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1. 发明授权

US08745990B2 Gas turbine engine with integrated electric starter/generator 有权
标题翻译：带集成电动起动器/发电机的燃气轮机
公开(公告)号：US08745990B2
公开(公告)日：2014-06-10
申请号：US12694786
申请日：2010-01-27
申请人： Philip Burkholder , Rigoberto J. Rodriguez , Steven Gagne , Kenneth M. Pesyna
发明人： Philip Burkholder , Rigoberto J. Rodriguez , Steven Gagne , Kenneth M. Pesyna
IPC分类号： F02N11/04
CPC分类号： F01D9/065 , F01D15/10 , F02C7/275 , F02C7/32 , F04D25/04 , F04D25/0606 , F16L9/003 , Y02T50/671
摘要： An electrical machine is embedded into the compressor assembly of a gas turbine engine. An electrical system interface module distributes electrical current to and from the embedded electrical machine for starting the gas turbine engine and for operating accessory components. Accordingly, the gas turbine engine and accessory components can be started and operated without a power-takeoff shaftline and without an external accessory gearbox.
摘要翻译：电机被嵌入到燃气轮机的压缩机组件中。电气系统接口模块将电流分配给嵌入式电机，以启动燃气涡轮发动机和操作附件部件。因此，燃气涡轮发动机和辅助部件可以在没有动力输出轴线和没有外部附件齿轮箱的情况下启动和操作。

2. 发明申请

US20110018273A1 STARTER/GENERATOR INTEGRATED INTO COMPRESSOR OF TURBINE ENGINE 审中-公开
标题翻译：集成到涡轮发动机压缩机的起动机/发电机
公开(公告)号：US20110018273A1
公开(公告)日：2011-01-27
申请号：US12509887
申请日：2009-07-27
申请人： Philip Burkholder , Rigoberto J. Rodriguez , Steven Gagne , Kenneth M. Pesyna
发明人： Philip Burkholder , Rigoberto J. Rodriguez , Steven Gagne , Kenneth M. Pesyna
IPC分类号： H02K7/18 , F02C6/04
CPC分类号： F02C7/275 , F01D9/065 , F01D15/10 , F02C7/32 , F04D19/02 , F04D25/0606
摘要： A turbine engine compressor has a rotor including rotating compressor discs. Magnets are positioned on the rotating compressor discs. Electrical coils are positioned in a stationary guide vane internal ring so as to create an electric machine providing starting torque to a rotor, and/or generating electrical energy once the rotor is rotating.
摘要翻译：涡轮发动机压缩机具有包括旋转压缩机盘的转子。磁铁位于旋转的压缩机盘上。电线圈定位在固定的导向叶片内环中，以便在转子旋转时产生向转子提供启动扭矩的电机和/或产生电能。

3. 发明授权

US09534537B2 Phase change material cooling system for a vehicle 有权
标题翻译：车辆相变材料冷却系统
公开(公告)号：US09534537B2
公开(公告)日：2017-01-03
申请号：US13432590
申请日：2012-03-28
申请人： Steven Gagne , Rigoberto J. Rodriguez , William L. Siegel , John R. Arvin
发明人： Steven Gagne , Rigoberto J. Rodriguez , William L. Siegel , John R. Arvin
IPC分类号： F02C6/08 , F02C7/12 , F02C7/32 , F02C6/20 , F41H13/00 , F01D15/10
CPC分类号： F02C7/141 , F01D15/08 , F01D15/10 , F02C3/04 , F02C6/08 , F02C6/20 , F02C7/12 , F02C7/16 , F02C7/32 , F05D2220/323 , F05D2220/50 , F05D2220/76 , F05D2240/35 , F05D2260/207 , F25B23/00 , F25B2400/24 , F41H13/005 , F41H13/0068 , H02K7/1823 , Y02T50/675
摘要： A system is disclosed one form of which is an aircraft that includes a pod capable of housing a work providing device. The pod can also include a thermal conditioning system and a power generation device that can be powered from the work providing device. The pod can provide thermal conditioning services and power services to a payload aboard the aircraft. In one non-limiting form the payload is a directed energy member that can be cooled using the thermal conditioning system and powered using the power generation device.
摘要翻译：公开了一种系统，其一种形式是包括能够容纳工作提供装置的荚的飞机。吊舱还可以包括热调节系统和可以从工作提供装置供电的发电装置。荚可以为飞机上的有效载荷提供热调节服务和电力服务。在一个非限制性形式中，有效载荷是能够使用热调节系统进行冷却并使用发电装置供电的定向能量构件。

4. 发明申请

US20110025157A1 SYSTEM OF ELECTRICAL GENERATION FOR COUNTER-ROTATING OPEN-ROTOR BLADE DEVICE 审中-公开
标题翻译：逆向旋转叶片装置的电机系统
公开(公告)号：US20110025157A1
公开(公告)日：2011-02-03
申请号：US12510334
申请日：2009-07-28
申请人： Mark J. Blackwelder , John Timothy Alt , Steven Gagne , Daniel Kent Vetters
发明人： Mark J. Blackwelder , John Timothy Alt , Steven Gagne , Daniel Kent Vetters
IPC分类号： H02K23/60
CPC分类号： H02K16/005 , H02K7/1807
摘要： A counter-rotating open-rotor blade aircraft propulsion system includes a structure supporting a plurality of blades. A rotor is drivingly coupled to the structure supporting the plurality of blades. The rotor includes a rotating coil disposed in the structure supporting the plurality of blades. A rotating magnetic field source includes two Halbach permanent magnet arrays.
摘要翻译：反向旋转的开式叶片飞机推进系统包括支撑多个叶片的结构。转子驱动地联接到支撑多个叶片的结构。转子包括设置在支撑多个叶片的结构中的旋转线圈。旋转磁场源包括两个Halbach永磁体阵列。

5. 发明授权

US08967531B2 Aircraft and airborne electrical power and thermal management system 有权
标题翻译：飞机和机载电力和热力管理系统
公开(公告)号：US08967531B2
公开(公告)日：2015-03-03
申请号：US13432842
申请日：2012-03-28
申请人： Steven Gagne , Rigoberto Rodriguez , William L. Siegel , John R. Arvin
发明人： Steven Gagne , Rigoberto Rodriguez , William L. Siegel , John R. Arvin
IPC分类号： B64D41/00 , B64D13/00 , B64D13/08 , F02C7/32 , B64D13/06
CPC分类号： B64D13/006 , B64D13/08 , B64D33/04 , B64D33/08 , B64D41/00 , B64D41/007 , B64D2013/0614 , B64D2013/0674 , F02C6/08 , F02C7/32 , H02K7/1823
摘要： A unique airborne electrical power and thermal management system and a unique aircraft having a unique airborne electrical power and thermal management system are provided. The electrical power and thermal management system includes a turbine, which may power loads, for example but not limited to, a generator and a refrigerant compressor. The turbine may be in fluid communication with a gas turbine engine bleed air source to extract power from bleed air for powering the loads. A combustor may be fluidly disposed between the bleed air source and the turbine. The turbine may be part of a gas turbine engine distinct from a propulsion gas turbine engine. In one aspect, at least a portion of the electrical power and thermal management system may be disposed within an aircraft external pod. The pod may be configured to appear similar to a conventional external fuel tank pod employed by the aircraft.
摘要翻译：提供独特的机载电力和热管理系统和独特的飞机，具有独特的机载电力和热管理系统。电力和热管理系统包括涡轮机，其可以为例如但不限于发电机和制冷剂压缩机的负载供电。涡轮机可以与燃气涡轮发动机排气源流体连通，以从放气中提取动力以为负载供电。燃烧器可以流体地设置在排放空气源和涡轮机之间。涡轮机可以是不同于推进燃气涡轮发动机的燃气涡轮发动机的一部分。在一个方面，电力和热管理系统的至少一部分可以设置在飞行器外部舱内。荚可以被配置为看起来类似于飞机使用的常规外部燃料箱舱。

6. 发明申请

US20120256045A1 AIRBORNE COOLING SYSTEM 有权
标题翻译： AIRBORNE冷却系统
公开(公告)号：US20120256045A1
公开(公告)日：2012-10-11
申请号：US13432482
申请日：2012-03-28
申请人： Steven Gagne
发明人： Steven Gagne
IPC分类号： B64D33/10 , B64D1/12
CPC分类号： B64D1/08 , B64D13/00 , B64D33/10 , B64D2013/0614 , B64D2013/0674 , F28D5/00 , F28D2021/0021 , F41H13/0043 , F42B15/34
摘要： An aircraft having a cooling system is disclosed. The cooling system can be used to cool a heat emitting component. In one form the cooling system is a refrigerant system and includes a relatively high temperature device such as, but not limited to, a condenser. The relatively high temperature component is placed in thermal communication with a passing air flow. In one embodiment the aircraft includes a pod in which at least a portion of the cooling system is disposed. For example, a condenser of a vapor cycle refrigerant system can be located in the pod and in thermal communication with the air flow. The cooling system can also include a device capable of delivering a cooling fluid into the air flow and/or to the relatively high temperature component. The cooling fluid can be evaporated to provided additional cooling.
摘要翻译：公开了一种具有冷却系统的飞机。冷却系统可用于冷却发热部件。在一种形式中，冷却系统是制冷剂系统，并且包括相对高温的装置，例如但不限于冷凝器。相对较高的温度部件被放置成与通过的空气流热连通。在一个实施例中，飞行器包括其中布置有冷却系统的至少一部分的舱。例如，蒸气循环制冷剂系统的冷凝器可以位于容器中并与气流热连通。冷却系统还可以包括能够将冷却流体输送到空气流和/或相对高温部件的装置。冷却液可以被蒸发以提供额外的冷却。

7. 发明授权

US08973868B2 Airborne cooling system 有权
标题翻译：机载冷却系统
公开(公告)号：US08973868B2
公开(公告)日：2015-03-10
申请号：US13432482
申请日：2012-03-28
申请人： Steven Gagne
发明人： Steven Gagne
IPC分类号： B64D33/10 , B64D1/08 , F42B15/34 , B64D13/06
CPC分类号： B64D1/08 , B64D13/00 , B64D33/10 , B64D2013/0614 , B64D2013/0674 , F28D5/00 , F28D2021/0021 , F41H13/0043 , F42B15/34
摘要： An aircraft having a cooling system is disclosed. The cooling system can be used to cool a heat emitting component. In one form the cooling system is a refrigerant system and includes a relatively high temperature device such as, but not limited to, a condenser. The relatively high temperature component is placed in thermal communication with a passing air flow. In one embodiment the aircraft includes a pod in which at least a portion of the cooling system is disposed. For example, a condenser of a vapor cycle refrigerant system can be located in the pod and in thermal communication with the air flow. The cooling system can also include a device capable of delivering a cooling fluid into the air flow and/or to the relatively high temperature component. The cooling fluid can be evaporated to provided additional cooling.
摘要翻译：公开了一种具有冷却系统的飞机。冷却系统可用于冷却发热部件。在一种形式中，冷却系统是制冷剂系统，并且包括相对高温的装置，例如但不限于冷凝器。相对较高的温度部件被放置成与通过的空气流热连通。在一个实施例中，飞行器包括其中布置有冷却系统的至少一部分的舱。例如，蒸气循环制冷剂系统的冷凝器可以位于容器中并与气流热连通。冷却系统还可以包括能够将冷却流体输送到空气流和/或相对高温部件的装置。冷却液可以被蒸发以提供额外的冷却。

8. 发明授权

US08826675B2 Thermal system having electrical device 有权
标题翻译：具有电气装置的热系统
公开(公告)号：US08826675B2
公开(公告)日：2014-09-09
申请号：US13451663
申请日：2012-04-20
申请人： Rigoberto Rodriguez , Steven Gagne , Donald W. Burns
发明人： Rigoberto Rodriguez , Steven Gagne , Donald W. Burns
IPC分类号： F25D25/00 , H02K9/12 , H02K9/14
CPC分类号： H02K9/12 , F25B31/006 , H02K9/14
摘要： A thermal system is disclosed in thermal communication with an electrical device. In one form the thermal system is a refrigeration system. The electrical device can be disposed within the refrigeration system such that a working fluid of the refrigeration system exchanges heat with the electrical device. In one embodiment the refrigeration system includes a container in which the electrical device is disposed. The electrical device can be an electrical motor, but other forms are contemplated. The container can be located anywhere in the thermal system. In one non-limiting embodiment the working fluid of the refrigeration system wets a stator of the motor. A partition can be used to separate the stator from the motor to keep the motor free from working fluid.
摘要翻译：公开了一种与电气设备热连接的热系统。在一种形式中，热系统是制冷系统。电气设备可以设置在制冷系统内，使得制冷系统的工作流体与电气设备交换热量。在一个实施例中，制冷系统包括其中设置电气装置的容器。电气设备可以是电动机，但是可以考虑其它形式。容器可以位于热系统的任何地方。在一个非限制性实施例中，制冷系统的工作流体润湿电动机的定子。可以使用隔板将定子与电动机分离，以保持电动机不受工作流体的影响。

9. 发明申请

US20120266613A1 THERMAL SYSTEM HAVING ELECTRICAL DEVICE 有权
标题翻译：具有电气设备的热系统
公开(公告)号：US20120266613A1
公开(公告)日：2012-10-25
申请号：US13451663
申请日：2012-04-20
申请人： Rigoberto Rodriguez , Steven Gagne , Donald W. Burns
发明人： Rigoberto Rodriguez , Steven Gagne , Donald W. Burns
IPC分类号： F25D31/00 , H02K9/00
CPC分类号： H02K9/12 , F25B31/006 , H02K9/14
摘要： A thermal system is disclosed in thermal communication with an electrical device. In one form the thermal system is a refrigeration system. The electrical device can be disposed within the refrigeration system such that a working fluid of the refrigeration system exchanges heat with the electrical device. In one embodiment the refrigeration system includes a container in which the electrical device is disposed. The electrical device can be an electrical motor, but other forms are contemplated. The container can be located anywhere in the thermal system. In one non-limiting embodiment the working fluid of the refrigeration system wets a stator of the motor. A partition can be used to separate the stator from the motor to keep the motor free from working fluid.
摘要翻译：公开了一种与电气设备热连接的热系统。在一种形式中，热系统是制冷系统。电气设备可以设置在制冷系统内，使得制冷系统的工作流体与电气设备交换热量。在一个实施例中，制冷系统包括其中设置电气装置的容器。电气设备可以是电动机，但是可以考虑其它形式。容器可以位于热系统的任何地方。在一个非限制性实施例中，制冷系统的工作流体润湿电动机的定子。可以使用隔板将定子与电动机分离，以保持电动机不受工作流体的影响。

10. 发明申请

US20120248242A1 AIRCRAFT AND AIRBORNE ELECTRICAL POWER AND THERMAL MANAGEMENT SYSTEM 有权
标题翻译：飞机和AIRBORNE电力和热管理系统
公开(公告)号：US20120248242A1
公开(公告)日：2012-10-04
申请号：US13432842
申请日：2012-03-28
申请人： Steven Gagne , Rigoberto Rodriguez , William L. Siegel , John R. Arvin
发明人： Steven Gagne , Rigoberto Rodriguez , William L. Siegel , John R. Arvin
IPC分类号： B64D41/00
CPC分类号： B64D13/006 , B64D13/08 , B64D33/04 , B64D33/08 , B64D41/00 , B64D41/007 , B64D2013/0614 , B64D2013/0674 , F02C6/08 , F02C7/32 , H02K7/1823
摘要： One embodiment of the present invention is a unique airborne electrical power and thermal management system. Another embodiment is a unique aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and electrical power and thermal management systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译：本发明的一个实施例是独特的机载电力和热管理系统。另一个实施例是独特的飞机。其他实施例包括用于飞机和电力和热管理系统的装置，系统，装置，硬件，方法和组合。本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。

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