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1. 发明申请

US20100096118A1 Ram Air Based Cooling And Ventilation System For An Aircraft 有权
标题翻译：基于Ram Air的冷却通风系统
公开(公告)号：US20100096118A1
公开(公告)日：2010-04-22
申请号：US12520240
申请日：2007-12-12
申请人： Thomas Scherer , Ruediger Schmidt , Alexander Solntsev
发明人： Thomas Scherer , Ruediger Schmidt , Alexander Solntsev
IPC分类号： F25B29/00 , B64D13/00 , B60H3/00 , B60H1/34 , F24F7/007
CPC分类号： B64D13/00 , Y02T50/56
摘要： The invention concerns a cooling system for an aircraft with an air inlet (4) through which air from the environment of the aircraft enters a ram air channel (2), and an air outlet (6) through which air emerges from the ram air channel (2). A heat exchanger (10) is arranged in the ram air channel (2). A ventilation device (8) is in fluid communication with the ram air channel (2). Also connected to the ram air channel (2) is a distribution line (12) to cool at least one heat-loaded component of the aircraft, in particular a cabin air conditioning system, and/or to ventilate an installation space of the at least one heat-loaded component.
摘要翻译：本发明涉及一种用于具有空气入口（4）的飞行器的冷却系统，来自飞行器环境的空气通过该进气口进入冲压空气通道（2）和空气出口（6），空气从冲压空气通道（2）。热交换器（10）设置在冲压空气通道（2）中。通风装置（8）与冲压空气通道（2）流体连通。还连接到冲压空气通道（2）的是分配线（12），用于冷却飞机的至少一个加热部件，特别是机舱空调系统，和/或至少使安装空间通风一个热负荷组件。

2. 发明申请

US20100258675A1 Drag-Optimised Ram-Air Duct And Process For Controlling A Mass Flow Of Ambient Air Or Cooling Air Through A Ram-Air Duct 有权
标题翻译：用于通过Ram-Air管道控制环境空气或冷却空气的质量流量的拖拉式优化的Ram-Air管道和过程
公开(公告)号：US20100258675A1
公开(公告)日：2010-10-14
申请号：US12753268
申请日：2010-04-02
申请人： Thomas Scherer , Alexander Solntsev , Ruediger Schmidt
发明人： Thomas Scherer , Alexander Solntsev , Ruediger Schmidt
IPC分类号： B64C1/38
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56 , Y10T137/0645
摘要： A ram-air duct (10) includes a ram-air inlet duct (20) and a ram-air outlet duct (30) arranged downstream of the ram-air inlet duct (20) and in fluid communication with the ram-air inlet duct (20). At an inlet (22) of the ram-air inlet duct (20) a movable element is arranged and adapted to set an inlet parameter (E) of the inlet (22). At an outlet (32) of the ram-air outlet duct (30) a movable element is arranged and adapted to set an outlet parameter (A) of the outlet (32). The outlet parameter (A) and the inlet parameter (E) are linked together by a function (ƒ), so that an outlet parameter (A) corresponding to a value (f(E)) of the function (ƒ) is assigned to each inlet parameter (E).
摘要翻译：冲压空气管道（10）包括冲压空气入口管道（20）和设置在冲压空气入口管道（20）下游并与冲压空气入口流体连通的冲压空气出口管道（30）导管（20）。在冲击空气入口管道（20）的入口（22）处，可移动元件被布置并适于设定入口（22）的入口参数（E）。在压头空气出口管道（30）的出口（32）处，可移动元件被布置并适于设定出口（32）的出口参数（A）。出口参数（A）和入口参数（E）通过功能（ƒ）链接在一起，从而将与功能（ƒ）的值（f（E））对应的出口参数（A）分配给每个入口参数（E）。

3. 发明申请

US20100258655A1 RAM AIR OUTLET DUCT 审中-公开
标题翻译： RAM空气出风口
公开(公告)号：US20100258655A1
公开(公告)日：2010-10-14
申请号：US12755845
申请日：2010-04-07
申请人： Alexander Solntsev , Ruediger Schmidt , Thomas Scherer
发明人： Alexander Solntsev , Ruediger Schmidt , Thomas Scherer
IPC分类号： B05B1/30
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56
摘要： A ram air outlet duct (10) for removing air from an aircraft includes a ram air outlet duct wall (20) bounding an interior (16) of the ram air outlet duct (10), a ram air outlet (12), and a ram air outlet duct flap (22) for adjusting a flow cross-section of the ram air outlet (12). To minimise additional drag caused by the ram air outlet duct (10) when it is mounted in an aircraft and the aircraft is flying, a flap area of to the ram air outlet duct flap (22) is smaller than a cross-sectional area of the ram air outlet (12) and/or the ram air outlet duct wall (20) has a rounded shape in a section (26) adjoining the ram air outlet (12).
摘要翻译：用于从飞行器去除空气的冲压空气出口管道（10）包括限定所述冲压空气出口管道（10）的内部（16）的压头空气出口管道壁（20），冲压空气出口（12）和用于调节冲压气体出口（12）的流动横截面的冲压出气管道挡板（22）。为了最小化冲压出气管道（10）在其安装在飞行器中并且飞行器飞行时引起的附加阻力，冲压气体出口管道挡板（22）的翼片区域小于冲压空气出口（12）和/或冲压出气管道壁（20）在与冲压气体出口（12）相邻的部分（26）中具有圆形形状。

4. 发明授权

US07618008B2 Air supply for an aircraft 有权
标题翻译：飞机供气
公开(公告)号：US07618008B2
公开(公告)日：2009-11-17
申请号：US11632881
申请日：2005-08-11
申请人： Thomas Scherer , Ruediger Schmidt , Alexander Solntsev
发明人： Thomas Scherer , Ruediger Schmidt , Alexander Solntsev
IPC分类号： B64C1/00
CPC分类号： B64D13/06 , B64D37/32 , B64D2013/0677 , Y02T50/44
摘要： Nowadays in aircraft on-board inert gas generation systems (OBIGGS) are used to generate inert gases. Cooled bleed air of engines or auxiliary turbines is fed to said OBIGGS systems. According to an embodiment of the present invention, an air supply device for an OBIGGS system in an aircraft is proposed that comprises a bleed position (1,2). By way of the bleed position (1,2), air from an air conditioning unit (4,5) on board the aircraft can be bled and can be fed to the OBIGGS system. There is thus no need for an additional heat exchanger and an additional ram-air channel. Maintenance expenditure and air resistance are thus reduced.
摘要翻译：如今在飞机上使用惰性气体发生系统（OBIGGS）来生成惰性气体。发动机或辅助涡轮机的冷却排气被供给到所述OBIGGS系统。根据本发明的实施例，提出了一种用于航空器中的OBIGGS系统的空气供应装置，其包括排放位置（1,2）。通过排放位置（1,2），飞机上的空调单元（4,5）的空气可以流出，并可以送到OBIGGS系统。因此，不需要额外的热交换器和附加的冲压空气通道。因此，维护费用和空气阻力减少。

5. 发明申请

US20070267060A1 Cooling of Air in an Aircraft 审中-公开
标题翻译：飞机空气冷却
公开(公告)号：US20070267060A1
公开(公告)日：2007-11-22
申请号：US11573857
申请日：2005-08-11
申请人： Thomas Scherer , Ruediger Schmidt , Alexander Solntsev
发明人： Thomas Scherer , Ruediger Schmidt , Alexander Solntsev
IPC分类号： F17D1/12
CPC分类号： B64D37/32 , B64D13/06 , B64D2013/0677 , Y02T50/44 , Y10T137/0391
摘要： Nowadays in aircraft so-called on-board inert gas generation systems (OBIGGS) are used to generate inert gases, to which OBIGGS cooled bleed air of engines or auxiliary power units is fed. According to an embodiment of the present invention, an air cooling device for an OBIGGS system in an aircraft is proposed that comprises a bleed position. By way of the bleed position, cooling air from an air conditioning unit on board the aircraft can be bled, which cooling air can subsequently be used for cooling supply air for the OBIGGS system. Thus, there is no need for an additional ram-air inlet channel for cooling the supply air. Air resistance and weight are thus reduced, and the stability of the primary structure is enhanced.
摘要翻译：现在在飞机上使用所谓的车载惰性气体发生系统（OBIGGS）来产生惰性气体，OBIGGS冷却发动机或辅助动力装置的排放空气。根据本发明的实施例，提出了一种用于飞行器中的OBIGGS系统的空气冷却装置，其包括排放位置。通过排放位置，飞机上的空调机组的冷却空气可以流出，随后可以使用冷却空气冷却OBIGGS系统的供气。因此，不需要用于冷却供给空气的额外的冲压空气入口通道。因此，降低了空气阻力和重量，提高了一次结构的稳定性。

6. 发明授权

US08262018B2 Drag-optimised ram-air duct and process for controlling a mass flow of ambient air or cooling air through a ram-air duct 有权
标题翻译：拖拉式优化的冲压空气管道和用于通过冲压空气管道控制环境空气或冷却空气的质量流量的过程
公开(公告)号：US08262018B2
公开(公告)日：2012-09-11
申请号：US12753268
申请日：2010-04-02
申请人： Thomas Scherer , Alexander Solntsev , Ruediger Schmidt
发明人： Thomas Scherer , Alexander Solntsev , Ruediger Schmidt
IPC分类号： B64D33/02
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/56 , Y10T137/0645
摘要： A ram-air duct includes a ram-air inlet duct and a ram-air outlet duct arranged downstream of the ram-air inlet duct and in fluid communication with the ram-air inlet duct. At an inlet of the ram-air inlet duct, a first movable element is arranged and adapted to set an inlet parameter of the inlet. At an outlet of the ram-air outlet duct, a second movable element is arranged and adapted to set an outlet parameter of the outlet. The outlet parameter and the inlet parameter are linked together by a function, so that an outlet parameter corresponding to a value of the function is assigned to each inlet parameter. A controller implements the control function by actuating movements of the first and second movable elements.
摘要翻译：冲压空气管道包括冲压空气入口管道和布置在冲压空气入口管道下游并与冲压空气入口管道流体连通的冲压空气出口管道。在冲压空气入口管道的入口处，布置第一可移动元件并适于设定入口的入口参数。在冲压空气出口管道的出口处，布置第二可移动元件并适于设定出口的出口参数。出口参数和入口参数通过功能连接在一起，从而将与功能值对应的出口参数分配给每个入口参数。控制器通过致动第一和第二可移动元件的运动来实现控制功能。

7. 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。

8. 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。

9. 发明授权

US09853287B2 Electrolyte materials for use in electrochemical cells 有权
公开(公告)号：US09853287B2
公开(公告)日：2017-12-26
申请号：US13216538
申请日：2011-08-24
申请人： Yuriy V. Mikhaylik , Igor P. Kovalev , John D. Affinito , Helmut Moehwald , Ruediger Schmidt , Anna Cristadoro , Ingrid Haupt , Raimund Pietruschka
发明人： Yuriy V. Mikhaylik , Igor P. Kovalev , John D. Affinito , Helmut Moehwald , Ruediger Schmidt , Anna Cristadoro , Ingrid Haupt , Raimund Pietruschka
IPC分类号： H01M10/052 , H01M10/056 , H01M10/0565 , H01M4/38 , H01M4/40 , H01M4/58 , H01M2/14 , H01M2/16 , H01M4/36 , H01M4/62 , H01M10/0525 , H01M4/134 , H01M10/0568 , H01M10/0569
CPC分类号： H01M4/581 , H01M2/145 , H01M2/1673 , H01M4/134 , H01M4/366 , H01M4/382 , H01M4/405 , H01M4/5815 , H01M4/62 , H01M10/0525 , H01M10/0565 , H01M10/0568 , H01M10/0569 , H01M2300/0037
摘要： Electrolyte materials for use in electrochemical cells, electrochemical cells comprising the same, and methods of making such materials and cells, are generally described. In some embodiments, the materials, processes, and uses described herein relate to electrochemical cells comprising sulfur and lithium such as, for example, lithium sulfur batteries. The electrolyte can comprise a polymeric material and, in some cases, an absorbed auxiliary material. For example, the electrolyte material can be capable of forming a gel, and the auxiliary material can comprise an electrolyte solvent. In some instances, the electrolyte material can comprise at least one organic (co)polymer selected from polyethersulfones, polyvinylalcohols (PVOH) and branched polyimides (HPI). The non-fluid material in the electrolyte, when configured for use, can, alone or in combination with the optional absorbed auxiliary material, have a yield strength greater than that of lithium metal, in some embodiments.

10. 发明授权

US09577243B2 Use of expanded graphite in lithium/sulphur batteries 有权
标题翻译：在锂/硫电池中使用膨胀石墨
公开(公告)号：US09577243B2
公开(公告)日：2017-02-21
申请号：US13700696
申请日：2011-05-26
申请人： Ruediger Schmidt , Alexander Panchenko , Bastian Ewald , Philip Hanefeld , Sorin Ivanovici , Helmut Moehwald , Igor P. Kovalev
发明人： Ruediger Schmidt , Alexander Panchenko , Bastian Ewald , Philip Hanefeld , Sorin Ivanovici , Helmut Moehwald , Igor P. Kovalev
IPC分类号： H01M4/02 , H01M4/133 , H01M4/136 , H01M4/38 , H01M4/1397 , H01M4/04 , H01M4/62 , H01M10/052
CPC分类号： H01M4/133 , H01M4/0485 , H01M4/136 , H01M4/1397 , H01M4/38 , H01M4/621 , H01M4/625 , H01M10/052 , Y02E60/122
摘要： The present invention relates to a solid composite for use in the cathode of a lithium-sulphur electric current producing cell wherein the solid composite comprises 1 to 75 wt.-% of expanded graphite, 25 to 99 wt.-% of sulphur, 0 to 50 wt.-% of one or more further conductive agents other than expanded graphite, and 0 to 50 wt.-% one or more binder, based on the total amount of the solid composite, a lithium-sulphur electric current producing cell comprising (i) a cathode comprising the solid composite, (ii) an anode and (iii) an electrolyte interposed between said cathode and said anode, and a process for preparing the solid composite comprising the steps (I) preparing a slurry comprising sulphur, expanded graphite, and optionally further components in a liquid medium by dispersing the sulphur, the expanded graphite, and optionally the further components in the liquid medium; (II) casting the slurry provided in step (I) on a substrate or placing the slurry provided in step (I) into a mold; and (III) removing some or all of the liquid medium from the slurry cast in step (II) to form a solid composite.
摘要翻译：本发明涉及一种用于锂 - 硫电流产生电池的阴极的固体复合材料，其中固体复合材料包含1至75重量％的膨胀石墨，25至99重量％的硫，0至 50重量％的膨胀石墨以外的一种或多种其它导电剂和0至50重量％的一种或多种粘合剂，基于固体复合材料的总量，锂 - 硫电流产生电池包含（ i）包含固体复合材料的阴极，（ii）阳极和（iii）介于所述阴极和所述阳极之间的电解质，以及制备所述固体复合材料的方法，包括步骤（I）制备包含硫，膨胀石墨，以及任选地通过将硫，膨胀石墨和任选的其它组分分散在液体介质中的液体介质中的其它组分; （II）将在步骤（I）中提供的浆料浇铸在基材上或将步骤（I）中提供的浆料放入模具中; 和（III）从步骤（II）中浇铸的浆料中除去一些或全部液体介质以形成固体复合材料。

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