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1. 发明申请

WO2012041773A3 RECEIVER FOR SOLAR ENERGY PRODUCTION INSTALLATIONS 审中-公开
标题翻译：接收器，用于太阳能生产设施
公开(公告)号：WO2012041773A3
公开(公告)日：2012-11-15
申请号：PCT/EP2011066574
申请日：2011-09-23
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , KRAFTANLAGEN MUENCHEN GMBH , HOFFSCHMIDT BERNHARD , KOLL GERRIT
发明人： HOFFSCHMIDT BERNHARD , KOLL GERRIT
IPC分类号： F24J2/07 , F24J2/28 , F24J2/46
CPC分类号： F24J2/07 , F24J2/28 , F24J2/4625 , Y02E10/41 , Y02E10/44
摘要： The invention relates to a high-temperature receiver for solar power stations, especially for heliostat power stations, with air as a heat transfer medium. The receiver has a supporting structure (14), which bears a number of rows of receiver modules (13) that use absorber elements (36) to capture the solar radiation. The absorber elements take in outside air and discharge it as hot air (25) through hot-air tubes (24). To cool the hot-air tubes (24), cooling jackets (26) are provided inside the hollow space (15). The cooling is performed using returned air that generally still contains residual heat. This is blown out from outlet nozzles (41), which are arranged before the front sides (36a) of the adjacent absorber modules, and so the returned air that is expelled is taken in by a number of absorber modules. As a result, energy losses are largely avoided and a high level of efficiency is achieved.
摘要翻译：本发明涉及一种高温接收器，用于太阳能发电厂，尤其是用于使用空气作为传热介质定日镜发电厂。该接收器包括一个支承结构（14）承载多个接收器模块（13）的行的该捕获的太阳辐射吸收体（36）。通过吸收体外部的空气被吸入和热空气（25）通过热空气管（24）排出。用于冷却热空气管（24）的空腔（15）的内部设置冷却套（26）。冷却发生与回风，这.A。仍含有余热。这被吹出的吹出喷嘴（41），其是相对于相邻吸收器模块的前侧（36A）被向前移位，从而使排出的返回空气通过的多个的时间吸收模块吸入的。此能量损失可以在很大程度上避免和有更高的效率水平。

2. 发明申请

WO2010145970A3 METHOD FOR GENERATING SUPERHEATED STEAM IN A SOLAR THERMAL POWER PLANT, AND SOLAR THERMAL POWER PLANT 审中-公开
标题翻译：方法产生过热蒸汽，太阳能热电站和太阳能热发电厂
公开(公告)号：WO2010145970A3
公开(公告)日：2012-08-23
申请号：PCT/EP2010057982
申请日：2010-06-08
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , FELDHOFF JAN FABIAN , ECK MARKUS
发明人： FELDHOFF JAN FABIAN , ECK MARKUS
IPC分类号： F22B1/00 , F22B29/08
CPC分类号： F22B1/006 , F22B29/08 , Y02E10/46
摘要： The invention relates to a method for generating superheated steam in a solar thermal power plant, wherein steam is generated by solar energy in an evaporator area in a flow passage for heat transfer medium, and the steam is superheated by solar energy in a superheater area, wherein a terminal evaporation point of the evaporator area is positionally fixed in a control process, wherein a spatial temperature gradient in the superheater area and a temperature in the evaporator area are determined and the mass flow of heat transfer medium in the flow passage is adjusted as a function of the temperature gradients and the measured temperature in the evaporator area.
摘要翻译：一种用于在太阳能热电站产生过热蒸汽的，其中，在用于通过在蒸发器部分太阳能热传递流体的连续路径，在通过蒸汽的太阳能过热器区中产生和过热蒸汽，其中，蒸发器部分的蒸发结束点在固定就位在一个控制方法的工序这在过热器区域和温度的空间温度在蒸发器部分和传热介质的在输送管线中的温度梯度的函数，并且所测量的温度的质量流量来确定在蒸发器区域进行调整。

3. 发明申请

WO2010086383A3 DUAL BAND ANTENNA, IN PARTICULAR FOR SATELLITE NAVIGATION APPLICATIONS 审中-公开
标题翻译：双频天线，特别是卫星导航应用
公开(公告)号：WO2010086383A3
公开(公告)日：2011-03-03
申请号：PCT/EP2010051021
申请日：2010-01-28
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , HECKLER MARCOS VINICIO THOMAS , NOVA LAVADO ENRIQUE
发明人： HECKLER MARCOS VINICIO THOMAS , NOVA LAVADO ENRIQUE
IPC分类号： H01Q5/10 , H01Q9/04 , H01Q1/24 , H01Q1/38
CPC分类号： H01Q9/0414 , H01Q1/243 , H01Q1/38 , H01Q1/521 , H01Q9/0428 , H01Q9/0457
摘要： The invention relates to a dual band antenna, in particular for satellite navigation applications, comprising a multilayer structure that is provided with an upper first antenna element (12) for receiving electromagnetic waves having a frequency in a first frequency band, a lower second antenna element (16) arranged below the first antenna element (12) for receiving electromagnetic waves having a frequency in a second frequency band, a first and a second electrically conductive ground layer (20,28) that are arranged one above the other and that are arranged in turn below the lower second antenna element (16), and a conducting-track layer (24) having at least one first conducting track (30,32) for electromagnetically coupling with the first antenna element (12) and having at least one second conducting track (34,36) for electromagnetically coupling with the second antenna element (16). The first ground layer (20) facing the lower second antenna element (16) comprises a hole (40,42), below which the at least one second conducting track (34,36) extends. The at least one first conducting track (30,32) is connected to the upper first antenna element (12) by means of an electrical conductor (46,48) that extends through the first ground layer (20) and the lower second antenna element (16) in such a way that the electrical conductor is electrically insulated from the first ground layer and the lower second antenna element. Furthermore, the multilayer structure is provided with a first line adjustment element (58,60,62,64) coupled with the at least one first conducting track (30,32) for suppressing the coupling into the first conducting track (30,32) of electromagnetic waves having a frequency in the second frequency band that are received by means of the lower second antenna element (16) and coupled into the electrical conductor (46,48), a second line adjustment element (44) coupled with the at least one second conducting track (34,36) for suppressing the coupling into the second conducting track (34,36) of electromagnetic waves in the first frequency band that are received by means of the upper first antenna element (12), and several dielectric layers (14,18,22,26) that are arranged between the antenna elements (12,16), ground layers (20,28), and conducting-track layer (24) that lie one above the other.
摘要翻译：该双频带天线，特别是用于卫星导航应用，具有被设置用于在第一频带中接收电磁波的多层结构中，第一天线以下元件（12）设有一上部第一天线元件（12），其具有的频率较低的第二的天线元件（16），用于以第二频带接收具有频率的电磁波，其被依次布置在下第二天线元件（16）下面两个叠置的第一和第二导电接地层（20,28），以及一布线层（24）用于与所述第一天线元件（12）和用于与所述第二天线元件（16）电磁耦合的至少一个第二导体路径（34,36）的电磁耦合的至少一个第一导体路径（30,32）。面对所述第一接地层（20）的下第二天线元件（16）具有凹部（40,42），低于该至少一个第二导体路径（34,36）延伸。所述至少一个第一导体轨道（30,32）是通过所述第一接地层（20）和下部第二天线元件（16）通过并用这些延伸电隔离延伸的电导体（46,48）的装置，第一与上连接到天线元件（12）。此外，该多层结构被用于耦合的抑制经由下第二天线元件（16）设置有耦合到所述至少一个第一互连的输入端（30,32）第一Leitungsanpasselement（58,60,62,64）和接收（在电导体46 ，48），其耦合具有在第二频带在所述第一导体路径（30,32）的频率，耦合到所述至少一个第二导体路径（34,36）的第二Leitungsanpasselement（44），用于从上部第一天线元件上方抑制干扰的输入的电磁波（12）在所述重叠的天线元件（12,16），所述块状物层（20,28）和之间的第二导体轨道（34,36）和多个介电层的（14,18,22,26）接收的电磁波在所述第一频带提供布置布线层（24）。

4. 发明申请

WO2010124875A3 METHOD AND DEVICE FOR DETERMINING WARNINGS IN A SENSOR-ASSISTED EARLY WARNING SYSTEM 审中-公开
标题翻译：方法和装置在传感器基础的早期预警系统中确定警告
公开(公告)号：WO2010124875A3
公开(公告)日：2010-12-23
申请号：PCT/EP2010002661
申请日：2010-04-30
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , POST JOACHIM , ZOSSEDER KAI , WEGSCHEIDER STEPHANIE , MUECK MATTHIAS , RAAPE ULRICH , STEINMETZ TILMANN , UNIV WUERZBURG J MAXIMILIANS
发明人： POST JOACHIM , ZOSSEDER KAI , WEGSCHEIDER STEPHANIE , MUECK MATTHIAS , RAAPE ULRICH , STEINMETZ TILMANN
IPC分类号： G08B21/10
CPC分类号： G08B21/10
摘要： The invention relates to a system and method for the computer-assisted processing and evaluation of information generated by a plurality of sensors in an early warning system for detecting natural events or technical events. The sensors of the early warning system are associated with a predetermined spatial region. One or more propagation models indicate one or more spatially and temporally differentiated effect curves depending on different predetermined information. A spatially and temporally differentiated effect curve is determined on the basis of the captured information and the propagation models, wherein the propagation models are used to calculate a corresponding likely effect curve of the event. One or more reaction models indicate a time frame depending on different predetermined effect curves or different predetermined propagations models, wherein the time frame corresponds to a previously established time that is necessary for initiating protective measures in the corresponding spatial region. A warning information signal is calculated on the basis of the calculated spatially and temporally differentiated effect curve and reaction models.
摘要翻译：本发明涉及一种由多个传感器生成的早期预警系统，用于检测自然灾害或技术事件为基于计算机的处理和评价信息的系统和方法。与给定的地理区域相关的预警系统的传感器。的一个或多个传播模型指定为不同的预定信息的功能的一个或多个有区别的空间和时间效应曲线。分化的空间和时间效应曲线是基于所述检测信息和所述传播模型来确定，该传播模型用于计算一个对应的可能碰撞的情况下的过程。一个或多个反应的模型指定根据各种预定冲击梯度，或各种预定传播模型的一段时间，其中需要的预定时间的时间段采取在相应的子区域的保护作用。一个警告信息信号是基于计算的区别在空间和时间的影响过程和响应模型计算。

5. 发明申请

WO2006042490A9 PRE-TACTICAL CONTROL DEVICE 审中-公开
标题翻译：预战术控制装置
公开(公告)号：WO2006042490A9
公开(公告)日：2007-09-20
申请号：PCT/DE2005001597
申请日：2005-09-13
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , FLUGSICHERUNG GMBH DEUTSCHE , PICK ANDREAS , PIEKERT FLORIAN , ALBERT OLIVER FRANZ , KAUFHOLD RAINER
发明人： PICK ANDREAS , PIEKERT FLORIAN , ALBERT OLIVER FRANZ , KAUFHOLD RAINER
IPC分类号： G08G5/00
CPC分类号： G08G5/0043
摘要： Disclosed is a pre-tactical control device (1) for controlling traffic, which is to be connected to a tactical control system (2) used for assigning times of traffic events that are to be respected by means of transport at defined traffic junctions. Said pre-tactical control device (1) establishes target times (t z ) for traffic events of individual means of transport at the defined traffic junctions within a pre-tactical control time horizon which is greater than a tactical control time horizon of the tactical control system (2), the pre-tactical control device (1) comprising at least one assigned time of a traffic event. The target times (t z ) are determined at least in accordance with predefined traffic plans (FP), updates to said traffic plans (FP'), and predictions about the traffic capacities (KAP(t)) that can be handled at a traffic junction over time such that the target times (t z ) optimize the traffic events at the traffic junction regarding the capacity while respecting the traffic capacities (KAP(t)) that can be handled at a traffic junction, respecting the predefined traffic plans (FP), and keeping planning and controlling processes stable. The target times (t z ) are introduced into the tactical control system (2) as control parameters.
摘要翻译：预战术控制设施（1）的流量控制，其被提供用于连接到战术控制系统（2），用于交通事件时间，其必须遵循的指定传输节点的传输分配，设定目标时间（T _{ž），用于个人交通事件运输到在预战术控制时间段所定义的业务节点固定大于战术控制系统（2）的策略控制时间段和包括至少一个分配的业务事件的时间。目标时间（T _{ž）至少为预定的流量计划（FP）功能，更新的交通计划（FP“）和大约预测的（随时间显影通信量容量KAP（t）的一个业务节点）确定为使得目标时间（T _{ž）优化在交通节点的交通事件在容量方面（符合在处理的业务节点通信量容量KAP（t））的，在预定的流量计划遵守（FP）下规划和管理优化的稳定性。目标时间（T _{ž）在这里进行与控制参数到战术控制系统（2）。}}}}

6. 发明申请

WO2006010502A2 BEAM CONTROL SURFACE AND METHOD FOR THE PRODUCTION OF A BEAM CONTROL SURFACE 审中-公开
标题翻译：雷·拉登和方法生产喷气RUDERS的
公开(公告)号：WO2006010502A2
公开(公告)日：2006-02-02
申请号：PCT/EP2005007761
申请日：2005-07-16
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , HEIDENREICH BERNHARD , ZUBER CHRISTIAN
发明人： HEIDENREICH BERNHARD , ZUBER CHRISTIAN
IPC分类号： F42B10/66 , F02K9/90
CPC分类号： F42B10/665 , F02K9/90 , F02K9/974 , Y10T29/49337 , Y10T156/1031
摘要： The invention relates to a beam control surface which can be used in hot gas flows. Said beam control surface comprises a wing which comprises a core area and a covering layer area which surrounds the core area. The covering layer area is made of a fibre-reinforced material and the fibres in the covering layer area are orientated in an essentially parallel manner in relation to the wing surface and/or the covering layer area is made of a fibre-reinforced material which is reinforced with short fibres.
摘要翻译：提供了一种用于在热气体流中使用的推进器，带有一个翼，其包括芯区域和覆盖皮肤区域的环绕芯区，其中所述覆盖的皮肤区域由纤维增强材料制成，并且其中，在所述盖的皮肤区域中的纤维取向基本上平行于所述翼面和/ 或其中所述覆盖的皮肤区域是由一个用短纤维，纤维增强材料增强。

7. 发明申请

WO2005056643A2 PRODUCTION OF AEROGELS CONTAINING FILLERS 审中-公开
标题翻译：填料气凝胶的生产
公开(公告)号：WO2005056643A2
公开(公告)日：2005-06-23
申请号：PCT/EP2004012402
申请日：2004-11-03
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , RATKE LORENZ , BRUECK SABINE
发明人： RATKE LORENZ , BRUECK SABINE
IPC分类号： C04B14/06 , C04B14/24 , C04B14/30 , C04B20/00 , C04B26/12 , C04B28/24 , C04B30/00 , C04B38/00 , C08J
CPC分类号： C04B38/0022 , C04B26/12 , C04B28/24 , C04B30/00 , C04B14/24 , C04B40/0263 , C04B14/302 , C04B40/0268 , C04B38/0045 , C04B14/064 , C04B14/028 , C04B14/301
摘要： The invention relates to a method for producing an aerogel that contains a filler and has an extremely low thermal conductivity. The aerogel moulded body contains an inorganic filler with a thermal conductivity of up to 0.5 Wm K .
摘要翻译：含填料的制备气凝胶的本发明是一种用于Hertstellung含有填料的气凝胶具有极低的热导率的方法。包含具有至多0.5了Wm <-1>ķ<-1>的热传导性的无机填料，气凝胶模塑制品。

8. 发明申请

WO0218121A9 METHOD AND DEVICE FOR INSERTING PREPREG LAYERS INTO SHAPING TOOLS 审中-公开
标题翻译：在工具工具中引入纤维层的方法和布置
公开(公告)号：WO0218121A9
公开(公告)日：2002-09-19
申请号：PCT/EP0109949
申请日：2001-08-29
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , INVENT INNOVATIVE VERBUNDWERKS , SAERTEX WAGENER GMBH & CO KG , ROTH EKKEHARD , SCHOEPPINGER CARSTEN , HERMANN AXEL , KLEINEBERG MARKUS , PABSCH ARNO
发明人： ROTH EKKEHARD , SCHOEPPINGER CARSTEN , HERMANN AXEL , KLEINEBERG MARKUS , PABSCH ARNO
IPC分类号： B29C70/30 , B29C70/54
CPC分类号： B29C70/30 , B29C70/541 , B29C70/543
摘要： The invention relates to a method for inserting prepreg layers (21, 22, 23) into shaping tools (10) while producing component parts from fiber reinforced composite materials. The inventive method involves the use of a rigid supporting structure (30) having a gas-permeable top side (32) whose outer contour corresponds to the inner contour of the shaping tool (10) for the component part. The wall thickness of the component part is thinner than the inner contour of the shaping tool (10). The interior (31) of the supporting structure (30) is subjected to a pressure that is low relative to the outside pressure. One or more prepreg layers (21, 22, 23) are placed in succession on the gas-permeable top side (32) of the supporting structure (30). The supporting structure (30) with the prepreg layers (21, 22, 23) placed thereon is inserted into the shaping tool (10) in the existence of a low pressure that continues to prevail inside the interior (31) of the supporting structure (30). While doing this, it is ensured that the prepreg layers (21, 22, 23) are arranged between the inner contour of the shaping tool (10) and the outer contour of the top side (32) of the supporting structure (30). Next, the low pressure inside the interior (31) of the supporting structure (30) is discontinued. Lastly, the supporting structure (30) is removed from the shaping tool (10).
摘要翻译：在用于模制插入预浸料层（21，22，23）的方法，管芯（10）在制造部件的由具有气体透过性的上侧（32）的纤维复合材料，刚性支撑结构（30）被使用时，（成形工具的内轮廓的外轮廓 10）对应于设备。尺寸小于模制工具（10）的内部轮廓的尺寸小于部件的壁厚。支撑结构（30）的内部（31）被置于相对于外部压力的负压下。一层或多层纤维层（21,22,23）连续沉积在支撑结构（30）的透气上侧（32）上。所述支撑结构（30）置于与纤维层（21，22，23）被引入与在所述支撑结构（30）在所述模具（10）通行的负压的内部（31）继续进行。确保模具（10）的内轮廓和支撑结构（30）的上侧（32）的外轮廓之间的纤维层层（21,22,23）被布置。然后，关闭支撑结构（30）的内部（31）中的负压。最后将支撑结构（30）从模具（10）中移除。

9. 发明申请

WO9933089A3 METHOD AND DEVICE FOR DETECTING SAMPLE MOLECULES IN A CARRIER GAS 审中-公开
标题翻译：用于确定载气中样品分子的方法和装置
公开(公告)号：WO9933089A3
公开(公告)日：1999-09-30
申请号：PCT/EP9808069
申请日：1998-12-10
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , GROTHEER HORST HENNING , OSER HARALD , THANNER REINHOLD
发明人： GROTHEER HORST-HENNING , OSER HARALD , THANNER REINHOLD
IPC分类号： F16K15/18 , F16K31/06 , H01J49/04 , H01J49/40 , H01J49/16
CPC分类号： F16K31/0655 , F16K15/183 , H01J49/0422 , H01J49/162
摘要： A method for detecting the presence of sample molecules in a carrier gas. According to said method, a divergent jet of carrier gas is produced in a vacuum by expanding gas through a nozzle and the sample molecules are ionised into sample molecules in an ionisation area of the carrier gas jet by means of photon absorption. The sample molecules are pulled into a mass spectrometer by an electrical field where they are detected. In order to improve this method, the distance between the discharge opening of the nozzle and the ionisation area can be chosen freely. The ions from the sample molecule are substantially pulled into the mass spectrometer in the direction of the axis of the carrier gas jet.
摘要翻译：为载气，其中，发散载体气体射流是通过所述载气的膨胀的装置通过喷嘴到产生真空的检测试样分子的方法，所述样品分子通过光子的吸收离子化在载体气体射流的电离通过电抽选区进行采样分子离子和样品分子离子被吸引到质谱仪并且在这样的改进，该喷嘴的出口开口和所述电离之间的距离可以自由选择的方式在质谱仪检测，根据其建议，所述样品分子离子抽入质谱仪基本上沿着载体气体射流的轴线的方向上的本发明是。

10. 发明申请

WO2012150137A3 PROTECTIVE DEVICE AND METHOD FOR PROTECTING A PRESSURE CONTAINER 审中-公开
标题翻译：保护装置及方法用于保护打印TANK
公开(公告)号：WO2012150137A3
公开(公告)日：2013-05-02
申请号：PCT/EP2012057265
申请日：2012-04-20
申请人： DEUTSCH ZENTR LUFT & RAUMFAHRT , BRINNER ANDREAS
发明人： BRINNER ANDREAS
IPC分类号： F17C1/06 , F17C13/08
CPC分类号： F17C1/06 , F17C13/084 , F17C2201/0109 , F17C2201/056 , F17C2203/0604 , F17C2203/0619 , F17C2203/0636 , F17C2203/0663 , F17C2205/0107 , F17C2205/0111 , F17C2205/0115 , F17C2205/0126 , F17C2205/0169 , F17C2205/0196 , F17C2205/0308 , F17C2205/0323 , F17C2205/0397 , F17C2221/012 , F17C2223/0123 , F17C2223/036 , F17C2260/011 , F17C2260/012 , F17C2270/0105 , F17C2270/0168 , F17C2270/0189 , F17C2270/0194 , Y02E60/321
摘要： The aim of the invention is to create a protective device for a pressure container for storing a pressurised gas, which device has a low mass and can be produced cost-effectively. Said aim is achieved in that the protective device comprises a protective case for encasing the pressure container and a safety case for encasing the protective case, wherein the safety case comprises a material that contracts when heated.
摘要翻译：为了提供一种用于压力容器的保护装置，用于存储具有低质量和廉价以产生加压气体，建议的是，保护装置包括一个保护盖，用于覆盖所述压力容器和用于封闭所述保护性护套安全护套，安全鞘包括在加热下收缩的材料。

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