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1. 发明授权

US07753036B2 Compound cycle rotary engine 有权
标题翻译：复合循环旋转发动机
公开(公告)号：US07753036B2
公开(公告)日：2010-07-13
申请号：US11824645
申请日：2007-07-02
申请人： Charles E. Lents , Stephen P. Zeppieri , Roy N. Guile , Vincent C. Nardone , Jonathan Lauter , Arindam Dasgupta
发明人： Charles E. Lents , Stephen P. Zeppieri , Roy N. Guile , Vincent C. Nardone , Jonathan Lauter , Arindam Dasgupta
IPC分类号： F02B33/00
CPC分类号： F01C11/008 , F01C1/22 , F02B29/0437 , F02B37/00 , F02B41/10 , F02B53/04 , F02B2275/32 , Y02T10/142 , Y02T10/144 , Y02T10/163 , Y02T10/17
摘要： A compound cycle engine system has a rotary engine, which rotary engine generates exhaust gas. The system further has a compressor for increasing the pressure of inlet air to be supplied to the engine to a pressure in the range of from 3.0 to 5.0 atmospheres and an intercooler for providing the inlet air to the engine at a temperature in the range of from 150 to 250 degrees Fahrenheit. The system further has one or more turbines for extracting energy from the exhaust gas. The Miller Cycle is implemented in the rotary engine, enabling the compression ratio to be lower than the expansion ratio, allowing the overall cycle to be optimized for lowest weight and specific fuel consumption.
摘要翻译：复合循环发动机系统具有旋转发动机，该旋转发动机产生废气。该系统还具有用于将供给发动机的入口空气的压力提高到3.0-5.0大气压的压缩机，以及用于在从...的范围内的温度下向发动机提供入口空气的中间冷却器 150至250华氏度。该系统还具有用于从废气中提取能量的一个或多个涡轮机。米勒循环在旋转发动机中实现，使压缩比低于膨胀比，从而可以优化整体循环，以获得最低的重量和特定的燃油消耗。

2. 发明申请

US20090007882A1 Compound cycle rotary engine 有权
标题翻译：复合循环旋转发动机
公开(公告)号：US20090007882A1
公开(公告)日：2009-01-08
申请号：US11824645
申请日：2007-07-02
申请人： Charles E. Lents , Stephen P. Zeppieri , Roy N. Guile , Vincent C. Nardone , Jonathan Lauter , Arindam Dasgupta
发明人： Charles E. Lents , Stephen P. Zeppieri , Roy N. Guile , Vincent C. Nardone , Jonathan Lauter , Arindam Dasgupta
IPC分类号： F02B53/02
CPC分类号： F01C11/008 , F01C1/22 , F02B29/0437 , F02B37/00 , F02B41/10 , F02B53/04 , F02B2275/32 , Y02T10/142 , Y02T10/144 , Y02T10/163 , Y02T10/17
摘要： A compound cycle engine system has a rotary engine, which rotary engine generates exhaust gas. The system further has a compressor for increasing the pressure of inlet air to be supplied to the engine to a pressure in the range of from 3.0 to 5.0 atmospheres and an intercooler for providing the inlet air to the engine at a temperature in the range of from 150 to 250 degrees Fahrenheit. The system further has one or more turbines for extracting energy from the exhaust gas. The Miller Cycle is implemented in the rotary engine, enabling the compression ratio to be lower than the expansion ratio, allowing the overall cycle to be optimized for lowest weight and specific fuel consumption.
摘要翻译：复合循环发动机系统具有旋转发动机，该旋转发动机产生废气。该系统还具有用于将供给发动机的入口空气的压力提高到3.0-5.0大气压的压缩机，以及用于在从...的范围内的温度下向发动机提供入口空气的中间冷却器 150至250华氏度。该系统还具有用于从废气中提取能量的一个或多个涡轮机。米勒循环在旋转发动机中实现，使压缩比低于膨胀比，从而可以优化整体循环，以获得最低的重量和特定的燃油消耗。

3. 发明申请

US20080070078A1 Jet fuel based high pressure solid oxide fuel cell system 有权
标题翻译：喷气燃料基高压固体氧化物燃料电池系统
公开(公告)号：US20080070078A1
公开(公告)日：2008-03-20
申请号：US11524348
申请日：2006-09-19
申请人： Mallika Gummalla , Jean Yamanis , Benoit Olsommer , Zissis Dardas , Robert Bayt , Hari Srinivasan , Arindam Dasgupta , Larry Hardin
发明人： Mallika Gummalla , Jean Yamanis , Benoit Olsommer , Zissis Dardas , Robert Bayt , Hari Srinivasan , Arindam Dasgupta , Larry Hardin
IPC分类号： H01M8/04 , H01M8/12
CPC分类号： H01M8/0675 , B64D41/00 , B64D2041/005 , H01M8/04014 , H01M8/04097 , H01M8/04111 , H01M8/04141 , H01M8/04164 , H01M8/0612 , H01M8/0618 , H01M8/12 , H01M2250/20 , Y02E60/50 , Y02T50/44 , Y02T90/32 , Y02T90/36
摘要： A power system for an aircraft includes a solid oxide fuel cell system which generates electric power for the aircraft and an exhaust stream; and a heat exchanger for transferring heat from the exhaust stream of the solid oxide fuel cell to a heat requiring system or component of the aircraft. The heat can be transferred to fuel for the primary engine of the aircraft. Further, the same fuel can be used to power both the primary engine and the SOFC. A heat exchanger is positioned to cool reformate before feeding to the fuel cell. SOFC exhaust is treated and used as inerting gas. Finally, oxidant to the SOFC can be obtained from the aircraft cabin, or exterior, or both.
摘要翻译：一种用于飞行器的动力系统包括：为飞行器产生电力的燃料电池系统和排气流; 以及用于将热量从固体氧化物燃料电池的排气流传递到飞行器的需热系统或部件的热交换器。热量可以转移到飞机的主发动机的燃料。此外，可以使用相同的燃料为一次发动机和SOFC供电。定位热交换器以在进料到燃料电池之前冷却重整产物。 SOFC排气被处理并用作惰性气体。最后，可以从飞机机舱，外部或两者获得SOFC的氧化剂。

4. 发明授权

US08394552B2 Jet fuel based high pressure solid oxide fuel cell system 有权
公开(公告)号：US08394552B2
公开(公告)日：2013-03-12
申请号：US11524348
申请日：2006-09-19
申请人： Mallika Gummalla , Jean Yamanis , Benoit Olsommer , Zissis Dardas , Robert Bayt , Hari Srinivasan , Arindam Dasgupta , Larry Hardin
发明人： Mallika Gummalla , Jean Yamanis , Benoit Olsommer , Zissis Dardas , Robert Bayt , Hari Srinivasan , Arindam Dasgupta , Larry Hardin
IPC分类号： H01M4/48
CPC分类号： H01M8/0675 , B64D41/00 , B64D2041/005 , H01M8/04014 , H01M8/04097 , H01M8/04111 , H01M8/04141 , H01M8/04164 , H01M8/0612 , H01M8/0618 , H01M8/12 , H01M2250/20 , Y02E60/50 , Y02T50/44 , Y02T90/32 , Y02T90/36
摘要： A power system for an aircraft includes a solid oxide fuel cell system which generates electric power for the aircraft and an exhaust stream; and a heat exchanger for transferring heat from the exhaust stream of the solid oxide fuel cell to a heat requiring system or component of the aircraft. The heat can be transferred to fuel for the primary engine of the aircraft. Further, the same fuel can be used to power both the primary engine and the SOFC. A heat exchanger is positioned to cool reformate before feeding to the fuel cell. SOFC exhaust is treated and used as inerting gas. Finally, oxidant to the SOFC can be obtained from the aircraft cabin, or exterior, or both.

5. 发明申请

US20100242736A1 PRESSURE-BASED DISSOLVED GAS REMOVAL SYSTEM 有权
标题翻译：基于压力的溶解气体去除系统
公开(公告)号：US20100242736A1
公开(公告)日：2010-09-30
申请号：US12411621
申请日：2009-03-26
申请人： Neal R. Herring , Arindam Dasgupta , Haralambos Cordatos , Thomas G. Tillman , Jeremiah C. Lee
发明人： Neal R. Herring , Arindam Dasgupta , Haralambos Cordatos , Thomas G. Tillman , Jeremiah C. Lee
IPC分类号： B01D19/00
CPC分类号： F23K5/08 , B01D19/0036 , B01D19/0063 , F02C7/22 , F23K2301/10 , F23K2900/05082 , Y02T50/671
摘要： A fuel gas removal system includes a venturi for reducing a pressure of the fuel, a bubble separator containing media to assist in the formation of gas bubbles within the fuel to separate the gas bubbles from the fuel, and a port to remove gas bubbles created by the reduction of pressure of the fuel and the bubble separator.
摘要翻译：燃料气体去除系统包括用于降低燃料压力的文丘里管，气泡分离器，其包含介质以帮助在燃料内形成气泡以将气泡与燃料分开，以及用于除去由气体产生的气泡的端口降低燃料和气泡分离器的压力。

6. 发明授权

US06318077B1 Integrated thermal and exhaust management unit 失效
标题翻译：集成热和排气管理单元
公开(公告)号：US06318077B1
公开(公告)日：2001-11-20
申请号：US09523979
申请日：2000-03-13
申请人： George M. Claypole , Gregory Alan Major , Arindam Dasgupta
发明人： George M. Claypole , Gregory Alan Major , Arindam Dasgupta
IPC分类号： F01N310
CPC分类号： F02G5/02 , F01N3/2006 , F01N3/2033 , F01N3/2889 , F01N5/02 , Y02A50/2322 , Y02T10/16 , Y02T10/166 , Y02T10/26
摘要： An integrated thermal and exhaust management unit for a vehicle comprises a housing defining a chamber and having an inlet through which engine exhaust gas flows. A fuel-fired heater is adjacent to the housing and is operable to heat the engine exhaust gas flowing through the chamber. A catalytic converter is adjacent to and in downstream flow communication with the chamber for catalyzing the engine exhaust gas flowing therethrough. An exhaust gas heat recovery unit is radially adjacent to and in downstream flow communication with the catalytic converter for exchanging exhaust gas heat to liquid heat for transferring to heat-requiring areas of the vehicle. A controller controls the operation of the management unit whereby the fuel-fired heater is powered if the catalyst temperature is less than a catalyst light-off temperature for efficient treatment of vehicle emissions. The exhaust gas heat recovery unit is only powered if the catalyst temperature is at or above the light-off temperature and there are heat-requiring areas in the vehicle.
摘要翻译：用于车辆的集成热和排气管理单元包括限定腔室并具有引擎排气流过的入口的壳体。燃料加热器邻近壳体并且可操作以加热流过腔室的发动机废气。催化转化器邻近并与下游流动连通，用于催化从其流过的发动机废气。废气热回收单元与催化转化器径向相邻并且与下游流动连通，用于将废气热量交换到液体热量以转移到车辆的需热区域。如果催化剂温度低于用于有效地处理车辆排放物的催化剂熄灭温度，则控制器控制管理单元的操作，由此燃料加热器被供电。如果催化剂温度等于或高于起燃温度并且车辆中存在热需要区域，则废气热回收单元仅供电。

7. 发明申请

US20130239542A1 STRUCTURES AND METHODS FOR INTERCOOLING AIRCRAFT GAS TURBINE ENGINES 审中-公开
标题翻译：用于中空飞机气涡轮发动机的结构和方法
公开(公告)号：US20130239542A1
公开(公告)日：2013-09-19
申请号：US13421906
申请日：2012-03-16
申请人： Arindam Dasgupta , Om P. Sharma
发明人： Arindam Dasgupta , Om P. Sharma
IPC分类号： F02C7/143 , F02C7/00
CPC分类号： F02C7/143 , B64D15/02 , B64D33/10 , B64D41/00 , F01D25/02 , F02C7/18 , F02C7/224 , F02K3/06 , F02K3/115 , F05D2220/323 , F05D2260/205 , F05D2260/211 , F05D2260/213 , Y02T50/676
摘要： A turbine engine has a fan comprising a duct and supporting struts, a first compressor configured to pressurize inlet air, and a second compressor configured to further pressurize the inlet air. A cooling circuit is located to cool the inlet air after the inlet air is pressurized by the first compressor and before the inlet air is further pressurized by the second compressor, and includes at least intercooler configured to transfer heat from inlet air to a secondary fluid heat sink.
摘要翻译：涡轮发动机具有包括管道和支撑支柱的风扇，构造成对入口空气加压的第一压缩机和被构造成进一步加压入口空气的第二压缩机。冷却回路被定位成在入口空气被第一压缩机加压之后并且在入口空气被第二压缩机进一步加压之前冷却入口空气，并且至少包括中间冷却器，其构造成将热量从入口空气传递到次级流体热水槽。

8. 发明授权

US08147600B2 Pressure-based dissolved gas removal system 有权
标题翻译：基于压力的溶解气体去除系统
公开(公告)号：US08147600B2
公开(公告)日：2012-04-03
申请号：US12411621
申请日：2009-03-26
申请人： Neal R. Herring , Arindam Dasgupta , Haralambos Cordatos , Thomas G. Tillman , Jeremiah C. Lee
发明人： Neal R. Herring , Arindam Dasgupta , Haralambos Cordatos , Thomas G. Tillman , Jeremiah C. Lee
IPC分类号： B01D19/00
CPC分类号： F23K5/08 , B01D19/0036 , B01D19/0063 , F02C7/22 , F23K2301/10 , F23K2900/05082 , Y02T50/671
摘要： A fuel gas removal system includes a venturi for reducing a pressure of the fuel, a bubble separator containing media to assist in the formation of gas bubbles within the fuel to separate the gas bubbles from the fuel, and a port to remove gas bubbles created by the reduction of pressure of the fuel and the bubble separator.
摘要翻译：燃料气体去除系统包括用于降低燃料压力的文丘里管，气泡分离器，其包含介质以帮助在燃料内形成气泡以将气泡与燃料分开，以及用于除去由气体产生的气泡的端口降低燃料和气泡分离器的压力。

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