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1. 发明授权

US07870741B2 Turbine engine valve assembly and method of assembling the same 有权
标题翻译：涡轮发动机气门组件及其组装方法
公开(公告)号：US07870741B2
公开(公告)日：2011-01-18
申请号：US11753907
申请日：2007-05-25
申请人： Donald Michael Corsmeier , David Lynn Dawson
发明人： Donald Michael Corsmeier , David Lynn Dawson
IPC分类号： F02K1/00
CPC分类号： F02C9/18 , F02K3/075 , F02K3/10 , F05D2260/50 , Y10T29/4932
摘要： A method of assembling a crank assembly for a turbine engine. The turbine engine includes a valve assembly including an outer fairing and an inner fairing coupled to the outer fairing with a strut. The valve assembly further includes an annular slide valve coupled between the inner and outer fairings. The valve assembly is positioned within a duct having a radially outer duct wall and a radially inner duct wall. The method includes coupling a first arm of a crank assembly to the annular slide valve, and coupling a second arm of the crank assembly to the outer fairing such that the crank assembly controls movement of the annular slide valve and for moving the outer and inner fairings between a first operational position and a second operational position to facilitate regulating an amount of airflow channeled through the turbine engine.
摘要翻译：一种组装用于涡轮发动机的曲柄组件的方法。涡轮发动机包括阀组件，该阀组件包括外部整流罩和与支撑件连接到外部整流罩的内部整流罩。阀组件还包括联接在内部和外部整流罩之间的环形滑阀。阀组件位于具有径向外管道壁和径向内管道壁的管道内。该方法包括将曲柄组件的第一臂联接到环形滑阀，以及将曲柄组件的第二臂联接到外整流罩，使得曲柄组件控制环形滑阀的运动并且用于移动外部和内部整流罩在第一操作位置和第二操作位置之间，以便于调节通过涡轮发动机引导的气流的量。

2. 发明授权

US07837436B2 Method and apparatus for regulating fluid flow through a turbine engine 有权
标题翻译：用于调节通过涡轮发动机的流体流动的方法和装置
公开(公告)号：US07837436B2
公开(公告)日：2010-11-23
申请号：US11753929
申请日：2007-05-25
申请人： Donald Michael Corsmeier , David Andrew Perveiler , George Joseph Johnson
发明人： Donald Michael Corsmeier , David Andrew Perveiler , George Joseph Johnson
IPC分类号： F01D17/00
CPC分类号： F02K3/075 , F02K3/077
摘要： A method for regulating fluid flow through a gas turbine engine is provided. The method includes coupling an outer fairing to a radially outer duct wall and coupling an inner fairing to a radially inner duct wall. An annular valve is coupled between the radially outer and the radially inner duct walls such that an outer bypass flow area is at least partially defined between the annular valve and the outer fairing, and such that an inner bypass flow area is at least partially defined between the annular valve and the inner fairing. The annular valve is selectively positioned between a first operational position and a second operational position, such that at least one of the outer bypass and the inner bypass flow areas is varied during a transition from a first turbine operation to a second turbine operation.
摘要翻译：提供了一种用于调节通过燃气涡轮发动机的流体流动的方法。该方法包括将外部整流罩联接到径向外部管道壁并将内部整流罩联接到径向内部管道壁。环形阀联接在径向外部管道壁和径向内部管道壁之间，使得外部旁路流动区域至少部分地限定在环形阀门和外部整流罩之间，并且使得内部旁路流动区域至少部分地限定在环形阀和内部整流罩。环形阀被选择性地定位在第一操作位置和第二操作位置之间，使得在从第一涡轮机操作到第二涡轮机操作的转变期间，外部旁路和内部旁路流动区域中的至少一个是变化的。

3. 发明申请

US20090035127A1 VALVE ASSEMBLY FOR A GAS TURBINE ENGINE 有权
标题翻译：气体涡轮发动机用阀组件
公开(公告)号：US20090035127A1
公开(公告)日：2009-02-05
申请号：US12202514
申请日：2008-09-02
申请人： Donald Michael Corsmeier
发明人： Donald Michael Corsmeier
IPC分类号： F02C9/18 , F02K3/02
CPC分类号： F02K1/386 , F01D17/143 , F02K3/10 , Y02T50/672
摘要： A method for channeling compressed air to a gas turbine engine augmentor is provided. The method includes coupling an annular slide valve to a gas turbine engine separation liner, coupling a valve seat to a gas turbine engine diffuser such that an airflow passage is defined between the annular slide valve and the valve seat, and channeling compressed air to the annular slide valve to facilitate regulating the quantity of fan bypass air channeled to the gas turbine engine augmentor.
摘要翻译：提供了一种用于将压缩空气引导到燃气涡轮发动机增压器的方法。该方法包括将环形滑阀联接到燃气涡轮发动机分离衬套，将阀座联接到燃气涡轮发动机扩散器，使得在环形滑阀和阀座之间限定气流通道，并将压缩空气引导到环形滑阀，以便调节通向燃气涡轮发动机增压器的风扇旁路空气的数量。

4. 发明授权

US08893382B2 Combustion system and method of assembling the same 有权
标题翻译：燃烧系统及其组装方法
公开(公告)号：US08893382B2
公开(公告)日：2014-11-25
申请号：US13249868
申请日：2011-09-30
申请人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe , Donald Scott Yeager , Mark Willard Marusko , Michael Joseph Zerbe
发明人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe , Donald Scott Yeager , Mark Willard Marusko , Michael Joseph Zerbe
IPC分类号： B23P17/00 , F23R3/50 , F23R3/00 , F23R3/60
CPC分类号： F23R3/50 , F23R3/002 , F23R3/60 , Y02E20/16 , Y10T29/49229 , Y10T29/4932
摘要： A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.
摘要翻译：一种组装燃气涡轮发动机的燃烧系统的方法包括提供燃烧室框架，内壳结构和外壳结构。该方法还包括将燃烧室框架安装在内壳结构和外壳结构之间，使得燃烧室框架联接到内壳结构和外壳结构。

5. 发明申请

US20130081270A1 COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME 有权
标题翻译：燃烧系统及其组装方法
公开(公告)号：US20130081270A1
公开(公告)日：2013-04-04
申请号：US13249868
申请日：2011-09-30
申请人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe
发明人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe
IPC分类号： B23P17/00 , F02C3/14
CPC分类号： F23R3/50 , F23R3/002 , F23R3/60 , Y02E20/16 , Y10T29/49229 , Y10T29/4932
摘要： A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.
摘要翻译：一种组装燃气涡轮发动机的燃烧系统的方法包括提供燃烧室框架，内壳结构和外壳结构。该方法还包括将燃烧室框架安装在内壳结构和外壳结构之间，使得燃烧室框架联接到内壳结构和外壳结构。

6. 发明授权

US07818957B2 Valve assembly for a gas turbine engine 有权
标题翻译：燃气涡轮发动机的阀组件
公开(公告)号：US07818957B2
公开(公告)日：2010-10-26
申请号：US12202514
申请日：2008-09-02
申请人： Donald Michael Corsmeier
发明人： Donald Michael Corsmeier
IPC分类号： B63H11/00
CPC分类号： F02K1/386 , F01D17/143 , F02K3/10 , Y02T50/672
摘要： A method for channeling compressed air to a gas turbine engine augmentor is provided. The method includes coupling an annular slide valve to a gas turbine engine separation liner, coupling a valve seat to a gas turbine engine diffuser such that an airflow passage is defined between the annular slide valve and the valve seat, and channeling compressed air to the annular slide valve to facilitate regulating the quantity of fan bypass air channeled to the gas turbine engine augmentor.
摘要翻译：提供了一种用于将压缩空气引导到燃气涡轮发动机增压器的方法。该方法包括将环形滑阀联接到燃气涡轮发动机分离衬套，将阀座联接到燃气涡轮发动机扩散器，使得在环形滑阀和阀座之间限定气流通道，并将压缩空气引导到环形滑阀，以便调节通向燃气涡轮发动机增压器的风扇旁路空气的数量。

7. 发明申请

US20090016874A1 METHOD AND APPARATUS FOR REGULATING FLUID FLOW THROUGH A TURBINE ENGINE 有权
标题翻译：通过涡轮发动机调节流体流量的方法和装置
公开(公告)号：US20090016874A1
公开(公告)日：2009-01-15
申请号：US11753929
申请日：2007-05-25
申请人： Donald Michael Corsmeier , David Andrew Perveiler , George Joseph Johnson
发明人： Donald Michael Corsmeier , David Andrew Perveiler , George Joseph Johnson
IPC分类号： F02C9/18
CPC分类号： F02K3/075 , F02K3/077
摘要： A method for regulating fluid flow through a gas turbine engine is provided. The method includes coupling an outer fairing to a radially outer duct wall and coupling an inner fairing to a radially inner duct wall. An annular valve is coupled between the radially outer and the radially inner duct walls such that an outer bypass flow area is at least partially defined between the annular valve and the outer fairing, and such that an inner bypass flow area is at least partially defined between the annular valve and the inner fairing. The annular valve is selectively positioned between a first operational position and a second operational position, such that at least one of the outer bypass and the inner bypass flow areas is varied during a transition from a first turbine operation to a second turbine operation.
摘要翻译：提供了一种用于调节通过燃气涡轮发动机的流体流动的方法。该方法包括将外部整流罩联接到径向外部管道壁并将内部整流罩联接到径向内部管道壁。环形阀联接在径向外部管道壁和径向内部管道壁之间，使得外部旁路流动区域至少部分地限定在环形阀门和外部整流罩之间，并且使得内部旁路流动区域至少部分地限定在环形阀和内部整流罩。环形阀被选择性地定位在第一操作位置和第二操作位置之间，使得在从第一涡轮机操作到第二涡轮机操作的转变期间，外部旁路和内部旁路流动区域中的至少一个是变化的。

8. 发明授权

US07475532B2 Valve assembly for a gas turbine engine 有权
标题翻译：燃气涡轮发动机的阀组件
公开(公告)号：US07475532B2
公开(公告)日：2009-01-13
申请号：US11214108
申请日：2005-08-29
申请人： Donald Michael Corsmeier
发明人： Donald Michael Corsmeier
IPC分类号： F02K3/02 , F02K3/10
CPC分类号： F02K1/386 , F01D17/143 , F02K3/10 , Y02T50/672
摘要： A method for channeling compressed air to a gas turbine engine augmentor is provided. The method includes coupling an annular slide valve to a gas turbine engine separation liner, coupling a valve seat to a gas turbine engine diffuser such that an airflow passage is defined between the annular slide valve and the valve seat, and channeling compressed air to the annular slide valve to facilitate regulating the quantity of fan bypass air channeled to the gas turbine engine augmentor.
摘要翻译：提供了一种用于将压缩空气引导到燃气涡轮发动机增压器的方法。该方法包括将环形滑阀联接到燃气涡轮发动机分离衬套，将阀座联接到燃气涡轮发动机扩散器，使得在环形滑阀和阀座之间限定气流通道，并将压缩空气引导到环形滑阀，以便调节通向燃气涡轮发动机增压器的风扇旁路空气的数量。

9. 发明授权

US08943835B2 Gas turbine engine combustor with CMC heat shield and methods therefor 有权
标题翻译：燃气轮机发动机燃烧器采用CMC隔热罩及其方法
公开(公告)号：US08943835B2
公开(公告)日：2015-02-03
申请号：US12776535
申请日：2010-05-10
申请人： Donald Michael Corsmeier , Mark Eugene Noe , Michael Todd Radwanski , Oliver Roghe , Jessica Licardi Subit , Ming Xie
发明人： Donald Michael Corsmeier , Mark Eugene Noe , Michael Todd Radwanski , Oliver Roghe , Jessica Licardi Subit , Ming Xie
IPC分类号： F02C1/00 , F23R3/00
CPC分类号： F23R3/42 , F23R3/002 , F23R3/007 , F23R2900/00017 , Y10T29/4932 , Y10T29/49826
摘要： A combustor for a gas turbine engine is disclosed. The combustor is described as comprising a dome plate coupled to a liner thereof, with at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate. Also described is a method for assembling a combustor for a gas turbine engine, including releasing a metal alloy heat shield from a dome plate and providing a ceramic matrix composite heat shield as replacement.
摘要翻译：公开了一种用于燃气涡轮发动机的燃烧器。燃烧器被描述为包括联接到其衬垫的圆顶板，至少一个隔热罩包括耦合在圆顶板的后端的陶瓷基体复合体。还描述了一种用于组装用于燃气涡轮发动机的燃烧器的方法，包括从圆顶板释放金属合金隔热罩并提供陶瓷基复合隔热罩作为替代物。

10. 发明申请

US20110271684A1 GAS TURBINE ENGINE COMBUSTOR WITH CMC HEAT SHIELD AND METHODS THEREFOR 有权
标题翻译：燃气涡轮发动机燃烧器与CMC热风及其方法
公开(公告)号：US20110271684A1
公开(公告)日：2011-11-10
申请号：US12776535
申请日：2010-05-10
申请人： Donald Michael CORSMEIER , Mark Eugene Noe , Michael Todd Radwanski , Oliver Roghe , Jessica Licardi Subit , Ming Xie
发明人： Donald Michael CORSMEIER , Mark Eugene Noe , Michael Todd Radwanski , Oliver Roghe , Jessica Licardi Subit , Ming Xie
IPC分类号： F02C3/14 , B23P11/00
CPC分类号： F23R3/42 , F23R3/002 , F23R3/007 , F23R2900/00017 , Y10T29/4932 , Y10T29/49826
摘要： A combustor for a gas turbine engine is disclosed. The combustor is described as comprising a dome plate coupled to a liner thereof, with at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate. Also described is a method for assembling a combustor for a gas turbine engine, including releasing a metal alloy heat shield from a dome plate and providing a ceramic matrix composite heat shield as replacement.
摘要翻译：公开了一种用于燃气涡轮发动机的燃烧器。燃烧器被描述为包括联接到其衬垫的圆顶板，至少一个隔热罩包括耦合在圆顶板的后端的陶瓷基体复合体。还描述了一种用于组装用于燃气涡轮发动机的燃烧器的方法，包括从圆顶板释放金属合金隔热罩并提供陶瓷基复合隔热罩作为替代物。

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