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1. 发明申请

US20090007482A1 Sulfur Evaporator 审中-公开
标题翻译：硫蒸发器
公开(公告)号：US20090007482A1
公开(公告)日：2009-01-08
申请号：US12166841
申请日：2008-07-02
申请人： Peter Sewzyk , Wolfgang Erdmann
发明人： Peter Sewzyk , Wolfgang Erdmann
IPC分类号： A01M13/00 , B01D1/02
CPC分类号： A01M1/2077
摘要： A fumigation apparatus (1) includes a sulfur evaporator (3) including a heat source (28) and a container (9). The heat source (28) includes an electrically operated heating coil (15). The container (9) includes a wall (11) and an inner space (13). The inner space (13) is designed and arranged to store sulfur (14) to be evaporated therein. The container (9) substantially is made of ceramic material. The heat source (28) and the container (9) are designed as one common structural unit. The heating coil (15) at least partly is arranged in the wall (11) of the container (9) such that it is embedded in the ceramic material.
摘要翻译：熏蒸装置（1）包括包括热源（28）和容器（9）的硫蒸发器（3）。热源（28）包括电动加热线圈（15）。容器（9）包括壁（11）和内部空间（13）。内部空间（13）设计和布置成存储要在其中蒸发的硫（14）。容器（9）基本上由陶瓷材料制成。热源（28）和容器（9）被设计为一个共同的结构单元。加热线圈（15）至少部分地布置在容器（9）的壁（11）中，使得其嵌入陶瓷材料中。

2. 外观设计

USD622813S1 Electric sulphur evaporator 有权
标题翻译：电硫蒸发器
公开(公告)号：USD622813S1
公开(公告)日：2010-08-31
申请号：US29299819
申请日：2008-01-04
申请人： Peter Sewzyk , Wolfgang Erdmann
设计人： Peter Sewzyk , Wolfgang Erdmann

3. 发明授权

US07688084B2 Testing apparatus and method for detecting a contact deficiency of an electrically conductive connection 失效
标题翻译：用于检测导电连接的接触不足的测试装置和方法
公开(公告)号：US07688084B2
公开(公告)日：2010-03-30
申请号：US12308159
申请日：2006-06-02
申请人： Wolfgang Erdmann , Eckehard Zuendorf
发明人： Wolfgang Erdmann , Eckehard Zuendorf
IPC分类号： G01R31/302
CPC分类号： G01R31/045
摘要： A testing apparatus and a method for detecting a contact deficiency of an electrically conductive connection. The testing apparatus comprises a measuring chamber, in which several system elements of the connection that are connected in an electrically conductive fashion are positioned, a heat radiator that is supplied with energy and the transferred thermal radiation of which is emitted into the measuring chamber and directed toward the region of the system elements that, after having been heated, generate a thermal field of the insulated and the metallic system components of these connected system elements, a thermal (image) acquisition unit for optically capturing the generated thermal field and for realizing a signal conversion into a thermal image of the connected system elements, and a thermal (image) reproduction unit for the visual reproduction of the converted thermal image.
摘要翻译：一种用于检测导电连接的接触不足的测试装置和方法。测试装置包括测量室，其中以导电方式连接的多个连接的系统元件被定位，提供能量的散热器，并且其传递的热辐射被发射到测量室中并被引导朝向系统元件的区域，其在加热之后产生这些连接的系统元件的绝缘体和金属系统部件的热场，热（图像）获取单元，用于光学捕获产生的热场并实现信号转换成连接的系统元件的热图像，以及用于视觉再现转换的热图像的热（图像）再现单元。

4. 发明授权

US07047739B2 Exhaust-gas turbocharger for an internal combustion engine 失效
标题翻译：用于内燃机的排气涡轮增压器
公开(公告)号：US07047739B2
公开(公告)日：2006-05-23
申请号：US10946375
申请日：2004-09-21
申请人： Peter Fledersbacher , Siegfried Sumser , Helmut Finger , Wolfgang Erdmann
发明人： Peter Fledersbacher , Siegfried Sumser , Helmut Finger , Wolfgang Erdmann
IPC分类号： F02D23/00 , F02B37/12 , F01D17/14 , F01D17/16 , F01D9/02
CPC分类号： F01D17/143 , F01D9/026 , F01D17/167 , F01N13/107 , F02B37/025 , F02B37/22 , F05D2220/40 , Y02T10/144
摘要： An exhaust-gas turbocharger in an internal combustion engine having a compressor in the induction tract and an exhaust-gas turbine in the exhaust-gas line wherein the exhaust-gas turbine has at least two spiral ducts which in each case open into a radial flow inlet passage. Arranged in the radial flow inlet passage is a guide cascade ring which is disposed between two axially delimiting walls. One of the walls is designed to be axially displaceable and adapted to accommodate the vanes of the guide cascade ring. The wall is displaceable axially outward to such an extent that the vanes of the radial guide cascade ring are no longer in contact with the wall and there is a direct, unobstructed flow path to an outflow duct in the exhaust-gas turbine.
摘要翻译：一种在内燃机中的排气涡轮增压器，其具有在所述排气管线中的压缩机和所述排气管线中的废气涡轮机，其中所述排气涡轮机具有至少两个螺旋管道，每个所述螺旋管道在每种情况下都敞开成径向流动入口通道。在径向流入口通道中布置有引导级联环，其布置在两个轴向限定的壁之间。一个壁被设计成可轴向移动并适于容纳引导级联环的叶片。该壁可以轴向向外移动到这样的程度，使得径向引导级联环的叶片不再与壁接触，并且存在与排气涡轮机中的流出管道直接无阻碍的流动路径。

5. 发明授权

US06553762B2 Exhaust gas turbocharger for an internal combustion engine 有权
公开(公告)号：US06553762B2
公开(公告)日：2003-04-29
申请号：US10021686
申请日：2001-12-11
申请人： Paul Löffler , Wolfgang Erdmann , Peter Fledersbacher , Siegfried Sumser , Friedrich Wirbeleit , Jürgen Willand
发明人： Paul Löffler , Wolfgang Erdmann , Peter Fledersbacher , Siegfried Sumser , Friedrich Wirbeleit , Jürgen Willand
IPC分类号： F02B3344
CPC分类号： F01D9/026 , F01D25/26 , F02B37/02 , F02B37/025 , F02C6/12 , Y02T10/144
摘要： In an exhaust gas turbocharger for an internal combustion engine including an exhaust gas turbine and a compressor connected to the turbine so as to be operated thereby, the turbine includes a housing consisting of an inner and an outer shell formed from steel sheets and being arranged in spaced relationship so as to form therebetween an intermediate space.

6. 发明授权

US06332913B1 Membrane module for selective gas separation 失效
标题翻译：选择性气体分离膜组件
公开(公告)号：US06332913B1
公开(公告)日：2001-12-25
申请号：US09471406
申请日：1999-12-23
申请人： Sven Breitschwerdt , Wolfgang Erdmann , Dietmar Heil , Carlo Schmid , Steffen Wieland
发明人： Sven Breitschwerdt , Wolfgang Erdmann , Dietmar Heil , Carlo Schmid , Steffen Wieland
IPC分类号： B01D5912
CPC分类号： B01D53/22 , B01D63/06 , B01D2319/04
摘要： A membrane module for selective gas separation includes one or more separation units stacked one on the other, and at least one of interposed frame plates or stack-end frame plates. Each separation unit includes a support plate with a separation gas receiving structure and at least one corresponding gas separating membrane. The frame plates having a gas mixture flow chamber structure. Each separating unit and the frame plates contain (1) gas-mixture connecting channel structures in a first and a second side area formed by overlapping openings in the plates and extending in a stacking direction, which are in fluid connection with the gas mixture flow chamber structures; and (2) separation gas connection channel structures in a third and fourth side area, which are in fluid connection with the separation gas receiving structure or structures.
摘要翻译：用于选择性气体分离的膜组件包括一个或多个彼此堆叠的分离单元，以及插入的框架板或堆叠端框架板中的至少一个。每个分离单元包括具有分离气体接收结构的支撑板和至少一个对应的气体分离膜。框架板具有气体混合物流动室结构。每个分离单元和框架板包含（1）在第一和第二侧区域中的气体混合连接通道结构，该第一和第二侧面区域由板中的重叠开口形成并在堆叠方向上延伸，该堆叠方向与气体混合物流动室流体连通结构; 和（2）与分离气体接收结构或结构流体连通的第三和第四侧区域中的分离气体连接通道结构。

7. 发明授权

US6126483A Interconnect system for heating conductors in an aircraft 失效
标题翻译：互联系统用于航空器中的导体加热
公开(公告)号：US6126483A
公开(公告)日：2000-10-03
申请号：US103120
申请日：1998-06-23
申请人： Safa Kirma , Heinz Stoever , Joachim Pfeiff , Wolfgang Erdmann
发明人： Safa Kirma , Heinz Stoever , Joachim Pfeiff , Wolfgang Erdmann
IPC分类号： B64D15/12 , H01R13/52 , H01R13/639 , H01R13/40
CPC分类号： B64D15/12 , H01R13/5221 , H01R13/6392 , H01R2107/00
摘要： A system of interconnected heating conductors, suitable for preventing freezing of water lines in an aircraft for example, includes a plurality of heater units (1, 12) electrically coupled together by respective coupling plugs (9, 10). Each heater unit comprises one or more heating conductor bands or cables (2, 21, 22), with a respective socket contact plug (9) connected to one end thereof and a respective pin contact plug (10) connected to the other end thereof. Each plug (9, 10) includes a housing (6) wherein the conductors of the heater band (2) are crimp-connected to electrical connectors (7), which include pin contacts (723) in the case of the pin contact plug (10) and socket contacts (77) in the case of the socket contact plug (9). The housing (6) is completely filled with a sealing compound (19) which is injected through a fill hole in the housing wall. The pin contacts (723) extend outwardly through contact chambers into a female cavity (411) of the plug (10), while the socket contacts (77) extend outwardly through contact chambers in a male plug member (412) of the plug (9). The two plugs may be matingly plugged together, and mechanically secured by locking bails (23) engaging retaining catches (24). This achieves a very effective seal against moisture penetration, and eliminates capillary action even when subjected to vibrations, shock, temperature variations, and low pressure conditions.
摘要翻译：一种互相连接的加热导体的系统，适用于防止例如飞行器中的水线冻结，包括通过相应的联接塞（9,10）电耦合在一起的多个加热器单元（1,2）。每个加热器单元包括一个或多个加热导体带或电缆（2,21,22），其一个相应的插座接触插头（9）连接到其一端，并且相应的针式接触插头（10）连接到另一端。每个插头（9,10）包括壳体（6），其中加热器带（2）的导体被压接连接到电连接器（7），电连接器（7）包括在针式接触插塞（图1）的情况下的销触点（723）在插座接触插头（9）的情况下，插座触头（77）和插座触点（77）。壳体（6）完全充满密封化合物（19），其通过壳体壁中的填充孔注入。销触点（723）通过接触室向外延伸到插头（10）的阴腔（411）中，而插座触头（77）通过插头（9）的插头构件（412）中的接触室向外延伸）。这两个插头可以配合地插在一起，并通过与保持卡扣（24）接合的锁定钉（23）机械地固定。这实现了对湿气渗透的非常有效的密封，并且即使经受振动，冲击，温度变化和低压条件也消除毛细作用。

8. 发明授权

US08221630B2 Process for dewatering a hydraulic fluid 有权
标题翻译：液压油脱水方法
公开(公告)号：US08221630B2
公开(公告)日：2012-07-17
申请号：US12827300
申请日：2010-06-30
申请人： Ingo Scheel , Ralf Pohlmann , Wolfgang Erdmann
发明人： Ingo Scheel , Ralf Pohlmann , Wolfgang Erdmann
IPC分类号： B01J49/00 , C02F1/42
CPC分类号： F15B21/041
摘要： The present invention provides a method and a device for dewatering a hydraulic fluid of a hydraulic system, in particular in the aerospace sector, comprising a container which has a sorbent, a feed which supplies the hydraulic fluid from the hydraulic system to the container for the hydraulic fluid to be passed through the sorbent such that it can be dewatered in a dewatering mode of the device, and a return which returns the dewatered hydraulic fluid from the container to the hydraulic system in the dewatering mode of the device. The hydraulic fluid can be dewatered continuously and very efficiently by the method and the device according to the invention.
摘要翻译：本发明提供了一种用于特别是在航空航天领域中对液压系统的液压流体进行脱水的方法和装置，该方法和装置包括一个容器，该容器具有一个吸附剂，一个将液压流体从液压系统供给到用于液压流体通过吸附剂，使得其可以在该装置的脱水模式中脱水，以及在装置的脱水模式中将脱水的液压流体从容器返回到液压系统的返回装置。可以通过根据本发明的方法和装置连续且非常有效地脱水。

9. 发明授权

US07073334B2 Variable exhaust gas turbocharger 失效
标题翻译：可变废气涡轮增压器
公开(公告)号：US07073334B2
公开(公告)日：2006-07-11
申请号：US10949959
申请日：2004-09-24
申请人： Siegfried Sumser , Peter Fledersbacher , Wolfgang Erdmann , Manfred Stute
发明人： Siegfried Sumser , Peter Fledersbacher , Wolfgang Erdmann , Manfred Stute
IPC分类号： F02D23/00 , F04D29/44 , F04D1/08 , F04D1/10 , F01D1/06
CPC分类号： F04D29/462 , F01D17/165 , F02B29/0406 , F02B37/24 , F02D41/0007 , F02M26/05 , F02M26/10 , F02M26/23 , F04D29/4213 , F05D2250/51 , Y02T10/144
摘要： In a variable exhaust gas turbocharger for an internal combustion engine having an exhaust gas turbine and a compressor with a variable vane structure wherein the exhaust gas turbocharger comprises a housing and a compressor wheel which is connected to an exhaust gas turbine wheel via a shaft, the compressor has a radial inflow flow passage in which a variable vane structure or throttle device is arranged upstream of the compressor wheel and another vane structure is arranged in the radial flow passage downstream of the compressor wheel in the direction of flow.
摘要翻译：在具有废气涡轮机的内燃机的可变废气涡轮增压器和具有可变叶片结构的压缩机中，其中排气涡轮增压器包括壳体和通过轴连接到废气涡轮机叶轮的压缩机叶轮，压缩机具有径向流入流动通道，其中可变叶片结构或节流装置布置在压缩机叶轮的上游，并且另一个叶片结构布置在沿着流动方向的压缩机叶轮下游的径向流动通道中。

10. 发明授权

US06977005B2 Waterless vacuum toilet system for aircraft 失效
标题翻译：无尘真空马桶系统用于飞机
公开(公告)号：US06977005B2
公开(公告)日：2005-12-20
申请号：US10620480
申请日：2003-07-15
申请人： Wolfgang Erdmann , Torsten Gienke , Hans-Juergen Heinrich
发明人： Wolfgang Erdmann , Torsten Gienke , Hans-Juergen Heinrich
IPC分类号： B64D11/02 , E03D11/02 , E03F1/00 , B01D35/16 , E03D5/00
CPC分类号： E03D11/02 , B64D11/02 , E03F1/006 , Y02T50/46
摘要： A waterless vacuum toilet system for an aircraft includes a toilet bowl connected via a suction valve and a waste collection pipe to a waste collection tank. Waste-contacting surfaces that come into contact with urine and fecal waste are coated with an adhesion-inhibiting or adhesion-reducing nanocoating. The adhesion of waste is significantly reduced, and the need for flushing water is completely eliminated. Instead, an air jet arrangement preferably including an annular ring nozzle or annular air gap directs an airflow into the toilet bowl and along the nanocoated waste-contacting surface thereof, to “air flush” the waste material from these surfaces. The flushing airflow may be induced through the air jet arrangement into the toilet bowl by the suction applied through the suction valve. The “air flushed” toilet system substantially reduces the total system weight and eliminates the need for toilet flushing water to be carried in the aircraft.
摘要翻译：用于飞机的无水真空马桶系统包括通过吸入阀连接的马桶和废物收集管连接到废物收集罐。与尿液和粪便废物接触的废物接触表面涂覆有粘附抑制或减粘剂纳米涂层。废物的附着力明显降低，彻底消除了冲洗水的需要。相反，优选地包括环形环喷嘴或环形空气间隙的空气喷射装置将气流引导到马桶中并沿着其与纳米填料的废物接触表面引导从这些表面“废气”冲洗废料。冲洗气流可以通过通过吸入阀施加的抽吸通过空气喷射装置引入马桶中。 “空气冲洗”厕所系统大大减少了总系统重量，并且不需要在飞机上携带的厕所冲洗水。

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