公开(公告)号：US20050168019A1

公开(公告)日：2005-08-04

申请号：US11051636

申请日：2005-01-27

申请人： Andreas Frey

发明人： Andreas Frey

IPC分类号： B60N2/427 ,  B60R21/055 ,  B64D11/06 ,  B60N2/42

CPC分类号： B64D11/0636 ,  B60N2/42709 ,  B64D11/06

摘要： A seat, in particular an aircraft passenger seat, has a seat component (10) and a backrest component (12) made at least in part of shell components. One shell component (22) is detachably connected to other components of the seat by a fastening mechanism. In the event of sudden introduction of force, as in the event of a crash, the shell component (22) is detached from the other components of the seat. A passive element is created by the shell component. When normal operating forces are present, that is, in the normal operating state of the seat, the passive element retains its position and shape. In the event of introduction of large force impulses, such as in sudden introduction of force in the event of a crash, the passive element is detached from the remaining shell structure of the seat without significant reaction forces being generated, which might cause injury of the seat occupant, and creates a free space in the seat.

摘要翻译： 座椅，特别是飞机乘客座椅具有至少部分壳体部件制成的座椅部件（10）和靠背部件（12）。 一个外壳部件（22）通过紧固机构可拆卸地连接到座椅的其它部件。 在突然引入力的情况下，如在碰撞的情况下，壳体部件（22）与座椅的其它部件分离。 被动元素由shell组件创建。 当存在正常的操作力时，即在座椅的正常操作状态下，被动元件保持其位置和形状。 在引入大的力冲击的情况下，例如在碰撞的情况下突然引入力时，被动元件从座椅的剩余壳体结构脱离，而不产生显着的反作用力，这可能导致 座位乘客，并在座椅上创建一个可用空间。

公开(公告)号：US20130215572A1

公开(公告)日：2013-08-22

申请号：US13846184

申请日：2013-03-18

申请人： Ozan Uluc ,  Ahmet Kayihan Kiryaman ,  Andreas Frey

发明人： Ozan Uluc ,  Ahmet Kayihan Kiryaman ,  Andreas Frey

IPC分类号： H05K7/20

CPC分类号： H05K7/20218 ,  H05K7/20645 ,  H05K7/20681

摘要： The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system, the aircraft electronics cooling system providing a thermal coupling between an electronic device to be cooled and the liquid cooling system of the aircraft. A coolant delivered by the liquid cooling system may flow through a board of the electronic device, through a heat sink on which the electronic device is arranged and/or through a housing in which the electronic device is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.

摘要翻译： 本发明涉及一种用于具有液体冷却系统的飞行器的改进的飞行器电子冷却系统，飞行器电子冷却系统提供待冷却的电子设备与飞机的液体冷却系统之间的热耦合。 由液体冷却系统输送的冷却剂可以通过电子设备布置在其上的散热器和/或通过其中布置电子设备的壳体流过电子设备的板。 在冷却回路中冷却剂可能永久处于液态。 在冷却电子设备的同时，冷却剂至少部分地蒸发。

公开(公告)号：US08438865B2

公开(公告)日：2013-05-14

申请号：US12514742

申请日：2007-11-20

申请人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Carsten Colberg ,  Peter Schwebke ,  Markus Kerber ,  Michael Dreyhaupt

发明人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Carsten Colberg ,  Peter Schwebke ,  Markus Kerber ,  Michael Dreyhaupt

IPC分类号： F25B17/00 ,  F25B15/00 ,  F25B27/00 ,  B60H1/32 ,  F25D17/02 ,  F25D3/00 ,  F25C5/08

CPC分类号： H05K7/20845 ,  B64D13/06 ,  B64D2013/0614 ,  H05K7/20127 ,  H05K7/20218 ,  H05K7/20872 ,  Y02T50/44 ,  Y02T50/56

摘要： A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18), as well as a second adsorber (26) which contains a medium for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18). A control system (22) is adapted to establish or to interrupt a fluid connection between the evaporator (14, 16, 18) and the first and/or the second adsorber(s) (24, 26).

摘要翻译： 用于冷却航空器装置（12）的冷却系统（10）包括用于接收待蒸发的流体（F）的蒸发器（14,16,18），包含介质（28）的第一吸附器（24） 用于吸附在蒸发器（14,16,18）中蒸发的流体（F）以及第二吸附器（26），所述第二吸附器包含吸附流体（F）的介质，所述介质在所述蒸发器 蒸发器（14,16,18）。 控制系统（22）适于建立或中断蒸发器（14,16,18）与第一和/或第二吸附器（24,26）之间的流体连接。

公开(公告)号：US20100101262A1

公开(公告)日：2010-04-29

申请号：US12532278

申请日：2008-03-25

申请人： Ozan Uluc ,  Andreas Frey ,  Sven Reisbach ,  Frank Bliemeister

发明人： Ozan Uluc ,  Andreas Frey ,  Sven Reisbach ,  Frank Bliemeister

IPC分类号： F25D17/04 ,  B65D88/00

CPC分类号： B64D13/00 ,  B64D2013/0614 ,  B64D2013/0629 ,  Y02T50/44 ,  Y02T50/56

摘要： A system (10) for cooling freight goods on board an aircraft comprises a refrigerating apparatus and a cooling station (14) to which cooling energy generated by said refrigerating apparatus is fed by means of a refrigerating medium and which is connected to an air infeed line (29) of an air-conditioning installation of the aircraft, wherein an air outlet aperture (16) of the cooling station (14) is connectable to a freight compartment (24) of the aircraft in order to discharge into said freight compartment (24) air which has been cooled down to a desired temperature.

摘要翻译： 一种用于冷却飞机上的货物的系统（10），包括制冷装置和冷却站（14），所述制冷装置通过冷藏介质供给由所述制冷装置产生的冷却能量，并且连接到空气进料管线 （29），其中所述冷却站（14）的空气出口孔（16）可连接到所述飞行器的货舱（24），以便排放到所述货物舱（24）中 ）空气已被冷却到所需温度。

公开(公告)号：US07697292B2

公开(公告)日：2010-04-13

申请号：US11850712

申请日：2007-09-06

申请人： Ozan Uluc ,  Ahmet Kayihan Kiryaman ,  Andreas Frey

发明人： Ozan Uluc ,  Ahmet Kayihan Kiryaman ,  Andreas Frey

IPC分类号： H05K7/20 ,  F28F7/00 ,  F28F27/00 ,  F28D15/00

CPC分类号： H05K7/20218 ,  H05K7/20645 ,  H05K7/20681

摘要： The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.

摘要翻译： 本发明涉及一种用于具有液体冷却系统（2）的飞行器的改进的飞行器电子冷却系统，飞行器电子冷却系统提供电子设备（40a，40b，40c，40d，42,44）之间的热耦合，以使其成为 冷却和飞机的液体冷却系统（2）。 由液体冷却系统（2）输送的冷却剂可以通过电子设备（42）布置的散热器流过电子设备（40a，40b，40c，40d）的板，和/或通过壳体 其中布置有电子设备（44）。 在冷却回路中冷却剂可能永久处于液态。 在冷却电子设备的同时，冷却剂至少部分地蒸发。

公开(公告)号：US20100051237A1

公开(公告)日：2010-03-04

申请号：US12514742

申请日：2007-11-20

申请人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Carsten Colberg ,  Peter Schwebke ,  Markus Kerber ,  Michael Dreyhaupt

发明人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Carsten Colberg ,  Peter Schwebke ,  Markus Kerber ,  Michael Dreyhaupt

IPC分类号： F28D15/00

CPC分类号： H05K7/20845 ,  B64D13/06 ,  B64D2013/0614 ,  H05K7/20127 ,  H05K7/20218 ,  H05K7/20872 ,  Y02T50/44 ,  Y02T50/56

摘要： A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18), as well as a second adsorber (26) which contains a medium for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18). A control system (22) is adapted to establish or to interrupt a fluid connection between the evaporator (14, 16, 18) and the first and/or the second adsorber(s) (24, 26).

摘要翻译： 用于冷却航空器装置（12）的冷却系统（10）包括用于接收待蒸发的流体（F）的蒸发器（14,16,18），包含介质（28）的第一吸附器（24） 用于吸附在蒸发器（14,16,18）中蒸发的流体（F）以及第二吸附器（26），所述第二吸附器包含吸附流体（F）的介质，所述介质在所述蒸发器 蒸发器（14,16,18）。 控制系统（22）适于建立或中断蒸发器（14,16,18）与第一和/或第二吸附器（24,26）之间的流体连接。

公开(公告)号：US07606534B2

公开(公告)日：2009-10-20

申请号：US10569842

申请日：2004-08-26

申请人： Volker Breuer ,  Andreas Frey

发明人： Volker Breuer ,  Andreas Frey

IPC分类号： H04K3/00 ,  H04B15/00 ,  H04M1/00 ,  H04B1/38

CPC分类号： H04W16/14 ,  H04W36/20

摘要： The reception of a first base station of a first mobile radio system in a first frequency range can be influenced by transmissions, associated with a connection, of at least one subscriber station of a second mobile radio system in a second frequency range adjacent to the first frequency range. A signaling unit of the first mobile radio station transmits a signal which is used to reduce the influence of the transmissions of the subscriber station of the second radio mobile system on the reception of the first base station in the first frequency range.

摘要翻译： 在第一频率范围内的第一移动无线电系统的第一基站的接收可以受到与第一移动无线电系统相邻的第二移动无线电系统的至少一个用户台在与第一频率范围相邻的第二频率范围内的传输的影响 频率范围。 第一移动无线电站的信令单元在第一频率范围内发送用于减少第二无线电移动系统的用户台的传输对第一基站的接收的影响的信号。

公开(公告)号：US20080149764A1

公开(公告)日：2008-06-26

申请号：US11660407

申请日：2005-08-11

申请人： Andreas Frey

发明人： Andreas Frey

IPC分类号： B64D11/06

CPC分类号： B64D11/0696 ,  B60N2/01575 ,  B60N2205/20 ,  Y02T50/46

摘要： The invention relates to a seat fixing device, in particular to an air passenger seat on a floor of an aircraft comprising at least one fastening rail (10) in the form or a hollow profile which is provided with a longitudinal channel (14) delimiting the free flanks (16) of the profile on the top part thereof (12) oriented to the scat, wherein said channel comprises through openings (18) disposed in a predetermined modular dimension which enlarge the free input section and are used for inserting at least one snap-locking part (24) of a locking body (26) which is movable to a clamping position with the profile (16) of the hollow profile (14) by the relative displacement of each snap-locking part (24) in a perpendicular direction with respect to the longitudinal axis (28) of the fastening rail (10). Said invention is characterised in that it provides for the eccentric drive (30) of the locking body (26) for carrying out said relative displacement, thereby making it possible to improve existing devices and syslems by reducing assembly costs on site.

摘要翻译： 本发明涉及一种座椅固定装置，特别涉及一种飞机地板上的乘客座椅，包括至少一个形式的紧固轨道（10）或中空轮廓，该中空轮廓设有纵向通道（14），该纵向通道限定 位于其顶部（12）上的轮廓的自由侧面（16）定向到散粒，其中所述通道包括以预定模块尺寸设置的通孔（18），其扩大自由输入部分并且用于插入至少一个 锁定体（26）的卡扣锁定部分（24）可通过每个卡扣锁定部件（24）在垂直方向上的相对位移而移动到具有中空型材（14）的轮廓（16）的夹紧位置 方向相对于紧固轨道（10）的纵向轴线（28）。 本发明的特征在于，其提供用于执行所述相对位移的锁定体（26）的偏心驱动装置（30），由此可以通过降低现场装配成本来改进现有装置和系统。

公开(公告)号：US20070019582A1

公开(公告)日：2007-01-25

申请号：US10552149

申请日：2004-02-26

申请人： Andreas Frey ,  Jurgen Mayer ,  Olivia Nemethova ,  Lars Wehmeier

发明人： Andreas Frey ,  Jurgen Mayer ,  Olivia Nemethova ,  Lars Wehmeier

IPC分类号： H04Q7/00

CPC分类号： H04W72/085 ,  H04W24/10 ,  H04W92/12

摘要： In a radio communication system, a common channel is provided which is allocated to a plurality of subscribers at the same time for data transmission between a base station and a subscriber station. Measurements regarding the transmission quality are carried out on the common channel and their results are available in the base station. If the transmission quality does not meet a defined criterion, the base station transmits a first message to a controlling radio network controller associated therewith, the first message containing information about the transmission quality and about subscriber stations for which a bad transmission quality was measured. The controlling radio network controller sends a second message which informs serving radio network controllers, associated with the subscriber stations having bad transmission quality and responsible for the configuration of the subscriber stations, about the bad transmission quality.

摘要翻译： 在无线通信系统中，提供公共信道，同时分配给多个用户，用于在基站和用户站之间进行数据传输。 关于传输质量的测量在公共信道上进行，其结果在基站中可用。 如果传输质量不符合定义的标准，则基站向与其相关联的控制无线电网络控制器发送第一消息，第一消息包含关于传输质量的信息以及关于测量传输质量差的用户站。 控制无线网络控制器发送第二消息，其通知与具有差的传输质量的用户站相关联的服务无线电网络控制器，并且负责用户站的配置关于传输质量差。

公开(公告)号：US20060138846A1

公开(公告)日：2006-06-29

申请号：US11072253

申请日：2005-03-07

申请人： Andreas Frey ,  Jurgen Bauer

发明人： Andreas Frey ,  Jurgen Bauer

IPC分类号： A47C7/50

CPC分类号： B64D11/0647 ,  B64D11/06 ,  B64D11/064 ,  B64D11/0649 ,  Y02T50/46

摘要： A passenger seat, an aircraft passenger seat in particular, has seat components such as a seat frame (20), a backrest (12), and a seat cushion carrier (30) with seat cushion (16). The seat depth between backrest (12) and a seat front edge (26) can be varied by an adjustment mechanism (32) with an energy accumulator, such that the seat depth is adjustable and fastenable in desired adjustment positions. The adjustment mechanism has at least one variable-volume energy accumulator. An adjustment position of the seat depth may be associated with each volume level. The seat depth adjustment may be effected essentially free of mechanical components such as sets of levers.

摘要翻译： 乘客座椅，特别是飞机乘客座椅具有诸如座椅框架（20），靠背（12）和具有座垫（16）的座垫支架（30）的座椅部件。 靠背（12）和座椅前边缘（26）之间的座椅深度可以通过具有能量储存器的调节机构（32）来改变，使得座椅深度可调节并且可在适当的调节位置固定。 调节机构具有至少一个可变容量的蓄能器。 座椅深度的调整位置可以与每个音量水平相关联。 座椅深度调整可以基本上不受诸如一组杠杆的机械部件的影响。