以便将空气从舱室结构的内部排出到排气口，设置在排气管线中的排气阀。电子控制单元适于根据由压力传感器提供的信号来控制供气阀和排放阀。

5. 发明申请

US20110234426A1 Apparatus and method for pressurising an aircraft cabin structure and measuring the amount of leakage of the aircraft cabin structure 有权
标题翻译：用于对飞机机舱结构加压并测量飞机机舱结构的泄漏量的装置和方法
公开(公告)号：US20110234426A1
公开(公告)日：2011-09-29
申请号：US12745513
申请日：2007-11-29
申请人： Thomas Uhlendorf , Michael Bielenberg , Matthias Geske , Jens Beier , Jürgen Hintzë , Michael Diesing-Jester
发明人： Thomas Uhlendorf , Michael Bielenberg , Matthias Geske , Jens Beier , Jürgen Hintzë , Michael Diesing-Jester
IPC分类号： G08B21/18 , G01M3/32
CPC分类号： G01M3/3263 , B64F5/60
摘要： An apparatus (10) for pressurising an aircraft cabin structure (12) and measuring the amount of leakage of the aircraft cabin structure (12) comprises an air supply line (14) which at a first end is connectable to a pressurized air source and which at a second end is connectable to the aircraft cabin structure (12) so as to supply pressurized air from the pressurized air source into the aircraft cabin structure (12), an air supply valve (36) disposed in the air supply line (14), a pressure sensor (50) for sensing the pressure inside the aircraft cabin structure (12) and for providing signals indicative of the pressure inside the aircraft cabin structure (12), an air discharge line (42) which at a first end is connectable to the aircraft cabin structure (12) an which at a second end is connectable to an air discharge opening (44) so as to discharge air from the inside of the cabin structure (12) to the air discharge opening (44), and an air discharge valve (48) disposed in the air discharge line (42). An electronic control unit (ECU) is adapted to control the air supply valve (36) and the discharge valve (48) in dependence on signals provided by the pressure sensor (50) so as to supply pressurized air into the aircraft cabin structure (12) until a first predetermined pressure level is reached inside the aircraft cabin structure (12), to maintain the pressure inside the aircraft cabin structure (12) at the first predetermined level for a first predetermined period of time, and thereafter to discharge air from the inside of the aircraft cabin structure (12).
摘要翻译：用于对飞机机舱结构（12）加压并测量飞机机舱结构（12）的泄漏量的装置（10）包括供气管线（14），其在第一端可连接到加压空气源，并且其中在第二端可连接到飞机机舱结构（12），以便将加压空气从加压空气源供应到飞行器机舱结构（12）中，设置在空气供应管线（14）中的供气阀（36），用于感测飞行器机舱结构（12）内的压力并用于提供指示飞机机舱结构（12）内的压力的信号的压力传感器（50），在第一端可连接的排气管（42）到机舱结构（12），其在第二端可连接到排气口（44），以将空气从舱室结构（12）的内部排出到排气口（44），并且排气阀（48）设置在空气排出口中拱形线（42）。电子控制单元（ECU）适于根据由压力传感器（50）提供的信号来控制供气阀（36）和排放阀（48），以便将加压空气供应到飞机机舱结构（12 ），直到在飞机机舱结构（12）内达到第一预定压力水平，以将飞机机舱结构（12）内的压力保持在第一预定水平上第一预定时间段，之后将空气从飞机舱内部结构（12）。

6. 发明申请

US20110136425A1 FRESH AIR INLET FOR AN AIRCRAFT 有权
标题翻译：新鲜空气入口飞机
公开(公告)号：US20110136425A1
公开(公告)日：2011-06-09
申请号：US12994911
申请日：2009-05-27
申请人： Johannes Eichholz , Jens Beier , Alexander Solntsev , Ruediger Schmidt
发明人： Johannes Eichholz , Jens Beier , Alexander Solntsev , Ruediger Schmidt
IPC分类号： B64D13/00
CPC分类号： B64D33/02 , B64C7/00 , B64D13/00 , B64D2033/022 , B64D2241/00 , Y02T50/44 , Y02T50/56
摘要： The invention relates to a fresh air inlet for an aircraft that features at least one ram air inlet with at least one ram air inlet opening, at least one secondary air inlet opening that is spaced apart from the ram air inlet and at least one movably mounted flap, wherein the flap can be moved into a first position and into a second position, and wherein the flap essentially covers the secondary air inlet opening in the first position and at least partially opens the secondary air inlet opening and at least in certain areas extends into the air flow directed toward the ram air inlet opening in order to shield the ram air inlet opening from foreign matter in the second position. The air inlet according to the invention makes it possible to reduce the pressure loss of the air inlet on the ground or during flight phases with relatively slow speed due to the enlarged cross-sectional surface. This results in that the actual ram air inlet can be optimized for cruising phases, and that the energy expenditure for any downstream compressors and flow-induced noises can be considerably reduced.
摘要翻译：本发明涉及一种用于飞机的新鲜空气入口，其具有至少一个冲压空气入口，其具有至少一个冲压空气入口，至少一个与冲压空气入口间隔开的二次空气入口，以及至少一个可移动地安装翼片，其中所述翼片可以移动到第一位置并进入第二位置，并且其中所述翼片在所述第一位置基本上覆盖所述次级空气入口开口并且至少部分地打开所述次级空气入口开口，并且至少在某些区域延伸进入朝向冲压空气入口开口的空气流中，以便将冲压空气入口与第二位置的异物屏蔽。根据本发明的空气入口使得可以由于横截面增大而以相对较慢的速度减小地面上空气入口或飞行阶段的压力损失。这导致实际的冲压进气口可以针对巡航阶段进行优化，并且可以大大减少任何下游压缩机和流动引起的噪声的能量消耗。

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