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1. 发明申请

US20100232938A1 Gas Turbine Having Seal Assembly with Coverplate and Seal 有权
标题翻译：燃气轮机具有盖板和密封件的密封组件
公开(公告)号：US20100232938A1
公开(公告)日：2010-09-16
申请号：US12402800
申请日：2009-03-12
申请人： John Wesley Harris, JR. , Matthew Robert Piersall , Brian Denver Potter
发明人： John Wesley Harris, JR. , Matthew Robert Piersall , Brian Denver Potter
IPC分类号： F02C7/28 , F01D11/08
CPC分类号： F01D5/26 , F01D5/3015 , F01D11/006
摘要： A gas turbine and a seal assembly for a machine having a rotating shaft, a wheel coupled to the rotating shaft, the wheel including a bucket coupled to the wheel comprising a coverplate that is fastened to the wheel and the bucket and a seal positioned between the coverplate and the wheel and the bucket.
摘要翻译：一种用于机器的燃气轮机和密封组件，其具有旋转轴，联接到旋转轴的轮，所述轮包括联接到所述车轮的铲斗，所述铲斗包括紧固到所述车轮和所述铲斗的盖板和位于所述车轮之间的密封件盖板和砂轮和铲斗。

2. 发明申请

US20100232939A1 Machine Seal Assembly 审中-公开
标题翻译：机器密封组件
公开(公告)号：US20100232939A1
公开(公告)日：2010-09-16
申请号：US12402808
申请日：2009-03-12
申请人： Matthew Robert Piersall , John Wesley Harris, JR. , Brian Denver Potter
发明人： Matthew Robert Piersall , John Wesley Harris, JR. , Brian Denver Potter
IPC分类号： F01D11/08
CPC分类号： F01D5/082 , F01D11/006 , F01D11/04 , F05D2240/55 , F05D2240/57
摘要： A machine and a seal assembly for a machine having a rotating shaft, a wheel coupled to the rotating shaft, the wheel including a bucket coupled to the wheel comprising a seal that extends along a side of the bucket and the wheel, covering an interface there between.
摘要翻译：一种用于机器的机器和密封组件，其具有旋转轴，联接到旋转轴的轮，所述轮包括联接到所述车轮的铲斗，所述铲斗包括沿着所述铲斗和所述车轮的侧面延伸的密封件，之间。

3. 发明申请

US20130189087A1 NEAR FLOW PATH SEAL FOR A TURBOMACHINE 有权
标题翻译：涡轮机附近的流路密封
公开(公告)号：US20130189087A1
公开(公告)日：2013-07-25
申请号：US13354610
申请日：2012-01-20
申请人： David Randolph Spracher , John Wesley Harris, JR. , Brian Denver Potter , Zachary James Taylor , Ryan Zane Ziegler
发明人： David Randolph Spracher , John Wesley Harris, JR. , Brian Denver Potter , Zachary James Taylor , Ryan Zane Ziegler
IPC分类号： F01D11/00
CPC分类号： F01D5/3007 , F01D11/001
摘要： A near flow path seal member for a turbomachine includes a seal body having a seal support member including a first end portion that extends to a second end portion through an intermediate portion. An arm member extends from the first end portion of the seal body. The arm member has a first end that extends to a second end to define an axial dimension of the arm member, a first edge that extends to a second, opposing edge to define a circumferential dimension of the arm member, and a surface having a profile that establishes a thickness variation of the arm member in each of the axial dimension and the circumferential dimension.
摘要翻译：用于涡轮机的近流路密封构件包括具有密封支撑构件的密封体，密封支撑构件包括通过中间部分延伸到第二端部的第一端部。臂部件从密封体的第一端部延伸。臂构件具有延伸到第二端以限定臂构件的轴向尺寸的第一端，延伸到第二相对边缘以限定臂构件的周向尺寸的第一边缘，以及具有轮廓的表面这确定了臂构件在轴向尺寸和周向尺寸中的每一个中的厚度变化。

4. 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。

5. 发明申请

US20120082549A1 APPARATUS AND METHODS FOR COOLING PLATFORM REGIONS OF TURBINE ROTOR BLADES 有权
标题翻译：用于冷却涡轮转子叶片平台区域的装置和方法
公开(公告)号：US20120082549A1
公开(公告)日：2012-04-05
申请号：US12894993
申请日：2010-09-30
申请人： Scott Edmond Ellis , John Wesley Harris, JR. , Adrian Lional Scott
发明人： Scott Edmond Ellis , John Wesley Harris, JR. , Adrian Lional Scott
IPC分类号： F01D5/08 , B23P15/04
CPC分类号： F01D5/187 , F01D5/087 , F05D2230/60 , F05D2230/80 , F05D2240/81 , F05D2250/185 , Y02T50/676 , Y10T29/49336 , Y10T29/49341 , Y10T29/49718 , Y10T29/49721
摘要： A platform cooling arrangement in a turbine rotor blade having a platform at an interface between an airfoil and a root, wherein the rotor blade includes an interior cooling passage that in operation, includes at least a high-pressure coolant region and a low-pressure coolant region, and wherein the platform includes a platform underside. The platform cooling arrangement may include: a plate that comprises a plate topside; a channel formed on the plate topside, the channel comprising an upstream end and a downstream end, and being open through the plate topside such that, upon attaching the plate to the platform, the platform underside comprises a channel ceiling; a high-pressure connector that connects the upstream end of the channel to the high-pressure coolant region of the interior cooling passage; and a low-pressure connector that connects the downstream end of the channel to the low-pressure coolant region of the interior cooling passage.
摘要翻译：在涡轮转子叶片中的平台冷却装置，其具有在翼型件和根部之间的界面处的平台，其中转子叶片包括内部冷却通道，其在运行中包括至少高压冷却剂区域和低压冷却剂区域，并且其中所述平台包括平台下侧。平台冷却装置可以包括：板，其包括顶板; 形成在板顶侧的通道，所述通道包括上游端和下游端，并且通过所述板顶部开口，使得在将所述板附接到所述平台时，所述平台下侧包括通道顶板; 高压连接器，其将通道的上游端连接到内部冷却通道的高压冷却剂区域; 以及将通道的下游端连接到内部冷却通道的低压冷却剂区域的低压连接器。

6. 发明申请

US20100196164A1 Turbine Coverplate Systems 有权
标题翻译：涡轮盖板系统
公开(公告)号：US20100196164A1
公开(公告)日：2010-08-05
申请号：US12366486
申请日：2009-02-05
申请人： Gary Charles Liotta , Christopher Sean Bowes , John Wesley Harris, JR.
发明人： Gary Charles Liotta , Christopher Sean Bowes , John Wesley Harris, JR.
IPC分类号： F01D5/32
CPC分类号： F01D5/3015 , F01D11/005 , F05D2240/55 , Y02T50/671
摘要： In one embodiment, a coverplate may be configured to axially overlay a plurality of blade retaining slots within a wheel post of a rotor wheel. The coverplate may include a tab for radially securing the coverplate within a complementary groove of the rotor wheel and an aperture configured to align with a corresponding aperture of the turbine wheel to receive a fastener for axially securing the coverplate to the rotor wheel.
摘要翻译：在一个实施例中，盖板可被构造成轴向地覆盖转子轮的轮柱内的多个叶片保持槽。盖板可以包括用于将盖板径向地固定在转子轮的互补槽内的突片，以及被配置为与涡轮机叶轮的相应孔对准的孔，以容纳用于将盖板轴向固定到转子轮的紧固件。

7. 发明申请

US20130187339A1 Near Flow Path Seal with Axially Flexible Arms 有权
标题翻译：近轴流动密封与轴向柔性臂
公开(公告)号：US20130187339A1
公开(公告)日：2013-07-25
申请号：US13354365
申请日：2012-01-20
申请人： John Wesley Harris, JR. , Bruce J. Badding , Brian D. Potter
发明人： John Wesley Harris, JR. , Bruce J. Badding , Brian D. Potter
IPC分类号： F16J15/44
CPC分类号： F01D11/00 , F01D11/001 , F01D11/008 , F05D2220/3213
摘要： The present application provides a near flow path seal for a gas turbine. The near flow path seal includes a base, a pair of arms extending from the base, and a curved indentation positioned between the pair of arms.
摘要翻译：本申请为燃气轮机提供近流路密封。近流路密封件包括基座，从基座延伸的一对臂和位于该对臂之间的弯曲凹槽。

8. 发明申请

US20120107135A1 APPARATUS, SYSTEMS AND METHODS FOR COOLING THE PLATFORM REGION OF TURBINE ROTOR BLADES 审中-公开
标题翻译：用于冷却涡轮转子叶片平台区域的装置，系统和方法
公开(公告)号：US20120107135A1
公开(公告)日：2012-05-03
申请号：US12915501
申请日：2010-10-29
申请人： John Wesley Harris, JR. , Daniel Howard Tragesser , Anthony Louis Giglio
发明人： John Wesley Harris, JR. , Daniel Howard Tragesser , Anthony Louis Giglio
IPC分类号： F01D5/18 , B23P15/02
CPC分类号： F01D5/186 , F01D5/187 , F05D2240/81 , F05D2260/202 , Y02T50/676 , Y10T29/49341
摘要： A platform cooling arrangement in a turbine rotor blade having a platform at an interface between an airfoil and a root, wherein the rotor blade includes an interior cooling passage that extends to the approximate radial height of the platform, and wherein, a pressure side of the platform comprises a planar topside that extends circumferentially from the airfoil to a pressure side slashface, and a suction side of the platform comprises a substantially planar topside that extends circumferentially from the airfoil to a suction side slashface. The platform cooling arrangement may include a linear plenum residing just inboard of the planar topside and linearly extending through the platform from either the pressure side slashface or the suction side slashface to a connection with the interior cooling passage, the linear plenum having a longitudinal axis that is approximately parallel to the planar topside; and a plurality of cooling apertures linearly extending from a topside outlet formed on the topside of the platform to a connection with the linear plenum, wherein the cooling apertures are configured such that each forms an acute angle with the topside of the platform.
摘要翻译：涡轮转子叶片中的平台冷却装置，其具有在翼型件和根部之间的界面处的平台，其中转子叶片包括延伸到平台的近似径向高度的内部冷却通道，并且其中，平台包括从翼型件到圆周方向延伸到压力侧斜面的平面顶面，并且平台的吸力侧包括从翼型件周向延伸到吸力侧斜面的基本平坦的顶侧。平台冷却装置可以包括位于平坦顶侧的刚好内侧并且从压力侧斜面或吸力侧斜面直线延伸穿过平台的线性增压室到与内部冷却通道的连接，线性增压室具有纵向轴线，大致平行于平面顶面; 以及多个冷却孔，其从形成在所述平台顶部上的顶部出口线性地延伸到与所述线性压力室的连接，其中所述冷却孔配置成使得每个与所述平台的顶侧形成锐角。

9. 发明申请

US20120107134A1 APPARATUS AND METHODS FOR COOLING PLATFORM REGIONS OF TURBINE ROTOR BLADES 有权
标题翻译：用于冷却涡轮转子叶片平台区域的装置和方法
公开(公告)号：US20120107134A1
公开(公告)日：2012-05-03
申请号：US12915477
申请日：2010-10-29
申请人： John Wesley Harris, JR. , Craig Allen Bielek , Scott Edmond Ellis , Xiaoyong Fu
发明人： John Wesley Harris, JR. , Craig Allen Bielek , Scott Edmond Ellis , Xiaoyong Fu
IPC分类号： F01D5/18 , B23P15/02
CPC分类号： F01D5/081 , F01D5/18 , F05D2240/81 , F05D2260/22141 , Y02T50/676
摘要： A platform cooling arrangement in a turbine rotor blade having a platform at an interface between an airfoil and a root, wherein the rotor blade includes an interior cooling passage that extends from a connection at the root to the approximate radial height of the platform, wherein, the interior cooling passage comprises a high-pressure coolant region and a low-pressure coolant region, and wherein a pressure side of the platform comprises a topside extending circumferentially from the airfoil to a pressure side slashface. The platform cooling arrangement may include: a platform cavity formed within the pressure side of the platform, a high-pressure connector that connects the platform cavity to the high-pressure coolant region of the interior cooling passage; a low-pressure connector that connects the platform cavity to the low-pressure coolant region of the interior cooling passage; and a pin bank formed within the platform cavity that includes radial pins.
摘要翻译：涡轮转子叶片中的平台冷却装置，其具有在翼型件和根部之间的界面处的平台，其中所述转子叶片包括从根部的连接部延伸到所述平台的近似径向高度的内部冷却通道，内部冷却通道包括高压冷却剂区域和低压冷却剂区域，并且其中平台的压力侧包括从翼面周向延伸到压力侧斜面的顶侧。平台冷却装置可以包括：形成在平台的压力侧内的平台空腔，将平台空腔连接到内部冷却通道的高压冷却剂区域的高压连接器; 将平台腔连接到内部冷却通道的低压冷却剂区域的低压连接器; 以及形成在所述平台腔内的销排，所述销组包括径向销。

10. 发明申请

US20120082564A1 APPARATUS AND METHODS FOR COOLING PLATFORM REGIONS OF TURBINE ROTOR BLADES 有权
标题翻译：用于冷却涡轮转子叶片平台区域的装置和方法
公开(公告)号：US20120082564A1
公开(公告)日：2012-04-05
申请号：US12894878
申请日：2010-09-30
申请人： Scott Edmond Ellis , Daniel Alan Hynum , John Wesley Harris, JR.
发明人： Scott Edmond Ellis , Daniel Alan Hynum , John Wesley Harris, JR.
IPC分类号： F01D5/18 , B23P15/02
CPC分类号： F01D5/081 , F01D5/3007 , F05D2240/81 , F05D2250/184 , F05D2250/185 , F05D2260/201 , Y02T50/676 , Y10T29/49341
摘要： A platform cooling arrangement in a turbine rotor blade having a platform that includes an interior cooling passage formed therein. The platform cooling arrangement may include: a main plenum residing just inboard of the planar topside and extending from an aft position to a forward position within one of the pressure side and the suction side of the platform, the main plenum having a longitudinal axis that is approximately parallel to the planar topside; a supply plenum that extends between the main plenum and the interior cooling passage; and a plurality of cooling apertures, each cooling aperture extending from one of the pressure side and the suction side slashface to a connection with the main plenum.
摘要翻译：具有平台的涡轮转子叶片中的平台冷却装置，该平台包括形成在其中的内部冷却通道。平台冷却装置可以包括：主平台顶部的内侧并且从后部位置延伸到平台的压力侧和吸入侧之一的前部位置的主增压室，主增压室具有纵向轴线，大致平行于平面顶面; 一个在主室和内部冷却通道之间延伸的供气室; 以及多个冷却孔，每个冷却孔从压力侧和抽吸侧斜面之一延伸到与主增压室的连接。

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