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1. 发明申请

US20120266612A1 THERMAL SYSTEM HAVING ELECTRICAL DEVICE 审中-公开
标题翻译：具有电气设备的热系统
公开(公告)号：US20120266612A1
公开(公告)日：2012-10-25
申请号：US13451643
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 , H05K7/20 , H02K9/00
CPC分类号： H05K7/20936 , F25B31/006 , H02K9/12 , H02K9/14 , H02K11/33
摘要： A thermal system is disclosed in thermal communication with an electrical device. In one form the thermal system is a refrigeration system having a compressor, condenser, and evaporator. The electrical device can be disposed within the thermal system such that a working fluid of the thermal system exchanges heat with the electrical device. In one embodiment the thermal system includes a container in which the electrical device is disposed. The working fluid in the container can, but need not, remain in substantially the same physical state when transferring heat with the electrical device.
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，热系统是具有压缩机，冷凝器和蒸发器的制冷系统。电气设备可以设置在热系统内，使得热系统的工作流体与电气设备交换热量。在一个实施例中，热系统包括其中设置电气设备的容器。当与电气设备传热时，容器中的工作流体可以但不一定保持基本上相同的物理状态。

2. 发明申请

US20120247117A1 VEHICLE SYSTEM 有权
标题翻译：车辆系统
公开(公告)号：US20120247117A1
公开(公告)日：2012-10-04
申请号：US13432590
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： F02C6/08 , F02C6/20 , F02C6/00
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。

3. 发明申请

US20120079830A1 SENSOR COMMUNICATION SYSTEM AND MACHINE HAVING THE SAME 有权
标题翻译：传感器通信系统和具有相同功能的机器
公开(公告)号：US20120079830A1
公开(公告)日：2012-04-05
申请号：US13153223
申请日：2011-06-03
申请人： Rigoberto Rodriguez , Mark Blackwelder
发明人： Rigoberto Rodriguez , Mark Blackwelder
IPC分类号： F01B25/00 , G01M15/00
CPC分类号： F01D17/02 , F01D17/085 , F01D17/20 , F01D25/162 , F23M11/045 , H04Q9/00 , Y02T50/671
摘要： A sensor communication system includes an electromagnetic waveguide disposed adjacent to at least one component of a machine. The electromagnetic waveguide can be configured to convey a fluid within the machine. The sensor communication system can also include a sensor assembly, which includes a sensor operable to sense at least one condition and a transmitter at least partially positioned in the electromagnetic waveguide. The transmitter can be operatively coupled to the sensor and be operable to emit a signal corresponding to the at least one condition sensed by the sensor. The sensor communication system can also include a receiver at least partially positioned in the electromagnetic waveguide and operable to wirelessly receive the signal emitted by the transmitter.
摘要翻译：传感器通信系统包括邻近机器的至少一个部件设置的电磁波导。电磁波导可以被配置为在机器内传送流体。传感器通信系统还可以包括传感器组件，其包括可操作以感测至少一个状态的传感器和至少部分地定位在电磁波导中的发射器。发射器可以可操作地耦合到传感器并且可操作地发射对应于由传感器感测的至少一个状态的信号。传感器通信系统还可以包括至少部分地位于电磁波导中并且可操作以无线地接收由发射机发射的信号的接收器。

4. 发明授权

US09303523B2 Sensor communication system and machine having the same 有权
标题翻译：传感器通信系统和机器具有相同的功能
公开(公告)号：US09303523B2
公开(公告)日：2016-04-05
申请号：US13153223
申请日：2011-06-03
申请人： Rigoberto Rodriguez , Mark Blackwelder
发明人： Rigoberto Rodriguez , Mark Blackwelder
IPC分类号： F01D17/02 , F01D17/20 , F01D25/16 , F01D17/08 , F23M11/04 , H04Q9/00
CPC分类号： F01D17/02 , F01D17/085 , F01D17/20 , F01D25/162 , F23M11/045 , H04Q9/00 , Y02T50/671
摘要： A sensor communication system includes an electromagnetic waveguide disposed adjacent to at least one component of a machine. The electromagnetic waveguide can be configured to convey a fluid within the machine. The sensor communication system can also include a sensor assembly, which includes a sensor operable to sense at least one condition and a transmitter at least partially positioned in the electromagnetic waveguide. The transmitter can be operatively coupled to the sensor and be operable to emit a signal corresponding to the at least one condition sensed by the sensor. The sensor communication system can also include a receiver at least partially positioned in the electromagnetic waveguide and operable to wirelessly receive the signal emitted by the transmitter.
摘要翻译：传感器通信系统包括邻近机器的至少一个部件设置的电磁波导。电磁波导可以被配置为在机器内传送流体。传感器通信系统还可以包括传感器组件，其包括可操作以感测至少一个状态的传感器和至少部分地定位在电磁波导中的发射器。发射器可以可操作地耦合到传感器并且可操作地发射对应于由传感器感测的至少一个状态的信号。传感器通信系统还可以包括至少部分地位于电磁波导中并且可操作以无线地接收由发射机发射的信号的接收器。

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。

7. 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。

8. 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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