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1. 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。

2. 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。

3. 发明授权

US06817575B1 Integrated system for providing aircraft environmental control 有权
标题翻译：提供飞机环境控制的综合系统
公开(公告)号：US06817575B1
公开(公告)日：2004-11-16
申请号：US10251721
申请日：2002-09-20
申请人： Jules Ricardo Munoz , Luca Bertuccioli , Michael K. Sahm , Jay Fletcher , Charles E. Lents , Steven E. Squier , Richard Welch , Arthur Curtis Becker
发明人： Jules Ricardo Munoz , Luca Bertuccioli , Michael K. Sahm , Jay Fletcher , Charles E. Lents , Steven E. Squier , Richard Welch , Arthur Curtis Becker
IPC分类号： B64D1308
CPC分类号： B64D13/06 , B64D2013/0614
摘要： The present invention relates to an integrated enviromental control system for an aircraft. The system uses bleed air from a propulsion engine to drive an air turbine which provides power to at least one aircraft component such as an aircraft mounted accessory drive. The system uses the bleed air exiting the air turbine as an air source for the cabin and/or flight deck enviromental control system.
摘要翻译：本发明涉及一种用于飞行器的综合环境控制系统。该系统使用来自推进发动机的排气来驱动空气涡轮机，该空气涡轮机向诸如飞机安装的附件驱动器的至少一个飞行器部件提供动力。该系统使用离开空气涡轮机的排气作为客舱和/或驾驶舱环境控制系统的空气源。

4. 发明授权

US06796527B1 Integrated air turbine driven system for providing aircraft environmental control 有权
标题翻译：集成的空气涡轮驱动系统，为飞机提供环境控制
公开(公告)号：US06796527B1
公开(公告)日：2004-09-28
申请号：US10251720
申请日：2002-09-20
申请人： Jules Ricardo Munoz , Luca Bertuccioli , Michael K. Sahm , Jay Fletcher , Charles E. Lents , Steve Squier , Richard Welch , Arthur Curtis Becker
发明人： Jules Ricardo Munoz , Luca Bertuccioli , Michael K. Sahm , Jay Fletcher , Charles E. Lents , Steve Squier , Richard Welch , Arthur Curtis Becker
IPC分类号： B64D1100
CPC分类号： B64D13/06 , B64D2013/0607 , B64D2013/0614
摘要： The present invention relates to an integrated air turbine driving system for providing aircraft environmental control. The system has at least one air driven turbine for providing power to an aircraft mounted accessory drive and for providing heated air to an aircraft anti-ice system. The system further has a subsystem for supplying cooled pressurized air to a flight deck and/or cabin and to aircraft avionics. Still further, the subsystem provides cooling air to other aircraft components such as a generator and/or an aircraft mounted accessory drive.
摘要翻译：本发明涉及一种用于提供飞行器环境控制的综合空气涡轮驱动系统。该系统具有至少一个用于向飞机安装的附件驱动器提供动力并用于向飞机防冰系统提供加热空气的空气驱动涡轮机。该系统还具有用于将冷却的加压空气供应到飞行甲板和/或舱室以及飞机航空电子设备的子系统。此外，子系统向其它飞行器部件（例如发电机和/或飞机安装的附件驱动器）提供冷却空气。

5. 发明申请

US20110204162A1 ARRANGEMENT FOR CONTROLLING FLUID JETS INJECTED INTO A FLUID STREAM 有权
标题翻译：控制注入流体流中的流体喷嘴的装置
公开(公告)号：US20110204162A1
公开(公告)日：2011-08-25
申请号：US13094881
申请日：2011-04-27
申请人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
发明人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
IPC分类号： B05B1/34
CPC分类号： F02K1/28 , F01D5/145 , F02C6/08 , F02K1/38 , F02K1/46 , F23D14/583 , Y02T50/673 , Y10T137/0329
摘要： In an air mixing arrangement wherein a primary fluid is introduced through an opening in a wall to be mixed with a secondary fluid flowing along the wall surface, the opening is airfoil shaped with its leading edge being orientated at an attack angle with respect to the secondary fluid flow stream so as to thereby enhance the penetration and dispersion of the primary fluid stream into the secondary fluid stream. The airfoil shaped opening is selectively positioned such that its angle of attack provides the desired lift to optimize the mixing of the two streams for the particular application. In one embodiment, a collar is provided around the opening to prevent the secondary fluid from contacting the surface of the wall during certain conditions of operation. Multiple openings maybe used such as the combination of a larger airfoil shaped opening with a smaller airfoil shaped opened positioned downstream thereof, or a round shaped opening placed upstream of an airfoil shaped opening. Pairs of openings and associated collars maybe placed in symmetric relationship so as to promote mixing in particular applications, and nozzles maybe placed on the inner side of wall to enhance the flow characteristics of the primary fluid.
摘要翻译：在空气混合装置中，其中主要流体通过壁中的开口引入以与沿着壁表面流动的次级流体混合，所述开口是翼型，其前缘相对于次级流体流动，从而增强初级流体流进入次级流体流的渗透和分散。翼型开口被选择性地定位成使得其迎角提供所需的升力以优化用于特定应用的两个流的混合。在一个实施例中，围绕开口设置套环，以防止在某些操作条件下次要流体接触壁的表面。可以使用多个开口，例如较大的翼型形状的开口与位于其下游的较小的翼型形状的组合，或者设置在翼型形状的开口的上游的圆形开口。一对开口和相关的套环可以放置在对称关系中，以促进特定应用中的混合，并且喷嘴可以放置在壁的内侧以增强初级流体的流动特性。

6. 发明授权

US08015827B2 Arrangement for controlling fluid jets injected into a fluid stream 有权
标题翻译：用于控制注入流体流中的流体射流的布置
公开(公告)号：US08015827B2
公开(公告)日：2011-09-13
申请号：US12142957
申请日：2008-06-20
申请人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Daniel R. Sabatino , Michael K. Sahm , Bernd R. Noack
发明人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Daniel R. Sabatino , Michael K. Sahm , Bernd R. Noack
IPC分类号： F02C6/04
CPC分类号： F02K1/28 , F01D5/145 , F02C6/08 , F02K1/38 , F02K1/46 , F23D14/583 , Y02T50/673 , Y10T137/0329
摘要： In an air mixing arrangement wherein a primary fluid is introduced through an opening in a wall to be mixed with a secondary fluid flowing along the wall surface, the opening is airfoil shaped with its leading edge being orientated at an attack angle with respect to the secondary fluid flow stream so as to thereby enhance the penetration and dispersion of the primary fluid stream into the secondary fluid stream. The airfoil shaped opening is selectively positioned such that its angle of attack provides the desired lift to optimize the mixing of the two streams for the particular application. In one embodiment, a collar is provided around the opening to prevent the secondary fluid from contacting the surface of the wall during certain conditions of operation. Multiple openings maybe used such as the combination of a larger airfoil shaped opening with a smaller airfoil shaped opened positioned downstream thereof, or a round shaped opening placed upstream of an airfoil shaped opening. Pairs of openings and associated collars maybe placed in symmetric relationship so as to promote mixing in particular applications, and nozzles maybe placed on the inner side of wall to enhance the flow characteristics of the primary fluid.
摘要翻译：在空气混合装置中，其中主要流体通过壁中的开口引入以与沿着壁表面流动的次级流体混合，所述开口是翼型，其前缘相对于次级流体流动，从而增强初级流体流进入次级流体流的渗透和分散。翼型开口被选择性地定位成使得其迎角提供所需的升力以优化用于特定应用的两个流的混合。在一个实施例中，围绕开口设置套环，以防止在某些操作条件下次要流体接触壁的表面。可以使用多个开口，例如较大的翼型形状的开口与位于其下游的较小的翼型形状的组合，或者设置在翼型形状的开口的上游的圆形开口。一对开口和相关的套环可以放置在对称关系中，以促进特定应用中的混合，并且喷嘴可以放置在壁的内侧以增强初级流体的流动特性。

7. 发明授权

US08683812B2 Arrangement for controlling fluid jets injected into a fluid stream of a bleed air discharge nozzle 有权
标题翻译：用于控制喷射到排气喷嘴的流体流中的流体喷嘴的布置
公开(公告)号：US08683812B2
公开(公告)日：2014-04-01
申请号：US13094881
申请日：2011-04-27
申请人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
发明人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
IPC分类号： F02C9/18
CPC分类号： F02K1/28 , F01D5/145 , F02C6/08 , F02K1/38 , F02K1/46 , F23D14/583 , Y02T50/673 , Y10T137/0329
摘要： In an air mixing arrangement wherein a primary fluid is introduced through an opening in a wall to be mixed with a secondary fluid flowing along the wall surface, the opening is airfoil shaped with its leading edge being orientated at an attack angle with respect to the secondary fluid flow stream so as to thereby enhance the penetration and dispersion of the primary fluid stream into the secondary fluid stream. The airfoil shaped opening is selectively positioned such that its angle of attack provides the desired lift to optimize the mixing of the two streams for the particular application. In one embodiment, a collar is provided around the opening to prevent the secondary fluid from contacting the surface of the wall during certain conditions of operation. Multiple openings maybe used such as the combination of a larger airfoil shaped opening with a smaller airfoil shaped opened positioned downstream thereof, or a round shaped opening placed upstream of an airfoil shaped opening. Pairs of openings and associated collars maybe placed in symmetric relationship so as to promote mixing in particular applications, and nozzles maybe placed on the inner side of wall to enhance the flow characteristics of the primary fluid.
摘要翻译：在空气混合装置中，其中主要流体通过壁中的开口引入以与沿着壁表面流动的次级流体混合，所述开口是翼型，其前缘相对于次级流体流动，从而增强初级流体流进入次级流体流的渗透和分散。翼型开口被选择性地定位成使得其迎角提供所需的升力以优化用于特定应用的两个流的混合。在一个实施例中，围绕开口设置套环，以防止在某些操作条件下次要流体接触壁的表面。可以使用多个开口，例如较大的翼型形状的开口与位于其下游的较小的翼型形状的组合，或者设置在翼型形状的开口的上游的圆形开口。一对开口和相关的套环可以放置在对称关系中，以促进特定应用中的混合，并且喷嘴可以放置在壁的内侧以增强初级流体的流动特性。

8. 发明申请

US20080251128A1 ARRANGEMENT FOR CONTROLLING FLUID JETS INJECTED INTO A FLUID STREAM 有权
标题翻译：控制注入流体流中的流体喷嘴的装置
公开(公告)号：US20080251128A1
公开(公告)日：2008-10-16
申请号：US12143037
申请日：2008-06-20
申请人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
发明人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
IPC分类号： B67D5/56
CPC分类号： F02K1/28 , F01D5/145 , F02C6/08 , F02K1/38 , F02K1/46 , F23D14/583 , Y02T50/673 , Y10T137/0329
摘要： In an air mixing arrangement wherein a primary fluid is introduced through an opening in a wall to be mixed with a secondary fluid flowing along the wall surface, the opening is airfoil shaped with its leading edge being orientated at an attack angle with respect to the secondary fluid flow stream so as to thereby enhance the penetration and dispersion of the primary fluid stream into the secondary fluid stream. The airfoil shaped opening is selectively positioned such that its angle of attack provides the desired lift to optimize the mixing of the two streams for the particular application. In one embodiment, a collar is provided around the opening to prevent the secondary fluid from contacting the surface of the wall during certain conditions of operation. Multiple openings maybe used such as the combination of a larger airfoil shaped opening with a smaller airfoil shaped opened positioned downstream thereof, or a round shaped opening placed upstream of an airfoil shaped opening. Pairs of openings and associated collars maybe placed in symmetric relationship so as to promote mixing in particular applications, and nozzles maybe placed on the inner side of wall to enhance the flow characteristics of the primary fluid.
摘要翻译：在空气混合装置中，其中主要流体通过壁中的开口引入以与沿着壁表面流动的次级流体混合，所述开口是翼型，其前缘相对于次级流体流动，从而增强初级流体流进入次级流体流的渗透和分散。翼型开口被选择性地定位成使得其迎角提供所需的升力以优化用于特定应用的两个流的混合。在一个实施例中，围绕开口设置套环，以防止在某些操作条件下次要流体接触壁的表面。可以使用多个开口，例如较大的翼型形状的开口与位于其下游的较小的翼型形状的组合，或者设置在翼型形状的开口的上游的圆形开口。一对开口和相关的套环可以放置在对称关系中，以促进特定应用中的混合，并且喷嘴可以放置在壁的内侧以增强初级流体的流动特性。

9. 发明授权

US08136342B2 Arrangement for controlling fluid jets injected into a fluid stream 有权
标题翻译：用于控制注入流体流中的流体射流的布置
公开(公告)号：US08136342B2
公开(公告)日：2012-03-20
申请号：US12950530
申请日：2010-11-19
申请人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
发明人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
IPC分类号： F02K1/00
CPC分类号： F02K1/28 , F01D5/145 , F02C6/08 , F02K1/38 , F02K1/46 , F23D14/583 , Y02T50/673 , Y10T137/0329
摘要： In an air mixing arrangement wherein a primary fluid is introduced through an opening in a wall to be mixed with a secondary fluid flowing along the wall surface, the opening is airfoil shaped with its leading edge being orientated at an attack angle with respect to the secondary fluid flow stream so as to thereby enhance the penetration and dispersion of the primary fluid stream into the secondary fluid stream. The airfoil shaped opening is selectively positioned such that its angle of attack provides the desired lift to optimize the mixing of the two streams for the particular application. In one embodiment, a collar is provided around the opening to prevent the secondary fluid from contacting the surface of the wall during certain conditions of operation. Multiple openings maybe used such as the combination of a larger airfoil shaped opening with a smaller airfoil shaped opened positioned downstream thereof, or a round shaped opening placed upstream of an airfoil shaped opening. Pairs of openings and associated collars maybe placed in symmetric relationship so as to promote mixing in particular applications, and nozzles maybe placed on the inner side of wall to enhance the flow characteristics of the primary fluid.
摘要翻译：在空气混合装置中，其中主要流体通过壁中的开口引入以与沿着壁表面流动的次级流体混合，所述开口是翼型，其前缘相对于次级流体流动，从而增强初级流体流进入次级流体流的渗透和分散。翼型开口被选择性地定位成使得其迎角提供所需的升力以优化用于特定应用的两个流的混合。在一个实施例中，围绕开口设置套环，以防止在某些操作条件下次要流体接触壁的表面。可以使用多个开口，例如较大的翼型形状的开口与位于其下游的较小的翼型形状的组合，或者设置在翼型形状的开口的上游的圆形开口。一对开口和相关的套环可以放置在对称关系中，以促进特定应用中的混合，并且喷嘴可以放置在壁的内侧以增强初级流体的流动特性。

10. 发明授权

US07976213B2 Arrangement for controlling fluid jets injected into a fluid stream 有权
标题翻译：用于控制注入流体流中的流体射流的布置
公开(公告)号：US07976213B2
公开(公告)日：2011-07-12
申请号：US12143037
申请日：2008-06-20
申请人： Fabio P. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
发明人： Fabio P. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
IPC分类号： B01F5/06
CPC分类号： F02K1/28 , F01D5/145 , F02C6/08 , F02K1/38 , F02K1/46 , F23D14/583 , Y02T50/673 , Y10T137/0329
摘要： In an air mixing arrangement wherein a primary fluid is introduced through an opening in a wall to be mixed with a secondary fluid flowing along the wall surface, the opening is airfoil shaped with its leading edge being orientated at an attack angle with respect to the secondary fluid flow stream to enhance penetration and dispersion of the primary fluid stream into the secondary fluid stream. The airfoil shaped opening is selectively positioned such that its angle of attack provides the desired lift to optimize the mixing of the two streams for the particular application. Embodiments of the arrangement can comprise a collar around the openings, multiple openings that comprise a larger opening and a smaller opening positioned downstream, pairs of openings and associated collars symmetric relationship, and nozzles on the inner side of the wall.
摘要翻译：在空气混合装置中，其中主要流体通过壁中的开口引入以与沿着壁表面流动的次级流体混合，所述开口是翼型，其前缘相对于次级流体流动以增强初级流体流进入次级流体流的渗透和分散。翼型开口被选择性地定位成使得其迎角提供所需的升力以优化用于特定应用的两个流的混合。该装置的实施例可以包括围绕开口的轴环，包括较大开口的多个开口和位于下游，一对开口和相关联的轴环对称关系的较小开口以及壁内侧上的喷嘴。

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