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51. 发明申请

US20120222397A1 GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO 有权
公开(公告)号：US20120222397A1
公开(公告)日：2012-09-06
申请号：US13340761
申请日：2011-12-30
申请人： Peter G. Smith , Stuart S. Ochs , Frederick M. Schwarz
发明人： Peter G. Smith , Stuart S. Ochs , Frederick M. Schwarz
IPC分类号： F02K3/075
CPC分类号： F01D17/162 , F04D29/563 , F05D2220/36
摘要： A turbofan engine includes a fan variable area nozzle axially movable relative to the fan nacelle to vary a fan nozzle exit area and adjust a pressure ratio of the fan bypass airflow during engine operation.

52. 发明授权

US08011883B2 Gas turbine engine blade tip clearance apparatus and method 有权
标题翻译：燃气轮机发动机叶片间隙装置及方法
公开(公告)号：US08011883B2
公开(公告)日：2011-09-06
申请号：US12166720
申请日：2008-07-02
申请人： Frederick M. Schwarz , J. Walter Smith
发明人： Frederick M. Schwarz , J. Walter Smith
IPC分类号： F01D11/08
CPC分类号： F01D11/22 , F01D11/20 , F01D11/24 , F04D29/052 , Y02T50/671
摘要： A method for controlling blade tip clearance within a gas turbine engine includes a compressor having at least one first rotor assembly, wherein the blade tips in each of at least one first rotor assembly has a mating geometry with at least one of at least one blade seal surfaces, and a clearance distance extending between the blade tips and the blade seal surfaces; a turbine having at least one second rotor assembly, wherein the blade tips in each of at least one second rotor assembly has a mating geometry with at least one of at least one blade seal surfaces, and a clearance distance extending between the blade tips and the blade seal surfaces; providing an actuator selectively operable to move at least one rotor assembly relative to the shroud; providing an electronic engine controller having a control logic for operating the actuator; and moving at least one first rotor assemblies and at least one second rotor assembly relative to the shroud using the actuator at a response rate according to the control logic to alter the clearance distance.
摘要翻译：用于控制燃气涡轮发动机内的叶片顶端间隙的方法包括具有至少一个第一转子组件的压缩机，其中至少一个第一转子组件中的每一个中的叶片尖端具有与至少一个叶片密封件表面和在叶片尖端和叶片密封表面之间延伸的间隙距离; 具有至少一个第二转子组件的涡轮机，其中至少一个第二转子组件中的每个中的叶片尖端具有与至少一个叶片密封表面中的至少一个的配合几何形状，以及在叶片尖端和叶片密封面; 提供选择性地可操作以相对于护罩移动至少一个转子组件的致动器; 提供具有用于操作致动器的控制逻辑的电子发动机控制器; 以及使用致动器以根据控制逻辑的响应速率相对于护罩移动至少一个第一转子组件和至少一个第二转子组件以改变间隙距离。

53. 发明授权

US07908840B2 Turbine engine with integrated generator having shared lubrication system 有权
标题翻译：具有集成发电机的涡轮发动机具有共享润滑系统
公开(公告)号：US07908840B2
公开(公告)日：2011-03-22
申请号：US11605671
申请日：2006-11-29
申请人： Frederick M. Schwarz , Jorn A. Glahn
发明人： Frederick M. Schwarz , Jorn A. Glahn
IPC分类号： F02C7/06
CPC分类号： F01D25/18 , F01D15/10 , F01D25/12 , F01D25/125 , F02C7/06 , F05D2220/76 , F05D2260/234 , Y02T50/671 , Y02T50/675
摘要： A heat exchange system for use in operating equipment having a plurality of subsystems in each of which a common working fluid is utilized to provide selected operations in that subsystem with a reservoir containing at least some of the common working fluid and has both a supply system and a return system connected between the reservoir and each of the plurality of subsystems through which any common working fluid in the reservoir can be conveyed. An airstream heat exchanger is provided connected in one of the supply and return systems so as to have the common working fluid conveyed therethrough cooled at selectively variable rates in the airstreams passing thereby during at least some such uses of the operating equipment.
摘要翻译：一种用于操作设备的热交换系统，其具有多个子系统，每个子系统中的共用工作流体用于在该子系统中提供包含至少一些公共工作流体的储存器，并具有供应系统和连接在储存器和多个子系统中的每个子系统之间的返回系统，通过该返回系统可以输送储存器中的任何公共工作流体。提供连接在一个供应和返回系统中的气流热交换器，以便在所述操作设备的至少一些这样的使用期间，通过其中通过的空气中的选择性可变速率使输送的通用工作流体冷却。

54. 发明申请

US20100275578A1 COOLING EXCHANGER DUCT 有权
标题翻译：冷却交换机
公开(公告)号：US20100275578A1
公开(公告)日：2010-11-04
申请号：US12820335
申请日：2010-06-22
申请人： Frederick M. Schwarz
发明人： Frederick M. Schwarz
IPC分类号： F02K99/00
CPC分类号： F02C7/14 , F02K3/115 , Y02T50/675
摘要： A method for using a heat exchange system in operating equipment in which a working fluid is utilized in providing selected operations thereof, including for use in lubricating systems for aircraft turbofan engine equipment, the heat exchange system for providing air and working fluid heat exchanges to cool the working fluid at selectively variable rates in the operating equipment developed airstreams. A heat exchanger core is provided in a controlled air flow duct system opening at its entrance to those airstreams and having its outlet end opening downstream in those airstreams.
摘要翻译：一种在操作设备中使用热交换系统的方法，其中使用工作流体来提供其选择的操作，包括用于飞行器涡扇发动机设备的润滑系统，用于提供空气和工作流体热交换以冷却的热交换系统在操作设备中选择性变化的工作流体产生气流。热交换器芯设置在受控的空气流动管道系统中，在其入口处开口，并且其出口端在这些气流中向下游开口。

55. 发明授权

US07810311B2 Cooling exchanger ducts 有权
标题翻译：冷却换热器管道
公开(公告)号：US07810311B2
公开(公告)日：2010-10-12
申请号：US11650825
申请日：2007-01-08
申请人： Frederick M. Schwarz , Jorn A. Glahn
发明人： Frederick M. Schwarz , Jorn A. Glahn
IPC分类号： F02K99/00
CPC分类号： F02C7/14 , F02K3/115 , Y02T50/675
摘要： A heat exchange system for use in operating equipment in which a working fluid is utilized in providing selected operations thereof, including for use in lubricating systems for aircraft turbofan engine equipment, the heat exchange system for providing air and working fluid heat exchanges to cool the working fluid at selectively variable rates in the operating equipment developed airstreams. A heat exchanger core is provided in a controlled air flow duct system opening at its entrance to those airstreams and having its outlet end opening downstream in those airstreams.
摘要翻译：一种用于操作设备的热交换系统，其中使用工作流体来提供其选择的操作，包括用于飞机涡轮风扇发动机设备的润滑系统，用于提供空气的热交换系统和工作流体热交换以冷却工作在操作设备中选择性变化的流体开发出气流。热交换器芯设置在受控的空气流动管道系统中，在其入口处开口，并且其出口端在这些气流中向下游开口。

56. 发明授权

US07407369B2 Gas turbine engine blade tip clearance apparatus and method 有权
标题翻译：燃气轮机发动机叶片间隙装置及方法
公开(公告)号：US07407369B2
公开(公告)日：2008-08-05
申请号：US11253235
申请日：2005-10-17
申请人： Frederick M. Schwarz , J. Walter Smith
发明人： Frederick M. Schwarz , J. Walter Smith
IPC分类号： F01D11/08
CPC分类号： F01D11/122 , F01D11/22 , F01D21/04 , F04D29/052 , F05D2260/403 , F16C23/06 , F16C2360/23 , Y02T50/671
摘要： A zero running clearance system for gas turbine engines includes a gas turbine engine compressor having one or more first rotor assemblies and one or more first stator assemblies disposed adjacent the one or more first rotor assemblies; a gas turbine engine turbine having one or more second rotor assemblies and one or more second stator assemblies disposed adjacent the one or more second rotor assemblies; one or more shroud segments having blade seal surfaces disposed radially outside of the tips of blades of both the first and second rotor assemblies and a clearance distance extending between the blade tips and blade seal surfaces; and, an actuator selectively operable to axially move the first and said second rotor assemblies to alter the clearance distance.
摘要翻译：用于燃气涡轮发动机的零运行间隙系统包括具有一个或多个第一转子组件和邻近一个或多个第一转子组件设置的一个或多个第一定子组件的燃气涡轮发动机压缩机; 具有一个或多个第二转子组件和邻近所述一个或多个第二转子组件设置的一个或多个第二定子组件的燃气涡轮发动机涡轮机; 一个或多个护罩段具有设置在第一和第二转子组件的叶片的尖端的径向外侧的叶片密封表面和在叶片尖端和叶片密封表面之间延伸的间隙距离; 以及致动器，其选择性地可操作以轴向移动所述第一和所述第二转子组件以改变所述间隙距离。

57. 发明申请

US20080134659A1 Zero running clearance centrifugal compressor 有权
标题翻译：零运行间隙离心压缩机
公开(公告)号：US20080134659A1
公开(公告)日：2008-06-12
申请号：US11635123
申请日：2006-12-06
申请人： Frederick M. Schwarz , Jesse W. Smith
发明人： Frederick M. Schwarz , Jesse W. Smith
IPC分类号： F02C3/14 , F03B3/06
CPC分类号： F04D29/051 , F01D11/08 , F01D11/22 , F02C3/08 , F02C7/06 , F04D29/052 , F04D29/059 , F04D29/622 , F04D29/624 , F05D2240/52
摘要： A turbine engine includes an engine housing enclosing: a centrifugal compressor having a rotor; at least one centrifugal compressor bore mounted to the rotor; at least one blade mounted to each of the at least one centrifugal bore and disposed proximate to at least one static wall; a turbine disposed in connection with the centrifugal compressor; a thrust bearing disposed in connection with the rotor; and means for moving said rotor with reference to the at least one static wall attached to the thrust bearing.
摘要翻译：涡轮发动机包括发动机壳体，其包围：具有转子的离心式压缩机; 至少一个安装在转子上的离心式压缩机孔; 至少一个叶片安装到所述至少一个离心孔中的每一个并且设置成邻近至少一个静态壁; 与离心式压缩机连接设置的涡轮机; 与转子相连的推力轴承; 以及用于相对于连接到推力轴承的至少一个静态壁移动所述转子的装置。

58. 发明授权

US07341426B2 Gas turbine engine blade tip clearance apparatus and method 有权
标题翻译：燃气轮机发动机叶片间隙装置及方法
公开(公告)号：US07341426B2
公开(公告)日：2008-03-11
申请号：US11025435
申请日：2004-12-29
申请人： Frederick M. Schwarz , Robert H. Perkinson , Jesse Walter Smith
发明人： Frederick M. Schwarz , Robert H. Perkinson , Jesse Walter Smith
IPC分类号： F01D11/08
CPC分类号： F01D11/22 , F01D11/122 , F04D29/052 , F05D2260/403 , F16C23/06 , F16C2360/23
摘要： A gas turbine engine is provided that includes one or more rotor assemblies, one or more shroud segments, and an actuator. The rotor assemblies are rotatable around an axially extending rotational axis, and each rotor assembly has a plurality of blades. Each blade has a blade tip. The one or more shroud segments each has a blade seal surface disposed radially outside of the one or more rotor assemblies. The blade tips and blade seal surfaces (collectively referred to as the blade seal surface) have mating conical geometries and a clearance distance extending between the blade tips and blade seal surface. The blade tips and blade seal surface are disposed at an angle relative to the axial centerline of the engine, which angle is greater than zero. The actuator is selectively operable to axially move one or both of the shroud segments and rotor assemblies relative to the other of the shroud segments and rotor assemblies to alter the clearance distance.
摘要翻译：提供了一种燃气涡轮发动机，其包括一个或多个转子组件，一个或多个护罩段和致动器。转子组件可围绕轴向延伸的旋转轴线旋转，并且每个转子组件具有多个叶片。每个叶片都有一个叶片尖端。一个或多个护罩段各自具有设置在一个或多个转子组件的径向外侧的叶片密封表面。叶片尖端和叶片密封表面（统称为叶片密封表面）具有匹配的圆锥形几何形状和在叶片尖端和叶片密封表面之间延伸的间隙距离。叶片尖端和叶片密封表面相对于发动机的轴向中心线成角度设置，该角度大于零。致动器可选择性地可操作以相对于护罩段和转子组件中的另一个轴向移动护罩段和转子组件中的一个或两个，以改变间隙距离。

59. 发明授权

US4708588A Turbine cooling air supply system 失效
标题翻译：涡轮冷却空气供应系统
公开(公告)号：US4708588A
公开(公告)日：1987-11-24
申请号：US682042
申请日：1984-12-14
申请人： Frederick M. Schwarz , James G. Griffin
发明人： Frederick M. Schwarz , James G. Griffin
IPC分类号： F01D5/08 , F02C7/18 , F04D29/58
CPC分类号： F02C7/18 , F01D5/081 , Y02T50/676
摘要： Apparatus for supplying pressurized cooling air to the turbine blades (20) of a gas turbine engine is disclosed. Multiple nozzles (38 and 40) of a tangential on-board injection system for pressurizing the cooling air are staged to provide variable rates of cooling airflow to the blades.
摘要翻译：公开了一种用于向燃气涡轮发动机的涡轮机叶片（20）供应加压冷却空气的装置。用于对冷却空气进行加压的切向机载喷射系统的多个喷嘴（38和40）进行分级，以向叶片提供可变速率的冷却气流。

60. 发明授权

US4332133A Compressor bleed system for cooling and clearance control 失效
标题翻译：用于冷却和间隙控制的压缩机排气系统
公开(公告)号：US4332133A
公开(公告)日：1982-06-01
申请号：US94251
申请日：1979-11-14
申请人： Frederick M. Schwarz , James G. Griffin , Vytautis P. Gudaitus
发明人： Frederick M. Schwarz , James G. Griffin , Vytautis P. Gudaitus
IPC分类号： F01D11/00 , F02C7/18 , F02C3/06 , F02C7/28
CPC分类号： F01D11/001 , F02C7/18 , Y02T50/675
摘要： To improve on thrust specific fuel consumption for a gas turbine engine, compressor bleed for turbine cooling is divided into an air distribution system where at least one duct is valved and the other is continuously flowing restrictively with the excess air passing through the turbine mixing with gas path air in the vicinity of the rotating turbine labyrinth type seal to assure seal cooling with sufficient heating of the rotating parts to achieve minimum gap clearance of the seal.
摘要翻译：为了提高燃气轮机的推力特定燃料消耗，用于涡轮冷却的压缩机排气被分成一个空气分配系统，其中至少一个管道被阀门和另一个管道连续流动，过量的空气通过涡轮与气体混合在旋转涡轮迷宫式密封件附近的路径空气，以确保密封冷却，同时对旋转部件进行足够的加热，以达到密封件的最小间隙。

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