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1. 发明授权

US07121796B2 Nozzle-cooling insert assembly with cast-in rib sections 有权
标题翻译：喷嘴冷却插入组件，带有嵌入肋条
公开(公告)号：US07121796B2
公开(公告)日：2006-10-17
申请号：US10834925
申请日：2004-04-30
申请人： Steven S. Burdgick , Gary M. Itzel
发明人： Steven S. Burdgick , Gary M. Itzel
IPC分类号： F01D5/18
CPC分类号： F01D5/189 , Y02T50/676 , Y10T29/49343
摘要： A cooling insert/nozzle assembly for use in gas turbines or similar machinery includes a nozzle having inner and outer ribs with cast-in “T” sections and “L” sections, respectively, at the end of the ribs in which air flow enters the nozzle. The assembly further includes a cooling insert having a flexible end which is inserted between adjacent ribs having either the cast-in “T” or “L” sections.
摘要翻译：用于燃气轮机或类似机械的冷却插入件/喷嘴组件包括具有内肋和外肋的喷嘴，所述内肋和外肋分别在肋的末端分别具有“T”形截面和“L”形截面，其中气流进入喷嘴。组件还包括具有柔性端部的冷却插入件，所述柔性端部插入在具有铸入“T”或“L”部分的相邻肋之间。

2. 发明申请

US20100221108A1 Turbine nozzle assemblies 有权
标题翻译：涡轮喷嘴总成
公开(公告)号：US20100221108A1
公开(公告)日：2010-09-02
申请号：US11518708
申请日：2006-09-11
申请人： Steven S. Burdgick , Thomas W. Crall
发明人： Steven S. Burdgick , Thomas W. Crall
IPC分类号： F01D9/02
CPC分类号： F01D9/044 , F01D3/02 , F01D25/246 , F05D2220/31 , F05D2230/53 , F05D2230/642 , F05D2260/36
摘要： A nozzle assembly for a turbine that may include: (1) a nozzle-blade having inner and outer sidewalls and, in part, defining a flowpath upon assembly into the turbine; (2) an outer ring; (3) a flowsplitter having a horizontal extension; (4) an interface between the outer ring and the outer sidewall having at least one of (i) a male/female interface or (ii) a radial interlock; and (5) an interface between the horizontal extension and the inner sidewall having at least one of (i) the male/female interface or (ii) the radial interlock. In some embodiments, one of the interface between the outer ring and the outer sidewall and the interface between the horizontal extension and the inner sidewall comprises a weld and one of the interface between the outer ring and the outer sidewall and the interface between the horizontal extension and the inner sidewall is weld free.
摘要翻译：一种用于涡轮机的喷嘴组件，其可以包括：（1）具有内壁和外侧壁的喷嘴刀片，并且在组装到涡轮机中时部分地限定流路; （2）外圈; （3）具有水平延伸的分流器; （4）外环和外侧壁之间的界面，其具有（i）阳/阴接口或（ii）径向互锁中的至少一个; 和（5）水平延伸部和内侧壁之间的界面，其具有（i）阳/阴接口或（ii）径向互锁中的至少一个。在一些实施例中，外环和外侧壁之间的界面之一以及水平延伸部和内侧壁之间的界面之一包括焊接部以及外环与外侧壁之间的界面之一以及水平延伸部内侧壁无焊缝。

3. 发明申请

US20080050221A1 Systems for moisture removal in steam turbine engines 有权
标题翻译：蒸汽涡轮发动机除湿系统
公开(公告)号：US20080050221A1
公开(公告)日：2008-02-28
申请号：US11511598
申请日：2006-08-28
申请人： Steven S. Burdgick , Frolov Boris Ivanovitch
发明人： Steven S. Burdgick , Frolov Boris Ivanovitch
IPC分类号： F01D25/32
CPC分类号： F01D25/32 , F05D2260/602
摘要： A system in a steam turbine for removing water droplets from the flowpath of a steam turbine that may include a groove for collecting water droplets, and a plurality of moisture removal holes originating within the groove. The groove may run in a circumferential manner around an outer sidewall of the steam turbine, be axially positioned upstream and in close proximity to the leading edge of a nozzle, and have a gradual slope at a leading edge and a steep wall at a trailing edge. The moisture removal holes may be a channel through the outer sidewall through which the water droplets that collect in the groove may flow.
摘要翻译：蒸汽涡轮机中的系统，用于从可能包括用于收集水滴的凹槽的蒸汽轮机的流动路径中除去水滴，以及源自凹槽内的多个除湿孔。凹槽可以以圆周方式围绕蒸汽轮机的外侧壁运行，轴向位于上游并且紧邻喷嘴的前缘，并且在前缘处具有渐变斜率，并且在后缘处具有陡壁。除湿孔可以是通过外侧壁的通道，通过该外侧壁收集在槽中的水滴可以流过。

4. 发明授权

US07874795B2 Turbine nozzle assemblies 有权
标题翻译：涡轮喷嘴总成
公开(公告)号：US07874795B2
公开(公告)日：2011-01-25
申请号：US11518708
申请日：2006-09-11
申请人： Steven S. Burdgick , Thomas W. Crall
发明人： Steven S. Burdgick , Thomas W. Crall
IPC分类号： F03B3/16
CPC分类号： F01D9/044 , F01D3/02 , F01D25/246 , F05D2220/31 , F05D2230/53 , F05D2230/642 , F05D2260/36
摘要： A nozzle assembly for a turbine that may include: (1) a nozzle blade having inner and outer sidewalls and, in part, defining a flowpath upon assembly into the turbine; (2) an outer ring; (3) a flowsplitter having a horizontal extension; (4) an interface between the outer ring and the outer sidewall having at least one of (i) a male/female interface or (ii) a radial interlock; and (5) an interface between the horizontal extension and the inner sidewall having at least one of (i) the male/female interface or (ii) the radial interlock. In some embodiments, one of the interface between the outer ring and the outer sidewall and the interface between the horizontal extension and the inner sidewall comprises a weld and one of the interface between the outer ring and the outer sidewall and the interface between the horizontal extension and the inner sidewall is weld free.
摘要翻译：一种用于涡轮机的喷嘴组件，其可以包括：（1）具有内侧壁和外侧壁的喷嘴叶片，并且部分地在组装到涡轮机中时限定流路; （2）外圈; （3）具有水平延伸的分流器; （4）外环和外侧壁之间的界面，其具有（i）阳/阴接口或（ii）径向互锁中的至少一个; 和（5）水平延伸部和内侧壁之间的界面，其具有（i）阳/阴接口或（ii）径向互锁中的至少一个。在一些实施例中，外环和外侧壁之间的界面之一以及水平延伸部和内侧壁之间的界面之一包括焊接部以及外环与外侧壁之间的界面之一以及水平延伸部内侧壁无焊缝。

5. 发明授权

US07766625B2 Methods and apparatus for reducing stress in turbine buckets 有权
标题翻译：减少涡轮叶片应力的方法和装置
公开(公告)号：US07766625B2
公开(公告)日：2010-08-03
申请号：US11396046
申请日：2006-03-31
申请人： Steven S. Burdgick , Christophe Lanaud , Adegboyega Makinde , Wendy Lin , Grama Praveen , Amitabh Bansal
发明人： Steven S. Burdgick , Christophe Lanaud , Adegboyega Makinde , Wendy Lin , Grama Praveen , Amitabh Bansal
IPC分类号： F01D5/14
CPC分类号： F01D5/26 , F01D5/16 , F01D5/282 , F05D2300/603 , Y02T50/672 , Y02T50/673
摘要： A method facilitates reducing stress in a turbine bucket including a metallic base metal. The method comprises providing a turbine bucket including at least one pocket formed therein, and filling at least one pocket defined in the bucket with a polymer composite having continuous fibers oriented in a resin matrix, such that the fibers have an orientation determined in accordance with a pre-selected frequency tuning of the bucket.
摘要翻译：一种有助于减少包括金属基底金属的涡轮机桶中的应力的方法。该方法包括提供一种包括形成在其中的至少一个袋的涡轮机桶，并且用在树脂基体中定向的连续纤维的聚合物复合物填充限定在桶中的至少一个袋，使得纤维具有根据预先选择的桶的频率调谐。

6. 发明授权

US5605438A Casing distortion control for rotating machinery 失效
标题翻译：旋转机械套管变形控制
公开(公告)号：US5605438A
公开(公告)日：1997-02-25
申请号：US580694
申请日：1995-12-29
申请人： Steven S. Burdgick , John R. Hess , Gary D. Mercer , Gregory A. Crum , James E. Cencula , John A. Eastman
发明人： Steven S. Burdgick , John R. Hess , Gary D. Mercer , Gregory A. Crum , James E. Cencula , John A. Eastman
IPC分类号： F01D25/14 , F01D25/24 , F01D25/26
CPC分类号： F01D25/26 , F01D25/145 , F01D25/24 , F01D25/243
摘要： A turbine casing is provided in two casing halves joined one to the other along a horizontal splitline having flanges with spaced boltholes. A circumferentially extending rib is provided about each casing half at a location just forward of the turbine buckets to minimize or eliminate distortion caused by internal pressure and meridional roll of the casing. One or more axially extending ribs is provided on each casing half. The axial ribs have a radial stiffness which substantially matches the stiffness and thermal response of the flanges.
摘要翻译：涡轮机壳体设置在沿着具有间隔开的螺栓的凸缘的水平分裂线彼此连接的两个半壳体中。围绕每个壳体半部在靠近涡轮机叶片的位置处设置周向延伸的肋，以最小化或消除由壳体的内部压力和子午线引起的变形。在每个壳体半部上设置一个或多个轴向延伸的肋。轴向肋具有基本上匹配凸缘的刚度和热响应的径向刚度。

7. 发明授权

US07997860B2 Welded nozzle assembly for a steam turbine and related assembly fixtures 有权
标题翻译：用于蒸汽轮机和相关组装夹具的焊接喷嘴组件
公开(公告)号：US07997860B2
公开(公告)日：2011-08-16
申请号：US11892716
申请日：2007-08-27
申请人： Steven S. Burdgick , Thomas P. Russo
发明人： Steven S. Burdgick , Thomas P. Russo
IPC分类号： F01D1/02
CPC分类号： F01D9/042 , F01D1/02 , F01D9/02 , F05D2230/232 , F05D2230/64 , Y10T29/49323
摘要： A nozzle blade comprising radially inner and outer walls with an airfoil portion extending therebetween; the inner and outer walls formed with alignment features on respective oppositely-facing surfaces aligned with a longitudinal center axis through the nozzle blade.
摘要翻译：一种喷嘴刀片，包括径向的内壁和外壁，翼型部分在其间延伸; 所述内壁和外壁在相应的相对表面上形成有对准特征，所述对置特征与通过所述喷嘴叶片的纵向中心轴对准。

8. 发明授权

US07789618B2 Systems for moisture removal in steam turbine engines 有权
标题翻译：蒸汽涡轮发动机除湿系统
公开(公告)号：US07789618B2
公开(公告)日：2010-09-07
申请号：US11511598
申请日：2006-08-28
申请人： Steven S. Burdgick , Frolov Boris Ivanovitch
发明人： Steven S. Burdgick , Frolov Boris Ivanovitch
IPC分类号： F01D25/32
CPC分类号： F01D25/32 , F05D2260/602
摘要： A system in a steam turbine for removing water droplets from the flowpath of a steam turbine that may include a groove for collecting water droplets, and a plurality of moisture removal holes originating within the groove. The groove may run in a circumferential manner around an outer sidewall of the steam turbine, be axially positioned upstream and in close proximity to the leading edge of a nozzle, and have a gradual slope at a leading edge and a steep wall at a trailing edge. The moisture removal holes may be a channel through the outer sidewall through which the water droplets that collect in the groove may flow.
摘要翻译：蒸汽涡轮机中的系统，用于从可能包括用于收集水滴的凹槽的蒸汽轮机的流动路径中除去水滴，以及源自凹槽内的多个除湿孔。凹槽可以以圆周方式围绕蒸汽轮机的外侧壁运行，轴向位于上游并且紧邻喷嘴的前缘，并且在前缘处具有渐变斜率，并且在后缘处具有陡壁。除湿孔可以是通过外侧壁的通道，通过该外侧壁收集在槽中的水滴可以流过。

9. 发明授权

US07588421B2 Methods and apparatus for mechanical retainment of non-metallic fillers in pockets 有权
标题翻译：在口袋中机械保持非金属填料的方法和装置
公开(公告)号：US07588421B2
公开(公告)日：2009-09-15
申请号：US11395632
申请日：2006-03-31
申请人： Steven S. Burdgick , Christophe Lanaud , Adegboyega Makinde , Wendy Lin
发明人： Steven S. Burdgick , Christophe Lanaud , Adegboyega Makinde , Wendy Lin
IPC分类号： F01D5/18
CPC分类号： F01D5/147 , F01D5/26 , F01D5/282 , Y02T50/672 , Y02T50/673
摘要： A method for making a turbine blade includes providing a bucket in the turbine blade with a plurality of window pockets passing all the way through a wall of the bucket, positioning the window pockets in regions minimizing or at least reducing stress concentrations on the window pockets, and casting a composite comprising a resin matrix and layers of a fabric material in the bucket.
摘要翻译：一种用于制造涡轮机叶片的方法包括在涡轮机叶片中设置多个窗口袋，所述多个窗口袋一直穿过所述桶的壁，将所述窗口袋定位成最小化或至少减小所述窗口袋上的应力集中的区域，并在桶中浇铸包含树脂基体和织物材料层的复合材料。

10. 发明授权

US06733229B2 Insert metering plates for gas turbine nozzles 有权
标题翻译：插入燃气轮机喷嘴的计量板
公开(公告)号：US06733229B2
公开(公告)日：2004-05-11
申请号：US10092572
申请日：2002-03-08
申请人： Steven S. Burdgick , Gary Itzel , Sanjay Chopra , Nesim Abuaf , Victor H. Correia
发明人： Steven S. Burdgick , Gary Itzel , Sanjay Chopra , Nesim Abuaf , Victor H. Correia
IPC分类号： F01D906
CPC分类号： F01D5/189 , F01D9/065 , F05D2260/201
摘要： The invention comprises a metering plate which is assembled to an impingement insert for use in the nozzle of a gas turbine. The metering plate can have one or more metering holes and is used to balance the cooling flow within the nozzle. A metering plate with multiple holes reduces static pressure variations which result from the cooling airflow through the metering plate. The metering plate can be assembled to the insert before or after the insert is inserted into the nozzle.
摘要翻译：本发明包括计量板，其被组装到用于燃气轮机的喷嘴中的冲击插入件。计量板可以具有一个或多个计量孔，并用于平衡喷嘴内的冷却流。具有多个孔的计量板减少了由通过计量板的冷却气流引起的静压变化。在将插入件插入喷嘴之前或之后，计量盘可以组装到插入件上。

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