公开(公告)号：US6086881A

公开(公告)日：2000-07-11

申请号：US79374

申请日：1998-05-15

申请人： Andreas Frey ,  Marian R. Neutra ,  Frank A. Robey

发明人： Andreas Frey ,  Marian R. Neutra ,  Frank A. Robey

IPC分类号： A61K9/16 ,  A61K9/51 ,  A61K39/385 ,  A61P37/04 ,  C07K14/16 ,  A61K38/00 ,  A61M36/14 ,  C07K5/00

CPC分类号： C07K14/005 ,  A61K39/385 ,  A61K2039/55505 ,  A61K2039/60 ,  A61K2039/627 ,  C12N2740/16122

摘要： The present invention is a spatially aligned conjugated composition which comprises at least one chemically modified substance which is immunologically representative of a prechosen infectious agent and provides a chemical constituent for entering into and forming a thioether bond; a plurality of chemically substituted metallic oxide particles which range from about 10-10,000 nanometers and are able to enter into a thioether bond and covalent linkage; and at least one thioether bond and linkage joining the metallic oxide particles in a controlled and spatially aligned manner to the antigen or hapten. The conjugated composition may be alternatively employed as an immunogen; as a vaccine; as a diagnostic tool and reactant; and as an analytical material suitable for testing the pharmacological activity of new compounds.

摘要翻译： 本发明是空间取向的共轭组合物，其包含至少一种化学修饰的物质，其具有免疫学上代表预先感染的物质并提供用于进入和形成硫醚键的化学成分; 多个化学取代的金属氧化物颗粒，其范围为约10-10,000纳米，并且能够进入硫醚键和共价键; 以及至少一个硫醚键和连接金属氧化物颗粒的控制和空间对准方式与抗原或半抗原的连接。 共轭组合物可以替代地用作免疫原; 作为疫苗; 作为诊断工具和反应物; 并且作为适用于测试新化合物的药理活性的分析物质。

公开(公告)号：US08336329B2

公开(公告)日：2012-12-25

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

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：US20110149517A1

公开(公告)日：2011-06-23

申请号：US13036815

申请日：2011-02-28

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 (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：US20090321062A1

公开(公告)日：2009-12-31

申请号：US12438489

申请日：2007-08-17

申请人： Wolfgang Ebigt ,  Wilson Willy Casas Noriega ,  Andreas Frey ,  Dirk Kastell

发明人： Wolfgang Ebigt ,  Wilson Willy Casas Noriega ,  Andreas Frey ,  Dirk Kastell

IPC分类号： F28F27/00

CPC分类号： F25B25/005 ,  B64D13/06 ,  B64D2013/0629 ,  B64D2013/064 ,  B64D2013/0674 ,  Y02T50/44 ,  Y02T50/56

摘要： A cooling system for cooling heat loads on board an aircraft comprises a cold producing device, a first cold carrier fluid circuit, which is thermally coupled to the cold producing device and is connected to a first heat load in order to carry off heat from the first heat load, and a second cold carrier fluid circuit, which is connected to a second heat load in order to carry off heat from the second heat load. A coupling system of the cooling system is adapted to selectively thermally couple the first cold carrier fluid circuit to the second cold carrier fluid circuit or thermally uncouple it from the second cold carrier fluid circuit. In a method for operating such a cooling system for cooling heat loads on board an aircraft, the first cold carrier fluid circuit is selectively thermally coupled to the second cold carrier fluid circuit or thermally uncoupled from the second cold carrier fluid circuit by means of the coupling system.

摘要翻译： 用于冷却飞机上的热负荷的冷却系统包括冷产生装置，第一冷载体流体回路，其与冷产生装置热耦合并连接到第一热负荷，以便从第一 热负载和第二冷载体流体回路，其连接到第二热负荷以便从第二热负荷传递热量。 冷却系统的联接系统适于选择性地将第一冷载体流体回路耦合到第二冷载体流体回路，或者使其与第二冷载体流体回路热分离。 在用于操作用于冷却飞机上的热负荷的这种冷却系统的方法中，第一冷载体流体回路选择性地热耦合到第二冷载体流体回路，或者通过耦合与第二冷载体流体回路热分离 系统。

公开(公告)号：US07431685B2

公开(公告)日：2008-10-07

申请号：US10239986

申请日：2001-03-28

申请人： Andreas Frey ,  Juergen Helfman ,  Marcus Alexander Schmidt ,  Gerhard Mueller

发明人： Andreas Frey ,  Juergen Helfman ,  Marcus Alexander Schmidt ,  Gerhard Mueller

IPC分类号： C40B50/00

CPC分类号： C07K1/047 ,  B01J19/0046 ,  B01J2219/00286 ,  B01J2219/00306 ,  B01J2219/00317 ,  B01J2219/00353 ,  B01J2219/00378 ,  B01J2219/00414 ,  B01J2219/00418 ,  B01J2219/00486 ,  B01J2219/00511 ,  B01J2219/0052 ,  B01J2219/00522 ,  B01J2219/00527 ,  B01J2219/00585 ,  B01J2219/0059 ,  B01J2219/00596 ,  B01J2219/00605 ,  B01J2219/00612 ,  B01J2219/00617 ,  B01J2219/00619 ,  B01J2219/00621 ,  B01J2219/00626 ,  B01J2219/00637 ,  B01J2219/00659 ,  B01J2219/00707 ,  B01J2219/00722 ,  B01J2219/00725 ,  C07B2200/11 ,  C07K1/045 ,  C40B40/06 ,  C40B40/10 ,  C40B60/14

摘要： The aim of the invention is to investigate the bonding of substances to target molecules. This is achieved by means of a densely packed device wherein various target molecules are bonded in a large number of sample areas. Cross-contamination and evaporation need to be minimized. The active surface of the sample areas have to be maximized. The inventive solution resides in the use of carrier plates, containing densely packed capillary structures and having a very large inner surface despite small outer dimensions. 1000 times more molecules can be bonded than on a flat outer surface of a comparable size. Cross contamination is avoided by the lack of cross links between the capillaries. Evaporation is minimized by a small outer surface. After the inner surface of the capillaries has been silanized, peptides and peptidomimetics are synthesized in a locally targeted manner. The molecular interactions of components of the substance library with active substances in a solution or a suspension are investigated by means of a local resolution optical detection method. Handling, especially cleaning and covering with substances, is carried out in a simple manner by rinsing liquids through the capillary plate.

摘要翻译： 本发明的目的是研究物质与目标分子的结合。 这是通过密集包装的装置实现的，其中各种目标分子结合在大量的样品区域中。 交叉污染和蒸发需要最小化。 样品区域的活性表面必须最大化。 本发明的解决方案在于使用载体板，其包含密集填充的毛细结构，并且尽管具有小的外部尺寸，但具有非常大的内表面。 与可比尺寸的平坦外表面相比，可以结合1000倍的分子。 由于毛细管之间缺少交叉连接来避免交叉污染。 蒸发通过小的外表面最小化。 在毛细血管的内表面已被硅烷化之后，肽和肽模拟物以局部靶向的方式合成。 通过局部分辨光学检测方法研究物质文库的成分与溶液或悬浮液中活性物质的分子相互作用。 通过用毛细管冲洗液体，以简单的方式进行处理，特别是清洁和物质的覆盖。

公开(公告)号：US20070164187A1

公开(公告)日：2007-07-19

申请号：US10570763

申请日：2004-08-10

申请人： Andreas Frey

发明人： Andreas Frey

IPC分类号： A47B97/00

CPC分类号： B64D11/0696 ,  B60N2/01575 ,  B60P7/0815

摘要： The invention relates to a seat securing system for securing air passenger seats to a securing rail (10), whereby the system permits a relative motion between a mounting part (24) and a base body (26) that, in the longitudinal direction of said securing rail (10), can be brought into a fixed position. In this securing position, a locking body (34), which can pivot from a release position and into a locking position and which is subjected to the action of an energy storage device (32), secures the respective detent parts (22, 30) and thus the base body (24) and mounting part (26) on the securing rail (10). Said energy storage device permits a compensation of tolerances so that the inventive fitting always rests securely against the rail (10).

摘要翻译： 本发明涉及一种用于将乘客座椅固定到固定轨道（10）上的座椅固定系统，由此系统允许安装部件（24）和基座主体（26）之间的相对运动，其在所述 固定轨道（10）可以进入固定位置。 在该固定位置，可从释放位置枢转并进入锁定位置并经受能量存储装置（32）的作用的锁定体（34）固定相应的制动部件（22,30） 因此基体（24）和固定轨道（10）上的安装部分（26）。 所述能量存储装置允许补偿公差，使得本发明的配件总是可靠地靠在轨道（10）上。

公开(公告)号：US20060142016A1

公开(公告)日：2006-06-29

申请号：US10529371

申请日：2003-09-01

申请人： Rifat Can ,  Hans-Ulrich Flender ,  Andreas Frey

发明人： Rifat Can ,  Hans-Ulrich Flender ,  Andreas Frey

IPC分类号： H04Q7/20

CPC分类号： H04W36/0094

摘要： A mobile radio telephone system has at least one first radio cell, several radio cells to that are adjacent to the first radio cell and base stations, each of the latter covering one of the radio cells. A sub-group of the adjacent radio cells is determined depending on the position of a mobile station in the first radio cell. The mobile station subsequently measures a quality parameter of only those signals of the base stations associated with the sub-groups of the adjacent radio cells. One possible advantage is that the time required to carry out the measurements is relatively short as a result of the reduction of their number.

摘要翻译： 移动无线电话系统具有至少一个第一无线电小区，与第一无线电小区和基站相邻的几个无线电小区，后者覆盖无线电小区之一。 根据移动台在第一无线电小区中的位置确定相邻无线电小区的子组。 移动台随后测量与相邻无线电小区的子组相关联的基站的那些信号的质量参数。 一个可能的优点是进行测量所需的时间相对较短，因为其数量的减少。

公开(公告)号：US08528348B2

公开(公告)日：2013-09-10

申请号：US12438489

申请日：2007-08-17

申请人： Wolfgang Ebigt ,  Wilson Willy Casas Noriega ,  Andreas Frey ,  Dirk Kastell

发明人： Wolfgang Ebigt ,  Wilson Willy Casas Noriega ,  Andreas Frey ,  Dirk Kastell

IPC分类号： F25B7/00

CPC分类号： F25B25/005 ,  B64D13/06 ,  B64D2013/0629 ,  B64D2013/064 ,  B64D2013/0674 ,  Y02T50/44 ,  Y02T50/56

摘要： An aircraft cooling system for cooling heat loads on board an aircraft includes a cold producing device, a first cold carrier fluid circuit thermally coupled to the cold producing device and connected to a first heat load in order to carry off heat from the first heat load, a second cold carrier fluid circuit connected to a second heat load in order to carry off heat from the second heat load, a heat exchanger disposed in the second cold carrier fluid circuit and configured to thermally couple the second cold carrier fluid circuit to an ambient temperature surrounding the aircraft, and a coupling system configured to selectively thermally couple the first cold carrier fluid circuit to the second cold carrier fluid circuit or thermally uncouple it from the second cold carrier fluid circuit.

摘要翻译： 用于冷却飞机上的热负荷的飞行器冷却系统包括冷产生装置，第一冷载体流体回路，其热连接到冷产生装置并连接到第一热负载以便从第一热负荷传送热量， 第二冷载体流体回路，连接到第二热负荷以便从第二热负荷传递热量;热交换器，设置在第二冷载体流体回路中并且构造成将第二冷载体流体回路热耦合到环境温度 围绕飞行器以及耦合系统，其被配置为选择性地将第一冷载体流体回路耦合到第二冷载体流体回路，或者使其与第二冷载体流体回路热分解。

公开(公告)号：US20110170263A1

公开(公告)日：2011-07-14

申请号：US13036822

申请日：2011-02-28

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 (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.

公开(公告)号：US20100202108A1

公开(公告)日：2010-08-12

申请号：US12708647

申请日：2010-02-19

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 (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。