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1. 发明授权

US07527675B2 Electrostatic particulate separation system and device 有权
标题翻译：静电颗粒分离系统和装置
公开(公告)号：US07527675B2
公开(公告)日：2009-05-05
申请号：US11520261
申请日：2006-09-13
申请人： Luca Bertuccioli , Bruce H. Easom , Leo A. Smolensky , Sergei F. Burlatsky , Eric J. Gottung , Michael A. Sloan , Lewis G. Hinman, III
发明人： Luca Bertuccioli , Bruce H. Easom , Leo A. Smolensky , Sergei F. Burlatsky , Eric J. Gottung , Michael A. Sloan , Lewis G. Hinman, III
IPC分类号： B03C3/15
CPC分类号： B03C3/017 , B03C3/15 , B03C2201/08
摘要： A device separates particulates from a gas stream flowing through the device. The device includes at least one high voltage electrode and a substantially cylindrical separator. The high voltage electrode applies a first voltage to the gas stream. The separator has an inlet for introducing the gas stream into the separator tangentially to an interior wall of the separator, a particulate outlet for expelling the particulates from the separator, and a gas stream outlet.
摘要翻译：装置将颗粒与流过装置的气流分离。该装置包括至少一个高压电极和基本上圆柱形的分离器。高压电极向气流施加第一电压。分离器具有用于将气流引导到分离器中的入口，其与分离器的内壁切向，用于从分离器排出微粒的颗粒出口和气流出口。

2. 发明申请

US20080060522A1 Electrostatic particulate separation system and device 有权
标题翻译：静电颗粒分离系统和装置
公开(公告)号：US20080060522A1
公开(公告)日：2008-03-13
申请号：US11520261
申请日：2006-09-13
申请人： Luca Bertuccioli , Bruce H. Easom , Leo A. Smolensky , Sergei F. Burlatsky , Eric J. Gottung , Michael A. Sloan , Lewis G. Hinman
发明人： Luca Bertuccioli , Bruce H. Easom , Leo A. Smolensky , Sergei F. Burlatsky , Eric J. Gottung , Michael A. Sloan , Lewis G. Hinman
IPC分类号： B03C3/14
CPC分类号： B03C3/017 , B03C3/15 , B03C2201/08
摘要： A device separates particulates from a gas stream flowing through the device. The device includes at least one high voltage electrode and a substantially cylindrical separator. The high voltage electrode applies a first voltage to the gas stream. The separator has an inlet for introducing the gas stream into the separator tangentially to an interior wall of the separator, a particulate outlet for expelling the particulates from the separator, and a gas stream outlet.
摘要翻译：装置将颗粒与流过装置的气流分离。该装置包括至少一个高压电极和基本上圆柱形的分离器。高压电极向气流施加第一电压。分离器具有用于将气流引导到分离器中的入口，其与分离器的内壁切向，用于从分离器排出微粒的颗粒出口和气流出口。

3. 发明申请

US20090277325A1 ELECTROSTATIC PARTICULATE SEPARATION FOR EMISSION TREATMENT SYSTEMS 有权
标题翻译：用于排放处理系统的静电颗粒分离
公开(公告)号：US20090277325A1
公开(公告)日：2009-11-12
申请号：US12116334
申请日：2008-05-07
申请人： Eric J. Gottung , Bruce H. Easom , Sergei F. Burlatsky , Leo A. Smolensky , Luca Bertuccioli
发明人： Eric J. Gottung , Bruce H. Easom , Sergei F. Burlatsky , Leo A. Smolensky , Luca Bertuccioli
IPC分类号： B01D45/00 , B03C3/017 , B01D50/00 , B03C3/01 , B01D45/12 , B01D46/46
CPC分类号： B01D45/12 , B01D46/0021 , B01D46/0024 , B01D46/0032 , B01D46/2407 , B01D50/002 , B03C3/017 , B03C3/06 , B03C3/15 , B03C2201/30
摘要： An emission treatment system includes a separation device having a vessel that includes an inlet for receiving an emission stream having entrained solid particles. A first outlet from the vessel discharges captured solid particles from the emission stream and a second outlet from the vessel discharges a clean stream having fewer entrained solid particles than the emission stream received into the separation device. A particle collector is fluidly connected with the separation device and includes a collection portion for capturing solid particles from the emission stream.
摘要翻译：排放处理系统包括具有容器的分离装置，该容器包括用于接收具有夹带的固体颗粒的排放流的入口。来自容器的第一出口从排放物流排放捕获的固体颗粒，并且来自容器的第二出口排出具有比接收到分离装置中的排放流更少的夹带的固体颗粒的清洁流。颗粒收集器与分离装置流体连接，并且包括用于从排放流捕获固体颗粒的收集部分。

4. 发明授权

US07883558B2 Electrostatic particulate separation for emission treatment systems 有权
标题翻译：排放处理系统的静电颗粒分离
公开(公告)号：US07883558B2
公开(公告)日：2011-02-08
申请号：US12116334
申请日：2008-05-07
申请人： Eric J. Gottung , Bruce H. Easom , Sergei F. Burlatsky , Leo A. Smolensky , Luca Bertuccioli
发明人： Eric J. Gottung , Bruce H. Easom , Sergei F. Burlatsky , Leo A. Smolensky , Luca Bertuccioli
IPC分类号： B03C3/14
CPC分类号： B01D45/12 , B01D46/0021 , B01D46/0024 , B01D46/0032 , B01D46/2407 , B01D50/002 , B03C3/017 , B03C3/06 , B03C3/15 , B03C2201/30
摘要： An emission treatment system includes a separation device having a vessel that includes an inlet for receiving an emission stream having entrained solid particles. A first outlet from the vessel discharges captured solid particles from the emission stream and a second outlet from the vessel discharges a clean stream having fewer entrained solid particles than the emission stream received into the separation device. A particle collector is fluidly connected with the separation device and includes a collection portion for capturing solid particles from the emission stream.
摘要翻译：排放处理系统包括具有容器的分离装置，该容器包括用于接收具有夹带的固体颗粒的排放流的入口。来自容器的第一出口从排放物流排放捕获的固体颗粒，并且来自容器的第二出口排出具有比接收到分离装置中的排放流更少的夹带的固体颗粒的清洁流。颗粒收集器与分离装置流体连接，并且包括用于从排放流捕获固体颗粒的收集部分。

5. 发明授权

US06663044B1 Vapor compression cycle environmental control system 有权
标题翻译：蒸汽压缩循环环境控制系统
公开(公告)号：US06663044B1
公开(公告)日：2003-12-16
申请号：US10251719
申请日：2002-09-20
申请人： Jules Ricardo Munoz , Luca Bertuccioli , Michael K. Sahm , Jay Fletcher , Charles E. Lents , Richard Welch , Steve Squier , Arthur Chris Becker
发明人： Jules Ricardo Munoz , Luca Bertuccioli , Michael K. Sahm , Jay Fletcher , Charles E. Lents , Richard Welch , Steve Squier , Arthur Chris Becker
IPC分类号： B64D1100
CPC分类号： B64D13/06 , B64D2013/0607 , B64D2013/0618 , B64D2013/0644 , B64D2013/0648 , Y02T50/56
摘要： The present invention relates to a vapor compression cycle environmental control system for use on aircraft. The system includes an environmental control subsystem which supplies pressurized ram air at a desired temperature to the aircraft's flight deck and/or cabin. The environmental control subsystem uses a vapor compression cycle subsystem to provide the ram air at the desired temperature. The system further includes an air turbine driven by engine bleed air to provide power to an aircraft mounted accessory drive and to provide heated air to an anti-ice system. The aircraft mounted accessory drive provides power to an air compressor which forms part of the environmental control subsystem and to a working fluid compressor which forms part of the vapor compression cycle subsystem.
摘要翻译：本发明涉及一种用于飞机上的蒸汽压缩循环环境控制系统。该系统包括环境控制子系统，其将期望温度的加压冲压空气供应到飞行器的驾驶舱和/或舱室。环境控制子系统使用蒸汽压缩循环子系统来提供在所需温度下的冲压空气。该系统还包括由发动机排放空气驱动的空气涡轮机，以向飞机安装的附件驱动器提供动力，并将热空气提供给防冰系统。飞机安装的附件驱动器为形成环境控制子系统的一部分的空气压缩机和形成蒸气压缩循环子系统的一部分的工作流体压缩机提供动力。

6. 发明申请

US20050166598A1 GAS TURBINE COOLING SYSTEM 有权
标题翻译：气体涡轮冷却系统
公开(公告)号：US20050166598A1
公开(公告)日：2005-08-04
申请号：US10767582
申请日：2004-01-29
申请人： Louis Spadaccini , He Huang , Luca Bertuccioli , Robert Bayt
发明人： Louis Spadaccini , He Huang , Luca Bertuccioli , Robert Bayt
IPC分类号： F02C7/12 , F02C3/24 , F02C7/18 , F02C7/22 , F02C7/224
CPC分类号： B01D19/0031 , F02C7/185 , F02C7/224 , Y02T50/672 , Y02T50/675
摘要： A cooling system for a gas turbine engine includes a fuel deoxygenator for increasing the cooling capacity of the fuel. The fuel deoxygenator removes dissolved gases from the fuel to prevent the formation of insoluble deposits. The prevention of insoluble deposits increases the usable cooling capacity of the fuel. The increased cooling capacity of the deoxygenated fuel provides a greater heat sink for cooling air used to protect engine components. The improved cooling capacity of the cooling air provides for increased engine operating temperatures that improves overall engine efficiency.
摘要翻译：用于燃气涡轮发动机的冷却系统包括用于增加燃料的冷却能力的燃料脱氧器。燃料脱氧器从燃料中除去溶解的气体，以防止形成不溶性沉积物。防止不溶性沉积物增加燃料的可用冷却能力。脱氧燃料的增加的冷却能力为用于保护发动机部件的冷却空气提供更大的散热器。冷却空气的改进的冷却能力提供了增加的发动机工作温度，从而提高整体发动机效率。

7. 发明授权

US06908062B2 Reduced bleed vapor compression cycle environmental control system for aircraft 有权
标题翻译：减少航空器泄放蒸气压缩循环环境控制系统
公开(公告)号：US06908062B2
公开(公告)日：2005-06-21
申请号：US10731184
申请日：2003-12-09
申请人： Jules Ricardo Munoz , Luca Bertuccioli , Roger W. Radomsky, Jr.
发明人： Jules Ricardo Munoz , Luca Bertuccioli , Roger W. Radomsky, Jr.
IPC分类号： B64D13/06 , B64D13/08
CPC分类号： B64D13/06 , B64D13/08 , B64D2013/0614 , B64D2013/0618 , Y02T50/44 , Y02T50/56
摘要： The present invention relates to A reduced bleed vapor compression cycle environmental control system for an aircraft. The environmental control system provides conditioned external ram air to compartments such as the cabin, the flight deck, avionics compartment, and other equipment compartments, where conditioned air is needed. The system includes a first compressor for compressing the external ram air to cabin pressure and an evaporator for cooling the external ram air to a desired temperature. The system further includes a low-pressure water separator for removing moisture from the ram air prior to the external ram air being delivered to the compartment(s). The ram air compressor as well as a compressor for a refrigerant loop are driven by a turbine that expands a minimal amount of bleed air from an engine.
摘要翻译：本发明涉及一种用于飞行器的减少放气蒸气压缩循环环境控制系统。环境控制系统为舱室，驾驶舱，航空电子设备室和需要调节空气的其他设备隔间提供空调的外部冲压空气。该系统包括用于将外部冲压空气压缩至机舱压力的第一压缩机和用于将外部冲压空气冷却至所需温度的蒸发器。该系统还包括一个低压水分离器，用于在外部冲压空气输送到隔室之前从冲压空气中除去水分。压头空气压缩机以及用于制冷剂回路的压缩机由涡轮机驱动，该涡轮机从发动机膨胀最少量的排出空气。

8. 发明授权

US06939392B2 System and method for thermal management 有权
标题翻译：热管理系统和方法
公开(公告)号：US06939392B2
公开(公告)日：2005-09-06
申请号：US10657299
申请日：2003-09-08
申请人： He Huang , Scott F. Kaslusky , Thomas G. Tillman , Timothy D. DeValve , Luca Bertuccioli , Michael K. Sahm , Louis J. Spadaccini , Robert L. Bayt , Foster Philip Lamm , Daniel R. Sabatino
发明人： He Huang , Scott F. Kaslusky , Thomas G. Tillman , Timothy D. DeValve , Luca Bertuccioli , Michael K. Sahm , Louis J. Spadaccini , Robert L. Bayt , Foster Philip Lamm , Daniel R. Sabatino
IPC分类号： C10L1/00 , B01D19/00 , B01D61/00 , B01D63/08 , B01D65/08 , B01D69/10 , B01D69/12 , B01D71/32 , B01D71/36 , F02C7/12 , F02C7/14 , F02C7/224
CPC分类号： B01D69/10 , B01D19/0031 , B01D61/00 , B01D63/082 , B01D63/084 , B01D65/08 , B01D2321/2008 , F02C7/12 , F02C7/14 , F02C7/224 , Y02T50/672 , Y02T50/675
摘要： A system for the management of thermal transfer in a gas turbine engine includes a heat generating sub-system in operable communication with the engine, a fuel source to supply a fuel, a fuel stabilization unit to receive the fuel from the fuel source and to provide the fuel to the engine, and a heat exchanger in thermal communication with the fuel to transfer heat from the heat generating sub-system to the fuel. A method of managing thermal transfer in an aircraft includes removing oxygen from a stream of a fuel fed to an engine used to drive the aircraft, transferring heat from a heat generating sub-system of the aircraft to the fuel, and combusting the fuel. A system for the thermal management of an aircraft provides for powering the aircraft, supplying a fuel deoxygenating the fuel, and transferring heat between a heat generating sub-system of the aircraft and the fuel.
摘要翻译：用于管理燃气涡轮发动机中的热传递的系统包括与发动机可操作地连通的发热子系统，用于供应燃料的燃料源，用于从燃料源接收燃料的燃料稳定单元，并且提供到发动机的燃料，以及与燃料热连通以将热量从发热子系统传递到燃料的热交换器。一种管理飞行器中的热转移的方法包括从供给到用于驱动飞行器的发动机的燃料流中除去氧气，将热量从飞机的发热子系统传递到燃料，并燃烧燃料。飞机的热管理系统为飞机提供动力，提供燃料脱氧燃料，并在飞机的发热子系统与燃料之间传递热量。

9. 发明授权

US07610179B2 Coupled parametric design of flow control and duct shape 有权
标题翻译：流量控制和管道形状的耦合参数化设计
公开(公告)号：US07610179B2
公开(公告)日：2009-10-27
申请号：US10948114
申请日：2004-09-24
申请人： Razvan Florea , Luca Bertuccioli
发明人： Razvan Florea , Luca Bertuccioli
IPC分类号： G06F17/50 , G06G7/48
CPC分类号： F01D25/305 , F01D5/145 , F01D9/023 , F01D17/105 , F02C9/18 , F05D2270/17 , G06F17/5009 , G06F2217/16 , Y02T50/673 , Y02T50/675
摘要： A method for designing gas turbine engine components using a coupled parametric analysis of part geometry and flow control is disclosed. Included are the steps of parametrically defining the geometry of the duct wall shape, parametrically defining one or more flow control actuators in the duct wall, measuring a plurality of performance parameters or metrics (e.g., flow characteristics) of the duct and comparing the results of the measurement with desired or target parameters, and selecting the optimal duct geometry and flow control for at least a portion of the duct, the selection process including evaluating the plurality of performance metrics in a pareto analysis. The use of this method in the design of inter-turbine transition ducts, serpentine ducts, inlets, diffusers, and similar components provides a design which reduces pressure losses and flow profile distortions.
摘要翻译：公开了一种使用零件几何和流量控制的耦合参数分析来设计燃气涡轮发动机部件的方法。包括参数定义管道壁形状的几何形状的步骤，参数地定义管道壁中的一个或多个流量控制致动器，测量管道的多个性能参数或度量（例如，流动特性），并比较所述测量具有期望的或目标参数，以及为所述管道的至少一部分选择最佳管道几何形状和流量控制，所述选择过程包括在帕累托分析中评估所述多个性能度量。在涡轮机过渡管道，蛇形管道，入口，扩散器和类似部件的设计中使用这种方法提供了减少压力损失和流量失真的设计。

10. 发明授权

US07231769B2 Gas turbine cooling system 有权
标题翻译：燃气轮机冷却系统
公开(公告)号：US07231769B2
公开(公告)日：2007-06-19
申请号：US10767582
申请日：2004-01-29
申请人： Louis J. Spadaccini , He Huang , Luca Bertuccioli , Robert L. Bayt
发明人： Louis J. Spadaccini , He Huang , Luca Bertuccioli , Robert L. Bayt
IPC分类号： F02C7/14
CPC分类号： B01D19/0031 , F02C7/185 , F02C7/224 , Y02T50/672 , Y02T50/675
摘要： A cooling system for a gas turbine engine includes a fuel deoxygenator for increasing the cooling capacity of the fuel. The fuel deoxygenator removes dissolved gases from the fuel to prevent the formation of insoluble deposits. The prevention of insoluble deposits increases the usable cooling capacity of the fuel. The increased cooling capacity of the deoxygenated fuel provides a greater heat sink for cooling air used to protect engine components. The improved cooling capacity of the cooling air provides for increased engine operating temperatures that improves overall engine efficiency.
摘要翻译：用于燃气涡轮发动机的冷却系统包括用于增加燃料的冷却能力的燃料脱氧器。燃料脱氧器从燃料中除去溶解的气体，以防止形成不溶性沉积物。防止不溶性沉积物增加燃料的可用冷却能力。脱氧燃料的增加的冷却能力为用于保护发动机部件的冷却空气提供更大的散热器。冷却空气的改进的冷却能力提供了增加的发动机工作温度，从而提高整体发动机效率。

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