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1. 发明授权

US06435812B1 Bore tube assembly for steam cooling a turbine rotor 失效
标题翻译：用于蒸汽冷却涡轮转子的孔管组件
公开(公告)号：US06435812B1
公开(公告)日：2002-08-20
申请号：US09566726
申请日：2000-05-09
申请人： Thomas Daniel DeStefano , Ian David Wilson
发明人： Thomas Daniel DeStefano , Ian David Wilson
IPC分类号： F01D514
CPC分类号： F01D5/185 , Y02T50/676
摘要： An axial bore tube assembly for a turbine is provided to supply cooling steam to hot gas components of the turbine wheels and return the spent cooling steam. A pair of inner and outer tubes define a steam supply passage concentric about an inner return passage. The forward ends of the tubes communicate with an end cap assembly having sets of peripheral holes communicating with first and second sets of radial tubes whereby cooling steam from the concentric passage is supplied through the end cap holes to radial tubes for cooling the buckets and return steam from the buckets is provided through the second set of radial tubes through a second set of openings of the end cap into the coaxial return passage. A radial-to-axial flow transitioning device, including anti-swirling vanes is provided in the end cap. A strut ring adjacent the aft end of the bore tube assembly permits axial and radial thermal expansion of the inner tube relative to the outer tube.
摘要翻译：提供了一种用于涡轮机的轴向孔管组件，以将冷却蒸汽供应到涡轮机叶轮的热气体部件并返回废冷却蒸汽。一对内管和外管限定了围绕内返回通道同心的蒸汽供应通道。管的前端与具有与第一和第二组径向管连通的一组周边孔的端盖组件连通，从而将来自同心通道的冷却蒸汽通过端盖孔供应到用于冷却桶和回流的径向管通过第二组径向管通过端帽的第二组开口提供到同轴返回通道中。在端盖中设置包括防旋转叶片的径向 - 轴向流动过渡装置。邻近钻孔管组件的后端的支柱环允许内管相对于外管的轴向和径向热膨胀。

2. 发明授权

US08267649B2 Coupling for rotary components 有权
标题翻译：旋转部件联轴器
公开(公告)号：US08267649B2
公开(公告)日：2012-09-18
申请号：US12467213
申请日：2009-05-15
申请人： Ian David Wilson
发明人： Ian David Wilson
IPC分类号： F01D25/00 , F16D11/04
CPC分类号： F01D5/066 , F01D5/026 , F05B2220/32 , F05D2220/31 , F05D2220/32 , F05D2260/402 , F05D2260/403 , F16D7/024
摘要： A system is disclosed that includes a turbine engine having a first rotary component having a first annular coupling disposed about a rotational axis of the engine. The first annular coupling has an axially converging surface relative to the rotational axis. The system also includes a second rotary component having a second annular coupling disposed about the rotational axis of the turbine engine, wherein the second annular coupling comprises an axially diverging surface such that the axially converging surface of the first annular coupling mates with the axially diverging surface.
摘要翻译：公开了一种包括具有第一旋转部件的涡轮发动机的系统，所述第一旋转部件具有绕发动机的旋转轴线设置的第一环形联轴器。第一环形联轴器具有相对于旋转轴线的轴向会聚表面。该系统还包括具有围绕涡轮发动机的旋转轴线设置的第二环形联接件的第二旋转部件，其中第二环形联接器包括轴向发散表面，使得第一环形联轴器的轴向会聚表面与轴向发散表面。

3. 发明申请

US20120027584A1 TURBINE SEAL SYSTEM 有权
标题翻译：涡轮密封系统
公开(公告)号：US20120027584A1
公开(公告)日：2012-02-02
申请号：US12848906
申请日：2010-08-02
申请人： Josef Scott Cummins , Ian David Wilson
发明人： Josef Scott Cummins , Ian David Wilson
IPC分类号： F01D25/00 , F01D5/08
CPC分类号： F01D11/003 , F01D11/001 , Y02T50/671
摘要： In accordance with one embodiment, a system includes a multi-stage turbine including a first turbine stage including a first wheel having multiple first slots spaced circumferentially about the first wheel, and multiple first blade segments each coupled to at least one of the multiple first slots. The multi-stage turbine also includes a second turbine stage including a second wheel having multiple second slots spaced circumferentially about the second wheel, and multiple second blade segments each coupled to at least one of the multiple second slots. The multi-stage turbine further includes a one-piece interstage seal extending axially between the first and second turbine stages, wherein the one-piece interstage seal comprises a first radial support coupled to the first wheel and a second radial support coupled to the second wheel, and the one-piece interstage seal extends circumferentially across at least two of the multiple first slots or at least two of the multiple second slots.
摘要翻译：根据一个实施例，一种系统包括多级涡轮机，该多级涡轮机包括第一涡轮机级，该第一涡轮机级包括具有围绕第一车轮周向间隔开的多个第一槽的第一轮和多个第一叶片段，每个第一叶片段连接至多个第一槽。多级涡轮机还包括第二涡轮级，其包括具有围绕第二轮周向间隔开的多个第二狭槽的第二轮，以及多个第二叶片段，每个第二叶片段联接到多个第二狭槽中的至少一个。多级涡轮机还包括在第一和第二涡轮级之间轴向延伸的单件级间密封件，其中单件级间密封件包括联接到第一轮的第一径向支撑件和联接到第二轮子的第二径向支撑件并且所述单件级间密封件沿所述多个第一槽中的至少两个或所述多个第二槽中的至少两个周向延伸。

4. 发明申请

US20100189551A1 Systems and Methods of Reducing Heat Loss from a Gas Turbine During Shutdown 有权
标题翻译：关闭期间降低燃气轮机热损失的系统和方法
公开(公告)号：US20100189551A1
公开(公告)日：2010-07-29
申请号：US12362086
申请日：2009-01-29
申请人： Henry G. Ballard, JR. , Ian David Wilson , Stephen Christopher Chieco , Andrew Ray Kneeland , Bradley James Miller , Kenneth Damon Black , Raymond Goetze
发明人： Henry G. Ballard, JR. , Ian David Wilson , Stephen Christopher Chieco , Andrew Ray Kneeland , Bradley James Miller , Kenneth Damon Black , Raymond Goetze
IPC分类号： F02C7/00
CPC分类号： F01D21/06 , F01D11/24 , F01D21/12
摘要： A method operates a gas turbine that includes a compressor section, a turbine section and an extraction cooling system. The method includes monitoring an operation of the gas turbine, directing a cooling air flow through the extraction cooling system from the compressor section to the turbine section in response to normal operation of the gas turbine, and directing a warming air flow through the extraction cooling system to the compressor section and the turbine section in response to shutdown of the gas turbine.
摘要翻译：一种方法操作包括压缩机部分，涡轮部分和提取冷却系统的燃气涡轮机。该方法包括：监测燃气轮机的运行，响应于燃气轮机的正常运行，将冷却空气流通过抽出冷却系统从压缩机部分引导到涡轮部分，并且引导加热空气流通过抽出冷却系统响应于燃气轮机的关闭而连接到压缩机部分和涡轮部分。

5. 发明授权

US08511976B2 Turbine seal system 有权
标题翻译：涡轮密封系统
公开(公告)号：US08511976B2
公开(公告)日：2013-08-20
申请号：US12848906
申请日：2010-08-02
申请人： Josef Scott Cummins , Ian David Wilson
发明人： Josef Scott Cummins , Ian David Wilson
IPC分类号： F01D11/02 , F01D5/06
CPC分类号： F01D11/003 , F01D11/001 , Y02T50/671
摘要： In accordance with one embodiment, a system includes a multi-stage turbine including a first turbine stage including a first wheel having multiple first slots spaced circumferentially about the first wheel, and multiple first blade segments each coupled to at least one of the multiple first slots. The multi-stage turbine also includes a second turbine stage including a second wheel having multiple second slots spaced circumferentially about the second wheel, and multiple second blade segments each coupled to at least one of the multiple second slots. The multi-stage turbine further includes a one-piece interstage seal extending axially between the first and second turbine stages, wherein the one-piece interstage seal comprises a first radial support coupled to the first wheel and a second radial support coupled to the second wheel, and the one-piece interstage seal extends circumferentially across at least two of the multiple first slots or at least two of the multiple second slots.
摘要翻译：根据一个实施例，一种系统包括多级涡轮机，该多级涡轮机包括第一涡轮机级，该第一涡轮机级包括具有围绕第一车轮周向间隔开的多个第一槽的第一轮和多个第一叶片段，每个第一叶片段连接至多个第一槽。多级涡轮机还包括第二涡轮级，其包括具有围绕第二轮周向间隔开的多个第二狭槽的第二轮，以及多个第二叶片段，每个第二叶片段联接到多个第二狭槽中的至少一个。多级涡轮机还包括在第一和第二涡轮级之间轴向延伸的单件级间密封件，其中单件级间密封件包括联接到第一轮的第一径向支撑件和联接到第二轮子的第二径向支撑件并且所述单件级间密封件沿所述多个第一槽中的至少两个或所述多个第二槽中的至少两个周向延伸。

6. 发明授权

US08061971B2 Apparatus and method for cooling a turbine 有权
标题翻译：用于冷却涡轮机的装置和方法
公开(公告)号：US08061971B2
公开(公告)日：2011-11-22
申请号：US12209832
申请日：2008-09-12
申请人： Eric Roush , Mark W. Flanagan , Ian David Wilson , George Frey , John Raymond Hess
发明人： Eric Roush , Mark W. Flanagan , Ian David Wilson , George Frey , John Raymond Hess
IPC分类号： F01D25/26
CPC分类号： F02C7/18 , F01D5/081 , F02C6/08
摘要： A cooling system for a turbine includes a blower configured to generate a cooling gas flow to be passed through a rotor cavity of the turbine; piping configured to deliver the cooling gas flow to the turbine; and at least one valve configured to control the cooling gas flow. The piping is operatively connected to the rotor of the turbine. A method of cooling a turbine includes generating a cooling gas flow with a blower to be passed through a rotor cavity of the turbine; and delivering the cooling gas flow to the turbine.
摘要翻译：一种用于涡轮机的冷却系统包括：鼓风机，其构造成产生要通过涡轮机的转子腔的冷却气流; 配置成将冷却气流输送到涡轮机的管道; 以及配置成控制冷却气流的至少一个阀。管道可操作地连接到涡轮机的转子。一种冷却涡轮机的方法包括：产生具有鼓风机的冷却气流，以通过涡轮机的转子腔; 并将冷却气流输送到涡轮。

7. 发明申请

US20100254805A1 GAS TURBINE INNER FLOWPATH COVERPIECE 有权
标题翻译：气体涡轮内流量罩
公开(公告)号：US20100254805A1
公开(公告)日：2010-10-07
申请号：US12417129
申请日：2009-04-02
申请人： Andres Jose Garcia-Crespo , Bradley Taylor Boyer , John Wesley Harris, JR. , Brian Denver Potter , Ian David Wilson
发明人： Andres Jose Garcia-Crespo , Bradley Taylor Boyer , John Wesley Harris, JR. , Brian Denver Potter , Ian David Wilson
IPC分类号： F01D11/00
CPC分类号： F01D11/001 , F05D2260/36
摘要： A gas turbine inner flow path cover piece for a gas turbine a first turbine wheel and a second turbine wheel is provided is provided. The gas turbine inner flow path cover piece can include a main body having an first surface and a second surface, side pieces disposed on the first surface of the main body and mating pairs disposed on the second surface of the main body.
摘要翻译：提供了一种用于燃气轮机的燃气轮机内部流路覆盖件，第一涡轮机叶轮和第二涡轮机叶轮。燃气轮机内流道盖件可以包括具有第一表面和第二表面的主体，设置在主体的第一表面上的侧片和设置在主体的第二表面上的配合对。

8. 发明授权

US06438837B1 Methods for aligning holes through wheels and spacers and stacking the wheels and spacers to form a turbine rotor 失效
标题翻译：用于通过轮和间隔件对准孔的方法，并且堆叠车轮和间隔件以形成涡轮转子
公开(公告)号：US06438837B1
公开(公告)日：2002-08-27
申请号：US09534048
申请日：2000-03-24
申请人： Robert Randolph Berry , Gene David Palmer , Ian David Wilson
发明人： Robert Randolph Berry , Gene David Palmer , Ian David Wilson
IPC分类号： B23P1500
CPC分类号： F01D5/06 , F01D5/066 , F05D2230/60 , F05D2230/64 , Y10T29/49316 , Y10T29/4932 , Y10T29/49895 , Y10T29/53961 , Y10T29/53978
摘要： A method of stacking a plurality of wheels and spacers forming a rotor for a turbine, the wheels and spacers having a plurality of circumferentially spaced, axially extending openings spaced radially from axes of the wheels and spacers including providing a support fixture having an axis and disposing a plurality of alignment rods about the fixture in circumferentially spaced relation to one another about and generally parallel to the axis. Each of the rods has a cross-section with a radial dimension less than a circumferential dimension. The method includes disposing the wheels and spacers on the support fixture with the alignment rods extending through the openings with clearances between the rods and margins of the openings being greater in a radial direction than in a circumferential direction.
摘要翻译：堆叠形成涡轮转子的多个车轮和间隔件的方法，所述车轮和间隔件具有与所述车轮和间隔件的轴线径向间隔开的多个周向间隔开的轴向延伸的开口，包括提供具有轴线的支撑夹具和设置围绕固定件的多个对准杆围绕并大致平行于轴线彼此周向间隔开。每个杆具有径向尺寸小于周向尺寸的横截面。该方法包括将车轮和间隔件设置在支撑固定装置上，其中对准杆延伸穿过开口，其中杆和间隙之间的间隙在径向方向上大于圆周方向。

9. 发明授权

US08210801B2 Systems and methods of reducing heat loss from a gas turbine during shutdown 有权
标题翻译：在关闭期间减少燃气轮机的热损失的系统和方法
公开(公告)号：US08210801B2
公开(公告)日：2012-07-03
申请号：US12362086
申请日：2009-01-29
申请人： Henry G. Ballard, Jr. , Ian David Wilson , Stephen Christopher Chieco , Andrew Ray Kneeland , Bradley James Miller , Kenneth David Black , Raymond Goetze
发明人： Henry G. Ballard, Jr. , Ian David Wilson , Stephen Christopher Chieco , Andrew Ray Kneeland , Bradley James Miller , Kenneth David Black , Raymond Goetze
IPC分类号： F02C6/08
CPC分类号： F01D21/06 , F01D11/24 , F01D21/12
摘要： A method operates a gas turbine that includes a compressor section, a turbine section and an extraction cooling system. The method includes monitoring an operation of the gas turbine, directing a cooling air flow through the extraction cooling system from the compressor section to the turbine section in response to normal operation of the gas turbine, and directing a warming air flow through the extraction cooling system to the compressor section and the turbine section in response to shutdown of the gas turbine.
摘要翻译：一种方法操作包括压缩机部分，涡轮部分和提取冷却系统的燃气涡轮机。该方法包括：监测燃气轮机的运行，响应于燃气轮机的正常运行，将冷却空气流通过抽出冷却系统从压缩机部分引导到涡轮部分，并且引导加热空气流通过抽出冷却系统响应于燃气轮机的关闭而连接到压缩机部分和涡轮部分。

10. 发明申请

US20120093639A1 APPARATUS AND METHOD FOR ALIGNING A TURBINE CASING 有权
标题翻译：用于调整涡轮机壳的装置和方法
公开(公告)号：US20120093639A1
公开(公告)日：2012-04-19
申请号：US12903466
申请日：2010-10-13
申请人： Henry Grady Ballard, JR. , Ian David Wilson , Martel Alexander McCallum , Stephen Christopher Chieco , Kenneth Damon Black , Christopher Paul Cox
发明人： Henry Grady Ballard, JR. , Ian David Wilson , Martel Alexander McCallum , Stephen Christopher Chieco , Kenneth Damon Black , Christopher Paul Cox
IPC分类号： F01D25/28 , B23P19/00
CPC分类号： F01D25/28 , F01D25/243 , F01D25/26 , F01D25/265 , F05D2230/51 , F05D2230/64 , F05D2250/713 , Y10T29/53
摘要： A casing includes an inner shell and an outer shell that surrounds the inner shell and comprises a plurality of inflection points. An annular flange is between the inner shell and the outer shell, and a plurality of joints attach the inner shell to the annular flange. A connector is between the annular flange and the outer shell at each of the plurality of inflection points. A method for assembling a casing includes joining a plurality of curved sections to one another to generally define an arcuate inner shell and surrounding the arcuate inner shell with an outer shell. The method further includes attaching the arcuate inner shell to an annular flange at first attachment points and connecting the annular flange to the outer shell at second attachment points spaced approximately equidistantly from the first attachment points.
摘要翻译：壳体包括围绕内壳并包括多个拐点的内壳和外壳。环形凸缘位于内壳和外壳之间，并且多个接头将内壳连接到环形凸缘。在多个拐点中的每一个处，连接器位于环形凸缘和外壳之间。一种用于组装壳体的方法包括将多个弯曲部分彼此连接以大致限定弓形内壳并且围绕弓形内壳与外壳。该方法还包括将弧形内壳附接到第一附接点处的环形凸缘，并且在与第一附接点大致等距离间隔开的第二附接点处将环形凸缘连接到外壳。

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