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1. 发明授权

US5634766A Turbine stator vane segments having combined air and steam cooling circuits 失效
标题翻译：具有组合的空气和蒸汽冷却回路的涡轮定子叶片段
公开(公告)号：US5634766A
公开(公告)日：1997-06-03
申请号：US414697
申请日：1995-03-31
申请人： Francisco J. Cunha , David A. DeAngelis , Theresa A. Brown , Sanjay Chopra , Victor H. S. Correia , Daniel R. Predmore
发明人： Francisco J. Cunha , David A. DeAngelis , Theresa A. Brown , Sanjay Chopra , Victor H. S. Correia , Daniel R. Predmore
IPC分类号： F01D9/02 , F01D5/18 , F01D9/04 , F01D11/00 , F02C7/16 , F01D9/06
CPC分类号： F01D5/189 , F01D11/005 , F01D5/187 , F01D5/188 , F05D2240/10 , F05D2240/81 , F05D2260/201 , F05D2260/2212 , F05D2260/2322 , Y02T50/67 , Y02T50/676
摘要： Turbine stator vane segments have inner and outer walls with vanes extending therebetween. The inner and outer walls are compartmentalized and have impingement plates. Steam flowing into the outer wall passes through the impingement plate for impingement cooling of the outer wall surface. The spent impingement steam flows into cavities of the vane having inserts for impingement cooling the walls of the vane. The steam passes into the inner wall and through the impingement plate for impingement cooling of the inner wall surface and for return through return cavities having inserts for impingement cooling of the vane surfaces. The trailing edge is air-cooled.
摘要翻译：涡轮机定子叶片段具有内壁和外壁，叶片间延伸有叶片。内壁和外壁分隔开并具有冲击板。流入外壁的蒸汽通过冲击板，用于冲击冷却外壁表面。废冲击蒸汽流入具有用于冲击冷却叶片壁的插入件的叶片的空腔中。蒸汽进入内壁并通过冲击板，用于内壁表面的冲击冷却，并通过具有用于叶片表面的冲击冷却的插入件的返回腔返回。后缘是风冷的。

2. 外观设计

USD414031S Handheld fan 失效
公开(公告)号：USD414031S
公开(公告)日：1999-09-21
申请号：US93762
申请日：1998-09-17
申请人： Theresa A Brown
设计人： Theresa A Brown

3. 发明授权

US5743708A Turbine stator vane segments having combined air and steam cooling circuits 失效
标题翻译：具有组合的空气和蒸汽冷却回路的涡轮定子叶片段
公开(公告)号：US5743708A
公开(公告)日：1998-04-28
申请号：US674476
申请日：1996-07-02
申请人： Francisco J. Cunha , David A. DeAngelis , Theresa A. Brown , Sanjay Chopra , Victor H. S. Correia , Daniel R. Predmore
发明人： Francisco J. Cunha , David A. DeAngelis , Theresa A. Brown , Sanjay Chopra , Victor H. S. Correia , Daniel R. Predmore
IPC分类号： F01D9/02 , F01D5/18 , F01D9/04 , F01D11/00 , F02C7/16 , F01D9/06
CPC分类号： F01D5/189 , F01D11/005 , F01D5/187 , F01D5/188 , F05D2240/10 , F05D2240/81 , F05D2260/201 , F05D2260/2212 , F05D2260/2322 , Y02T50/67 , Y02T50/676
摘要： Turbine stator vane segments have inner and outer walls with vanes extending therebetween. The inner and outer walls are compartmentalized and have impingement plates. Steam flowing into the outer wall passes through the impingement plate for impingement cooling of the outer wall surface. The spent impingement steam flows into cavities of the vane having inserts for impingement cooling the walls of the vane. The steam passes into the inner wall and through the impingement plate for impingement cooling of the inner wall surface and for return through return cavities having inserts for impingement cooling of the vane surfaces. The trailing edge is air-cooled.
摘要翻译：涡轮机定子叶片段具有内壁和外壁，叶片间延伸有叶片。内壁和外壁分隔开并具有冲击板。流入外壁的蒸汽通过冲击板，用于冲击冷却外壁表面。废冲击蒸汽流入具有用于冲击冷却叶片壁的插入件的叶片的空腔中。蒸汽进入内壁并通过冲击板，用于内壁表面的冲击冷却，并通过具有用于叶片表面的冲击冷却的插入件的返回腔返回。后缘是风冷的。

4. 发明授权

US5713722A Turbine nozzle and related casting method for optimal fillet wall thickness control 失效
标题翻译：涡轮喷嘴和相关铸造方法，用于最佳的圆角壁厚控制
公开(公告)号：US5713722A
公开(公告)日：1998-02-03
申请号：US667157
申请日：1996-06-20
申请人： Victor H. Correia , Theresa A. Brown , Daniel R. Predmore
发明人： Victor H. Correia , Theresa A. Brown , Daniel R. Predmore
IPC分类号： F01D9/02 , B22C7/02 , B22C9/04 , B22C9/22 , F01D9/04 , F01D5/14
CPC分类号： B22C7/02 , B22C9/04
摘要： In a method of investment casting a turbine nozzle which includes an outer band, an inner band and an airfoil section extending between the inner and outer bands, an improvement including shaping a temporary wax form, and external shell and internal core components used in casting such that during pouring of molten metal into a space created by removal of the wax form, shell material lies on opposite sides of an outer fillet connecting the outer band to the airfoil section. The resulting gas turbine nozzle includes first and second horizontally oriented ribs extending about interior peripheries of the airfoil section vertically adjacent the outer and inner band fillets.
摘要翻译：在一种熔模铸造方法中，包括外带，内带和在内带和外带之间延伸的翼型部分的涡轮喷嘴，包括成型临时蜡形的改进，以及用于铸造的外壳和内芯部件在将熔融金属浇注到通过除去蜡形而产生的空间中时，外壳材料位于将外带连接到翼型部的外圆角的相对侧上。所得到的燃气涡轮喷嘴包括第一和第二水平定向的肋，所述第一和第二水平定向的肋沿着与外带和内带鱼片垂直相邻的翼型部的内周延伸。

5. 发明申请

US20130323031A1 TURBINE DAMPER 有权
标题翻译：涡轮阻尼器
公开(公告)号：US20130323031A1
公开(公告)日：2013-12-05
申请号：US13485789
申请日：2012-05-31
申请人： Qingxuan Michael Zhang , Theresa A. Brown , Leslie John Faulder
发明人： Qingxuan Michael Zhang , Theresa A. Brown , Leslie John Faulder
IPC分类号： F01D11/00 , B23P15/04 , F16J15/02 , F01D11/08
CPC分类号： F01D5/22 , F01D5/3015 , Y10T29/4932
摘要： A damper for a turbine rotor assembly of a gas turbine engine is disclosed. The damper includes a width dimension, a height dimension, and a length dimension and a forward plate. The damper further includes an aft plate that is larger than the forward plate along the width and height dimension and having a lower portion including two legs extending in the height dimension. The damper also includes a longitudinal structure extending in the length dimension and connecting the forward plate and the aft plate.
摘要翻译：公开了一种用于燃气涡轮发动机的涡轮转子组件的阻尼器。阻尼器包括宽度尺寸，高度尺寸和长度尺寸以及前板。阻尼器还包括沿着宽度和高度尺寸大于前板的后板，并且具有包括在高度尺寸上延伸的两个腿的下部。阻尼器还包括在长度尺寸上延伸并连接前板和后板的纵向结构。

6. 发明授权

US06499739B1 Restaurant theme board game 失效
标题翻译：餐厅主题板游戏
公开(公告)号：US06499739B1
公开(公告)日：2002-12-31
申请号：US09716534
申请日：2000-11-20
申请人： Theresa A. Brown
发明人： Theresa A. Brown
IPC分类号： A63F300
CPC分类号： A63F3/0478 , A63F9/18
摘要： A restaurant theme board game and a method of play, includes a playing surface; a playing piece for each player, and a course to be traversed by the playing pieces. The course includes waitress stations, each player's playing piece occupying a respective station. Each waitress station includes tables wherein each player required to traverse the tables of its waitress station five times to complete five levels. Each level must be traversed within a predetermined period of time. Question cards must be answered by each player during that player's turn in order for the player's playing piece to proceed along tables of the player's station. Money awards are given for correctly answering the questions. The first player who completely traverses the tables for each level within the predetermined time period and accumulates more rewards than any other player, wins the game.
摘要翻译：餐厅主题板游戏和游戏方法，包括游戏表面; 每个玩家的玩具，以及玩棋子穿过的路线。课程包括女服务员站，每个玩家的玩具占据相应的车站。每个女服务员站包括表，其中每个玩家需要遍历其女服务台的桌面五次以完成五个级别。必须在预定的时间段内遍历每个级别。玩家转牌时必须由每个玩家回答问题牌，以便玩家的玩家可以在玩家电台的桌子上进行。给予正确回答问题的奖金。在预定时间段内完成每个级别的桌子横向移动并且比任何其他玩家积累更多奖励的第一名玩家赢得比赛。

7. 发明授权

US5391052A Impingement cooling and cooling medium retrieval system for turbine shrouds and methods of operation 失效
标题翻译：用于涡轮罩的冲击冷却和冷却介质回收系统及其操作方法
公开(公告)号：US5391052A
公开(公告)日：1995-02-21
申请号：US152363
申请日：1993-11-16
申请人： Victor H. Correia , Theresa A. Brown , R. Paul Chiu
发明人： Victor H. Correia , Theresa A. Brown , R. Paul Chiu
IPC分类号： F01D11/10 , F01D11/24 , F01D25/12
CPC分类号： F01D11/10 , F01D11/24 , F05D2260/201 , F05D2260/2322
摘要： The steam impingement cooling and retrieval system for turbine shrouds includes a plurality of circumferentially spaced housings about a turbine shroud, each housing being divided by an impingement plate defining first and second chambers on opposite sides of the housing. Steam supplied into a first chamber passes through a plurality of apertures formed in the impingement plate into the second chamber for impingement cooling of the shroud surface forming the opposite wall of the housing. Post-impingement steam passes from the compartment into a manifold for flow through and exhaust passage. In one form, a plurality of compartments are formed in the impingement plate. A first set of the plurality of compartments include through apertures for delivering steam from the first chamber into the second chamber. The second set of compartments communicates only with the second chamber and an exhaust passage whereby post-impingement steam passes from the second chamber through apertures of the impingement plate into the second set of compartments for flow to a manifold at the end wall of the housing for delivery to the exhaust passage.
摘要翻译：用于涡轮机护罩的蒸汽冲击冷却和回收系统包括围绕涡轮机护罩的多个周向间隔开的壳体，每个壳体由限定在壳体的相对侧上的第一和第二腔室的冲击板分隔。供应到第一室的蒸汽穿过形成在冲击板中的多个孔进入第二室，用于冲击冷却形成壳体的相对壁的护罩表面。后冲击蒸汽从隔室进入歧管以流过和排出通道。在一种形式中，在冲击板中形成多个隔室。多个隔室的第一组包括用于将蒸汽从第一室输送到第二室中的通孔。第二组隔间仅与第二腔室和排气通道连通，由此后冲击蒸汽从第二腔室通过冲击板的孔通入第二组隔室，以流动到壳体的端壁处的歧管输送到排气通道。

8. 发明授权

US09650901B2 Turbine damper 有权
公开(公告)号：US09650901B2
公开(公告)日：2017-05-16
申请号：US13485789
申请日：2012-05-31
申请人： Qingxuan Michael Zhang , Theresa A. Brown , Leslie John Faulder
发明人： Qingxuan Michael Zhang , Theresa A. Brown , Leslie John Faulder
IPC分类号： F01D5/22 , F01D5/30
CPC分类号： F01D5/22 , F01D5/3015 , Y10T29/4932
摘要： A damper for a turbine rotor assembly of a gas turbine engine is disclosed. The damper includes a width dimension, a height dimension, and a length dimension and a forward plate. The damper further includes an aft plate that is larger than the forward plate along the width and height dimension and having a lower portion including two legs extending in the height dimension. The damper also includes a longitudinal structure extending in the length dimension and connecting the forward plate and the aft plate.

9. 发明授权

US06739839B1 First-stage high pressure turbine bucket airfoil 有权
标题翻译：第一级高压涡轮桶翼型
公开(公告)号：US06739839B1
公开(公告)日：2004-05-25
申请号：US10403696
申请日：2003-03-31
申请人： Theresa A. Brown , Majid Ahmadi , Eugene Clemens , Jacob C. Perry, II , Allyn K. Holiday , Richard A. Delehanty , Ariel Caesar Prepena Jacala
发明人： Theresa A. Brown , Majid Ahmadi , Eugene Clemens , Jacob C. Perry, II , Allyn K. Holiday , Richard A. Delehanty , Ariel Caesar Prepena Jacala
IPC分类号： F01D514
CPC分类号： F01D5/141 , F05D2220/76 , F05D2240/301 , Y10S416/02
摘要： The first-stage buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein Z is a perpendicular distance from a plane normal to a radius of the turbine centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at the radially innermost aerodynamic section of the airfoil and X and Y are coordinates defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled as a function of the same constant or number to provide a scaled-up or scaled-down airfoil section for the bucket.
摘要翻译：第一级铲斗具有基本上符合表I中列出的X，Y和Z的笛卡尔坐标值的翼型，其中Z是与垂直于涡轮机中心线的半径并且包含X和Y值的平面的垂直距离其中Z值在翼型的径向最内部空气动力学部分的X，Y平面处开始为零，X和Y是在每个距离Z处限定翼型轮廓的坐标.X，Y和Z值可以被缩放为函数相同的常数或数量，以提供用于铲斗的放大或缩小的翼型部分。

10. 发明授权

US5662160A Turbine nozzle and related casting method for optimal fillet wall thickness control 失效
标题翻译：涡轮喷嘴和相关铸造方法，用于最佳的圆角壁厚控制
公开(公告)号：US5662160A
公开(公告)日：1997-09-02
申请号：US542001
申请日：1995-10-12
申请人： Victor H. Correia , Theresa A. Brown , Daniel R. Predmore
发明人： Victor H. Correia , Theresa A. Brown , Daniel R. Predmore
IPC分类号： F01D9/02 , B22C7/02 , B22C9/04 , B22C9/22 , F01D9/04 , B22C9/00 , B22C7/00 , B22C9/02
CPC分类号： B22C7/02 , B22C9/04
摘要： In a method of investment casting a turbine nozzle which includes an outer band, an inner band and an airfoil section extending between the inner and outer bands, an improvement including shaping a temporary wax form, and external shell and internal core components used in casting such that during pouring of molten metal into a space created by removal of the wax form, shell material lies on opposite sides of an outer fillet connecting the outer band to the airfoil section. The resulting gas turbine nozzle includes first and second horizontally oriented ribs extending about interior peripheries of the airfoil section vertically adjacent the outer and inner band fillets.
摘要翻译：在一种熔模铸造方法中，包括外带，内带和在内带和外带之间延伸的翼型部分的涡轮喷嘴，包括成型临时蜡形的改进，以及用于铸造的外壳和内芯部件在将熔融金属浇注到通过除去蜡形而产生的空间中时，外壳材料位于将外带连接到翼型部的外圆角的相对侧上。所得到的燃气涡轮喷嘴包括第一和第二水平定向的肋，所述第一和第二水平定向的肋沿着与外带和内带鱼片垂直相邻的翼型部分的内周延伸。

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