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1. 发明申请

US20140001901A1 ELECTRIC MOTOR WITH A REDUNDANT SEAL ARRANGEMENT 审中-公开
标题翻译：具有冗余密封装置的电动马达
公开(公告)号：US20140001901A1
公开(公告)日：2014-01-02
申请号：US13535941
申请日：2012-06-28
申请人： Adam M. Finney , Roy D. Rasmussen , Aaron M. Finke
发明人： Adam M. Finney , Roy D. Rasmussen , Aaron M. Finke
IPC分类号： H02K5/12 , H02K15/00
CPC分类号： H02K5/128 , Y10T29/49009
摘要： An electric motor has a primary and a secondary seal isolating a rotor cavity from a stator cavity.
摘要翻译：电动机具有将转子腔与定子腔隔离的初级和次级密封。

2. 发明申请

US20130313067A1 INTEGRATED TORQUE LIMITER/NO-BACK DEVICE 有权
标题翻译：集成扭矩限制/无返回装置
公开(公告)号：US20130313067A1
公开(公告)日：2013-11-28
申请号：US13478172
申请日：2012-05-23
申请人： Adam M. Finney
发明人： Adam M. Finney
IPC分类号： F16D43/20
CPC分类号： F16D67/02 , B64C13/24 , B64C13/28 , B64D2045/001 , F16D7/005 , F16D43/215 , F16D43/218 , F16D55/02 , F16D55/16 , F16D55/48 , F16D2125/38 , F16H35/10 , Y02T50/44
摘要： An integrated torque limiter/no-back device for use in an actuator with an input shaft, an output and gear reduction. The device includes an input ramp to receive torque from the input shaft; a combined ramp to transfer torque; an output ramp to transfer torque to the gear reduction; one or more balls between the input ramp and the combined ramp and between the combined ramp and the output ramp to transfer torque; and a brake for causing torque to be grounded and for preventing backdriving of the input shaft by preventing movement of one or more of the input ramp, the combined ramp and the output ramp when a torque threshold has been met. The input ramp and the output ramp are a no-back ramp and a torque limiter ramp, respectively, and the device also includes a pin between the combined ramp and one or more of the no-back ramp and the gear reduction for transferring torque.
摘要翻译：用于具有输入轴，输出和齿轮减速的致动器的集成扭矩限制器/无背装置。该装置包括从输入轴接收扭矩的输入斜坡; 组合斜坡传递扭矩; 输出斜坡以将扭矩传递到齿轮减速; 在输入斜坡和组合斜坡之间以及组合斜坡和输出斜坡之间的一个或多个球以传递扭矩; 以及用于使扭矩接地的制动器，并且当已经满足扭矩阈值时，通过防止输入斜坡，组合斜坡和输出斜坡中的一个或多个的移动来防止输入轴的反向驱动。输入斜坡和输出斜坡分别是无背斜面和扭矩限制器斜坡，并且该装置还包括在组合斜坡和一个或多个无反转斜坡之间的销和用于传递转矩的齿轮减速。

3. 发明申请

US20130076035A1 MOTOR-GENERATOR TURBOMACHINE STARTER 审中-公开
标题翻译：电机发动机涡轮发动机
公开(公告)号：US20130076035A1
公开(公告)日：2013-03-28
申请号：US13246827
申请日：2011-09-27
申请人： Andreas C. Koenig , Adam M. Finney
发明人： Andreas C. Koenig , Adam M. Finney
IPC分类号： F02N11/08
CPC分类号： F02C7/275 , F02C7/32 , F02C7/36 , F05D2220/768 , F05D2260/4031
摘要： An exemplary turbomachine starter assembly includes a motor-generator that selectively operates in a motor mode or a generator mode. The motor-generator provides a rotational input to a turbomachine when operating in the motor mode. The motor-generator generates a supply of electrical power when operating in the generator mode. The supply of electrical power is used to power accessories of the turbomachine.
摘要翻译：示例性的涡轮机起动器组件包括电动发电机，其选择性地以电动机模式或发电机模式操作。当在电机模式下运行时，电动发电机为涡轮机提供旋转输入。当在发电机模式下工作时，电动发电机产生电力供应。供电电源用于为涡轮机的附件提供动力。

4. 发明申请

US20120036866A1 AUXILIARY POWER UNIT WITH MULTIPLE FUEL SOURCES 审中-公开
标题翻译：具有多个燃料源的辅助动力单元
公开(公告)号：US20120036866A1
公开(公告)日：2012-02-16
申请号：US12854230
申请日：2010-08-11
申请人： Adam M. Finney
发明人： Adam M. Finney
IPC分类号： F02C6/00 , F17D1/00 , G05D11/00
CPC分类号： F02C9/263 , F05D2220/50 , F05D2240/40 , Y10T137/0324 , Y10T137/2514
摘要： A system and method are disclosed for supplying fuel to an auxiliary power unit of an aircraft. The system includes a primary fuel source, a secondary fuel source, and a secondary valve. The primary fuel source is in fluid communication with the auxiliary power unit to provide a primary fuel thereto. Similarly, the secondary fuel source is in fluid communication with the auxiliary power unit to provide a secondary fuel thereto. The secondary valve regulates flow of the secondary fuel from the secondary fuel source to the auxiliary power unit. The method provides a secondary fuel from a secondary fuel source to the auxiliary power unit if an emergency operating condition experienced by the aircraft results from either exhaustion or contamination of a primary fuel.
摘要翻译：公开了用于向飞行器的辅助动力单元供应燃料的系统和方法。该系统包括主燃料源，二次燃料源和二次阀。主燃料源与辅助动力单元流体连通以向其提供主要燃料。类似地，二次燃料源与辅助动力单元流体连通以向其提供二次燃料。次级阀调节辅助燃料从辅助燃料源到辅助动力单元的流量。如果飞机经历的紧急操作条件是由于一次燃料的消耗或污染造成的，则该方法提供从次级燃料源到辅助动力单元的二次燃料。

5. 发明授权

US09255632B2 Integrated torque limiter/no-back device 有权
标题翻译：集成扭矩限制器/无背装置
公开(公告)号：US09255632B2
公开(公告)日：2016-02-09
申请号：US13478172
申请日：2012-05-23
申请人： Adam M. Finney
发明人： Adam M. Finney
IPC分类号： F16H35/10 , B64D31/06 , F16D43/21 , F16D55/48 , F16D55/16 , F16D125/38 , B64D45/00
CPC分类号： F16D67/02 , B64C13/24 , B64C13/28 , B64D2045/001 , F16D7/005 , F16D43/215 , F16D43/218 , F16D55/02 , F16D55/16 , F16D55/48 , F16D2125/38 , F16H35/10 , Y02T50/44
摘要： An integrated torque limiter/no-back device for use in an actuator with an input shaft, an output and gear reduction. The device includes an input ramp to receive torque from the input shaft; a combined ramp to transfer torque; an output ramp to transfer torque to the gear reduction; one or more balls between the input ramp and the combined ramp and between the combined ramp and the output ramp to transfer torque; and a brake for causing torque to be grounded and for preventing backdriving of the input shaft by preventing movement of one or more of the input ramp, the combined ramp and the output ramp when a torque threshold has been met. The input ramp and the output ramp are a no-back ramp and a torque limiter ramp, respectively, and the device also includes a pin between the combined ramp and one or more of the no-back ramp and the gear reduction for transferring torque.
摘要翻译：用于具有输入轴，输出和齿轮减速的致动器的集成扭矩限制器/无背装置。该装置包括从输入轴接收扭矩的输入斜坡; 组合斜坡传递扭矩; 输出斜坡以将扭矩传递到齿轮减速; 在输入斜坡和组合斜坡之间以及组合斜坡和输出斜坡之间的一个或多个球以传递扭矩; 以及用于使扭矩接地的制动器，并且当已经满足扭矩阈值时，通过防止输入斜坡，组合斜坡和输出斜坡中的一个或多个的移动来防止输入轴的反向驱动。输入斜坡和输出斜坡分别是无背斜面和扭矩限制器斜坡，并且该装置还包括在组合斜坡和一个或多个无反转斜坡之间的销和用于传递转矩的齿轮减速。

6. 发明申请

US20130031912A1 GAS TURBINE START ARCHITECTURE 审中-公开
标题翻译：燃气涡轮起动架构
公开(公告)号：US20130031912A1
公开(公告)日：2013-02-07
申请号：US13195223
申请日：2011-08-01
申请人： Adam M. Finney , Michael Krenz
发明人： Adam M. Finney , Michael Krenz
IPC分类号： F02C7/268
CPC分类号： F01D19/00 , F01D15/10 , F02C7/277 , Y02T50/671
摘要： A gas turbine starting architecture is used to start a gas turbine engine having at least a first spool. The architecture includes an electric power distribution bus, a motor, a compressor, a pneumatic distribution circuit, an air turbine starter, and a first tower shaft. The motor converts electric power provided by the electric power distribution bus to mechanical power. In turn, the mechanical power provided by the motor is converted to pneumatic power by the compressor for provision to a pneumatic distribution circuit. The air turbine starter converts pneumatic power from the pneumatic distribution circuit to mechanical power is provided via the first tower shaft to the at least one spool on the gas turbine engine.
摘要翻译：燃气轮机起动架构用于起动具有至少第一阀芯的燃气涡轮发动机。该结构包括配电总线，电动机，压缩机，气动分配回路，空气涡轮起动器和第一塔架轴。电动机将由配电总线提供的电力转换为机械动力。反过来，由电动机提供的机械动力由压缩机转换为气动动力，以供给气动分配回路。空气涡轮起动器将来自气动分配回路的气动动力转换成机械动力，经由第一塔轴提供至燃气涡轮发动机上的至少一个线轴。

7. 发明授权

US08327651B2 Transcritical fluid cooling for aerospace applications 有权
标题翻译：航空应用的跨临界流体冷却
公开(公告)号：US08327651B2
公开(公告)日：2012-12-11
申请号：US12498744
申请日：2009-07-07
申请人： Adam M. Finney , Young K. Park , Scott F. Kaslusky , Daniel R. Sabatino
发明人： Adam M. Finney , Young K. Park , Scott F. Kaslusky , Daniel R. Sabatino
IPC分类号： F25B9/00
CPC分类号： B64D13/08 , B64D2013/0614 , B64D2013/0674 , F25B1/10 , F25B9/008 , F25B9/06 , F25B2309/061 , F25B2400/13 , F25B2400/23 , Y02T50/44 , Y02T50/56
摘要： A cooling system includes a compressor for compressing a refrigerant from a subcritical state to a supercritical state, a cooler for transferring heat from the refrigerant, an expander for expanding the refrigerant in the supercritical state, an expansion valve for expanding the refrigerant from the supercritical state to the subcritical state and an evaporator for transferring heat from a cooling fluid to the refrigerant in the subcritical state. Work extracted by the expander provides power to the compressor. A method for cooling a vehicle includes compressing a refrigerant from a subcritical state to a supercritical state, cooling the refrigerant, expanding the refrigerant in the supercritical state where work produced by expanding the refrigerant is used to compress the refrigerant, expanding the refrigerant from the supercritical state to the subcritical state, cooling a cooling fluid with the refrigerant in the subcritical state and cooling vehicle components with the cooling fluid.
摘要翻译：冷却系统包括用于将制冷剂从亚临界状态压缩至超临界状态的压缩机，用于从制冷剂传递热的冷却器，用于使处于超临界状态的制冷剂膨胀的膨胀机，用于使制冷剂从超临界状态膨胀的膨胀阀到亚临界状态的蒸发器和用于将热量从冷却流体传递到亚临界状态的制冷剂的蒸发器。膨胀机提取的作业为压缩机提供动力。一种用于冷却车辆的方法包括将制冷剂从亚临界状态压缩至超临界状态，冷却制冷剂，使超临界状态下的制冷剂膨胀，使用膨胀制冷剂制造的工件用于压缩制冷剂，从超临界状态到亚临界状态，用亚临界状态的制冷剂冷却冷却流体，并用冷却流体冷却车辆部件。

8. 发明申请

US20120221157A1 LOW PRESSURE SPOOL EMERGENCY GENERATOR 审中-公开
标题翻译：低压SPOOL应急发电机
公开(公告)号：US20120221157A1
公开(公告)日：2012-08-30
申请号：US13036994
申请日：2011-02-28
申请人： Adam M. Finney , Michael Krenz , Carl A. Wagner , David L. Jacques
发明人： Adam M. Finney , Michael Krenz , Carl A. Wagner , David L. Jacques
IPC分类号： B60L1/00 , G06F1/26
CPC分类号： G06F1/26 , B64D41/00 , B64D2221/00 , F01D15/10 , F02C7/32 , F05D2270/09 , Y02T50/53
摘要： An emergency power system is useable on an aircraft having a gas turbine engine with a low pressure spool and a high pressure spool. The emergency power system includes an emergency electrical generator coupled to the low pressure spool during an emergency for generating emergency electrical power and one or more additional electrical power sources. A plurality of electrical loads are electrically connected to the emergency electrical generator and the one or more additional electrical power sources. Aircraft sensors provide data regarding emergency electrical power availability and emergency electrical power demand. A controller for controlling the emergency electrical generator determines emergency electrical power demand and emergency electrical power availability based upon data from the aircraft sensors. The controller controls the emergency electrical generator based upon the emergency electrical power demand and the emergency electrical power availability.
摘要翻译：应急电力系统可用于具有带有低压阀芯和高压阀芯的燃气涡轮发动机的飞机上。应急电力系统包括在紧急情况期间联接到低压阀芯的紧急发电机，用于产生紧急电力和一个或多个附加电力源。多个电负载电连接到紧急发电机和一个或多个附加电源。飞机传感器提供有关应急电力可用性和应急电力需求的数据。用于控制紧急发电机的控制器基于来自飞行器传感器的数据来确定应急电力需求和应急电力可用性。控制器根据紧急电力需求和应急电力可用性控制应急发电机。

9. 发明申请

US20130278369A1 SEALED INDUCTOR CONNECTION USING LITZ WIRE 有权
标题翻译：使用LITZ线的密封电感器连接
公开(公告)号：US20130278369A1
公开(公告)日：2013-10-24
申请号：US13449686
申请日：2012-04-18
申请人： Charles Shepard , Kris H. Campbell , Adam M. Finney , Robert Scott Downing
发明人： Charles Shepard , Kris H. Campbell , Adam M. Finney , Robert Scott Downing
IPC分类号： H01F27/10 , H01F27/04
CPC分类号： H01F5/04 , H01F27/025 , H01F27/04 , H01F27/2895 , H01F27/325
摘要： An inductor comprises a ferromagnetic core, a litz wire conductor encircling the ferromagnetic core, a housing, a bobbin, a conductive pin, and a seal assembly. The housing encloses the ferromagnetic core and the litz wire conductor. The conductive pin is conductively attached to the litz wire conductor, and extends therefrom to form an external electrical contact. The bobbin supports the litz wire conductor and positions the conductive pin in alignment with an aperture in the housing which is sealed against fluid egress by the seal assembly.
摘要翻译：电感器包括铁磁芯，围绕铁磁芯的绞合线导体，壳体，线轴，导电针和密封组件。外壳包围铁磁芯和绞合线导体。导电针导电地连接到绞合线导体，并从其延伸以形成外部电接触。线轴支撑绞合线导体，并将导电针定位成与壳体中的孔对准，密封件防止由密封组件流出的流体。

10. 发明申请

US20120192578A1 GAS TURBINE BLEED ECS COOLING 审中-公开
标题翻译：气体涡轮机冷却ECS冷却
公开(公告)号：US20120192578A1
公开(公告)日：2012-08-02
申请号：US13015109
申请日：2011-01-27
申请人： Adam M. Finney
发明人： Adam M. Finney
IPC分类号： F25B9/06
CPC分类号： B64D13/06 , B64D2013/0618 , Y02T50/56
摘要： A method for managing heat in an airplane includes extracting hot bleed air from a gas turbine engine, and cooling the hot bleed air in a first heat exchanger thereby forming warm bleed air. The method further includes expanding the warm bleed air with a turbine thereby forming cool bleed air, and using the cool bleed air as a heat sink in a second heat exchanger associated with an environmental control system and thereby forming used bleed air.
摘要翻译：一种用于管理飞机中的热量的方法包括从燃气涡轮发动机中提取热排出空气，并且在第一热交换器中冷却热排出空气，从而形成温暖的放气。该方法还包括用涡轮扩张温暖的放气，从而形成凉爽的排气，并且在与环境控制系统相关联的第二热交换器中使用冷排气作为散热器，从而形成用过的放气。

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