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1. 发明授权

US08111128B2 Multi-structure thermally trimmable resistors 有权
标题翻译：多结构热可微调电阻
公开(公告)号：US08111128B2
公开(公告)日：2012-02-07
申请号：US12524516
申请日：2008-02-06
申请人： Oleg Grudin , Salman Saed , Tommy Tsang , Bowei Zhang , Leslie M. Landsberger , L. Richard Williston
发明人： Oleg Grudin , Salman Saed , Tommy Tsang , Bowei Zhang , Leslie M. Landsberger , L. Richard Williston
IPC分类号： H01C3/04
CPC分类号： H01C17/267 , H01C17/22 , Y10T29/49082 , Y10T29/49099
摘要： A method for arranging a plurality of thermally isolated microstructures over at least one cavity, each of the microstructures housing at least part of a thermally-trimmable resistor, the thermally-trimmable resistor having at least a functional resistor, the method comprising: providing pairs of facing microstructures; grouping together sets of pairs of facing microstructures, each of the sets having at least one pair of facing microstructures; and arranging microstructures within a given set to have each microstructure exposed to heat from a same number of facing, side, and diagonal neighbors of microstructures from a same resistor.
摘要翻译：一种用于在至少一个空腔上布置多个热隔离微结构的方法，每个微结构容纳至少一部分可热可调电阻器，所述热可微调电阻器具有至少一个功能电阻器，所述方法包括：提供成对的面向微结构; 将一组相对的微结构分组在一起，每组具有至少一对面向的微结构; 并且在给定的组中布置微结构以使每个微结构暴露于来自相同电阻器的相同数量的微结构的面向，侧向和对角线相邻的热量。

2. 发明授权

US08105044B2 Compressor turbine blade airfoil profile 有权
标题翻译：压缩机涡轮叶片翼型
公开(公告)号：US08105044B2
公开(公告)日：2012-01-31
申请号：US12766329
申请日：2010-04-23
申请人： Remo Marini , Dan Olaru , Edward Vlasic , Silvio De Santis , Sophia Levy
发明人： Remo Marini , Dan Olaru , Edward Vlasic , Silvio De Santis , Sophia Levy
IPC分类号： B64C27/46
CPC分类号： F01D5/141 , F05D2240/301 , F05D2250/74 , Y10S416/02
摘要： A compressor turbine includes a series of compressor turbine blades each having an airfoil with a profile substantially in accordance with at least an intermediate portion of the Cartesian coordinate values of X, Y and Z set forth in Table 2. The X and Y values are distances, which when smoothly connected by an appropriate continuing curve, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete airfoil shape.
摘要翻译：压缩机涡轮机包括一系列压缩机涡轮叶片，每个叶片具有基本上根据表2所示的X，Y和Z的笛卡尔坐标值的至少中间部分的轮廓的翼型.X和Y值是距离当通过适当的连续曲线平稳地连接时，在每个距离Z处限定翼型轮廓部分。每个距离Z处的轮廓部分彼此平滑地连接以形成完整的翼型形状。

3. 发明授权

US08104260B2 Deswirling exhaust mixer 有权
标题翻译：旋流式排气混合器
公开(公告)号：US08104260B2
公开(公告)日：2012-01-31
申请号：US12470893
申请日：2009-05-22
申请人： Sami Girgis , David F. Glasspoole
发明人： Sami Girgis , David F. Glasspoole
IPC分类号： F02K1/48
CPC分类号： F02K1/386 , F02K1/48 , F05D2250/314
摘要： An exhaust mixer for a gas turbine engine including a plurality of circumferentially distributed alternating inner and outer lobes, where each of the inner lobes is configured with a circumferential offset between the base and the tip thereof, and a direction of the circumferential offset defined from the base to the tip of each of the inner lobes is the same for all of the inner lobes and opposite to that of a swirl component of a main gas path flow entering the exhaust mixer.
摘要翻译：一种用于燃气涡轮发动机的排气混合器，其包括多个周向分布的交替的内和外凸角，其中每个内凸角在基部和其顶端之间构造有周向偏移，并且沿着圆周偏移限定的圆周偏移的方向每个内叶片的顶端的底部对于所有的内叶片是相同的，并且与进入排气混合器的主气体流动流的旋流部件的顶部相反。

4. 发明授权

US08100659B2 HP turbine vane airfoil profile 有权
标题翻译：惠普涡轮叶片翼型
公开(公告)号：US08100659B2
公开(公告)日：2012-01-24
申请号：US12752271
申请日：2010-04-01
申请人： Remo Marini
发明人： Remo Marini
IPC分类号： F01D5/14
CPC分类号： F01D9/02 , F05D2220/3213 , F05D2240/12 , F05D2250/74
摘要： A two-stage high pressure turbine includes a second stage vane having an airfoil with a profile substantially in accordance with at least an intermediate portion of the Cartesian coordinate values of X, Y and Z set forth in Table 2. The X and Y values are distances, which when smoothly connected by an appropriate continuing curve, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete airfoil shape.
摘要翻译：两级高压涡轮机包括具有基本上根据表2所示的X，Y和Z的笛卡尔坐标值的至少中间部分的轮廓的翼型的第二级叶片.X和Y值是当通过适当的连续曲线平稳地连接时，在每个距离Z处限定翼型轮廓部分的距离。每个距离Z处的轮廓部分彼此平滑地连接以形成完整的翼型形状。

5. 发明授权

US08097972B2 Gas turbine with magnetic shaft forming part of a generator/motor assembly 有权
标题翻译：具有形成发电机/电动机组件的一部分的磁轴的燃气轮机
公开(公告)号：US08097972B2
公开(公告)日：2012-01-17
申请号：US12493705
申请日：2009-06-29
申请人： Enzo Macchia
发明人： Enzo Macchia
IPC分类号： F01D15/10 , F02C6/00 , H02K7/18 , H02P9/04 , F03H1/00 , F02K3/02 , F02C9/00
CPC分类号： F01D15/10 , F02C7/32 , F05D2220/768 , Y02T50/671
摘要： A gas turbine engine including a first shaft being one of a main shaft concentrically mounted to at least one turbine rotor and a tower shaft directly driven by the main shaft and extending generally radially therefrom, the first shaft having a reduced diameter portion located within the gas turbine engine, an electrical assembly having a rotor comprising permanent magnets retained on an outer surface of the reduced diameter portion and a stator comprising a magnetic field circuit disposed adjacent an outer periphery of the rotor, and an electrical connection between the magnetic field circuit and at least one of a power source and an electrically drivable accessory.
摘要翻译：一种燃气涡轮发动机，包括第一轴，其是同心地安装到至少一个涡轮转子的主轴和由主轴直接驱动并且大致径向延伸的塔轴，第一轴具有位于气体内的直径减小的部分涡轮发动机，具有保持在所述直径减小部分的外表面上的永磁体的转子的电气组件和定子，所述定子包括邻近所述转子的外周设置的磁场电路，以及所述磁场电路和所述磁场电路之间的电连接至少一个电源和电驱动的附件。

6. 发明授权

US08097376B2 Fuel cell system comprising modular design features 有权
标题翻译：燃料电池系统包括模块化设计特征
公开(公告)号：US08097376B2
公开(公告)日：2012-01-17
申请号：US12903742
申请日：2010-10-13
申请人： Dingrong Bai , Jean-Guy Chouinard , David Elkaim
发明人： Dingrong Bai , Jean-Guy Chouinard , David Elkaim
IPC分类号： H01M8/24 , H01M2/38
CPC分类号： H01M8/0612 , H01M8/0297 , H01M8/04052 , H01M8/04074 , H01M8/0625 , H01M8/247
摘要： There is described a fuel cell power system including a fuel processor subsystem, a fuel cell subsystem, and a power conditioning subsystem. The fuel processor subsystem comprises a main module for producing hydrogen rich streams from a hydrocarbon fuel, a balance of plant module for auxiliary components, and a control and electronic module for monitoring and controlling the fuel processor subsystem. The fuel cell subsystem comprises a main module for generation of electric power and thermal energy from hydrogen rich streams produced by the fuel processor module and air, a balance of plant module for auxiliary components, and a control and electronic module for monitoring and controlling the fuel cell subsystem. Each module has individual components attached thereto, the modules being designed and manufactured separately and assembled together to form the respective subsystems.
摘要翻译：描述了包括燃料处理器子系统，燃料电池子系统和功率调节子系统的燃料电池电力系统。燃料处理器子系统包括用于从烃燃料产生富氢流的主模块，辅助部件的工厂模块的平衡以及用于监测和控制燃料处理器子系统的控制和电子模块。燃料电池子系统包括用于从由燃料处理器模块和空气产生的富氢流产生电力和热能的主模块，辅助部件的工厂模块的平衡以及用于监测和控制燃料的控制和电子模块单元子系统。每个模块具有连接到其上的各个部件，模块被分开设计和制造并组装在一起以形成相应的子系统。

7. 发明授权

US08092145B2 Particle separator and separating method for gas turbine engine 有权
标题翻译：燃气轮机发动机颗粒分离器和分离方法
公开(公告)号：US08092145B2
公开(公告)日：2012-01-10
申请号：US12259602
申请日：2008-10-28
申请人： Alain C. Martel , Eugene Gekht
发明人： Alain C. Martel , Eugene Gekht
IPC分类号： F04D27/00 , F04D29/44
CPC分类号： F02C7/052 , F02C6/08 , F04D29/4206 , F04D29/4213 , F05D2260/607 , Y02T50/675
摘要： A system and method for particle separation in a gas turbine engine centrifugal impeller bleed air system using a tangential velocity component of the compressor bleed air to centrifuge the particles radially outwardly and convey the particles circumferentially, away from a clean air outlet and towards a particle outlet where the particles are extracted from the bleed air.
摘要翻译：在燃气轮机发动机离心式叶轮放气系统中使用压缩机排气的切向速度分量径向向外离心颗粒的系统和方法，其周向地输送颗粒，远离清洁空气出口并朝向颗粒出口其中颗粒从放气中提取。

8. 发明授权

US08083940B2 Oil strainer for a gas turbine engine 有权
标题翻译：燃气轮机的过滤器
公开(公告)号：US08083940B2
公开(公告)日：2011-12-27
申请号：US11466162
申请日：2006-08-22
申请人： Eric Durocher , Guy Lefebvre
发明人： Eric Durocher , Guy Lefebvre
IPC分类号： B01D29/085 , B01D29/17 , B01D29/37
CPC分类号： B01D35/02 , B01D2201/02
摘要： The oil strainer has a filtering portion and a flexible sleeve portion to which the filtering portion is connected. The flexible sleeve portion has a plurality of spigot-receiving slots on the upstream side of the strainer.
摘要翻译：滤油器具有过滤部分和过滤部分连接到的柔性套管部分。柔性套筒部分在过滤器的上游侧具有多个插口接收槽。

9. 发明授权

US08074452B2 Nested channel ducts for nozzle construction and the like 有权
标题翻译：用于喷嘴结构的嵌套通道导管等
公开(公告)号：US08074452B2
公开(公告)日：2011-12-13
申请号：US12124593
申请日：2008-05-21
申请人： Lev Alexander Prociw , Harris Shafique , John Sokalski , Claude Raymond Pelletier
发明人： Lev Alexander Prociw , Harris Shafique , John Sokalski , Claude Raymond Pelletier
IPC分类号： F02C7/22 , F23R3/00
CPC分类号： F23K5/06 , F02C7/222 , F23R3/283
摘要： A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel, adapted for conveying fuel flow, is formed in a surface of a gas turbine engine component. The channel includes at least a first discrete conduit and a second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.
摘要翻译：一种用于燃气涡轮发动机的多管道系统，多管道系统在多个管道入口和出口之间延伸。在燃气涡轮发动机部件的表面形成有用于输送燃料流的通道。通道包括至少第一离散导管和第二离散导管。第一和第二离散导管各自适于将独立的流体流从相应的入口引导到相应的出口。

10. 发明授权

US08065396B2 Message send queue reordering based on priority 有权
标题翻译：消息发送队列根据优先级重新排序
公开(公告)号：US08065396B2
公开(公告)日：2011-11-22
申请号：US12686001
申请日：2010-01-12
申请人： David Tapuska , Michael Knowles
发明人： David Tapuska , Michael Knowles
IPC分类号： G06F15/16 , G06F15/173
CPC分类号： H04L51/26 , H04L51/38 , H04L67/32 , H04L67/327
摘要： A method and system for communicating serialized data provides a mechanism for ordering the data in response to a priority. In an embodiment, a server sending the data uses the priority to order the data in a message send queue for sending the data to a requesting device. The server may comprise a gateway and the second device a wireless device communicating with the gateway. The wireless device may send a priority indication in association with a request for the data to facilitate the ordering.
摘要翻译：用于传送串行化数据的方法和系统提供了一种响应于优先级排序数据的机制。在一个实施例中，发送数据的服务器使用优先级来排序消息发送队列中的数据，以将数据发送到请求设备。服务器可以包括网关，第二设备包括与网关通信的无线设备。无线设备可以与数据的请求相关联地发送优先级指示以便于排序。

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