公开(公告)号：WO2008091377A2

公开(公告)日：2008-07-31

申请号：PCT/US2007/074320

申请日：2007-07-25

Applicant: POWER SYSTEMS MFG., LLC

Inventor： BIONDO, Charles ,  STROHL, J., Page ,  SAMUELSON, Jeffery, W. ,  FUCHS, Gerhard, E.

IPC: C22C19/05

CPC classification number: C22F1/10 ,  C22C19/03 ,  C22C19/05 ,  C22C19/056

Abstract: A nickel-based alloy suitable for casting gas turbine components having a lower density and basic heat treating process while achieving improved strength is disclosed. Multiple embodiments of the alloy are disclosed capable of providing both directionally-solidified and equiaxed castings. Also disclosed is a method of making a cast and heat treated article utilizing the improved nickel-base alloy.

Abstract translation: 公开了适用于铸造具有较低密度和基本热处理工艺的燃气涡轮机部件同时实现改善的强度的镍基合金。 公开了能够提供定向凝固和等轴铸造两者的合金的多个实施例。 还公开了使用改进的镍基合金制造铸造和热处理制品的方法。

公开(公告)号：WO2004038197A1

公开(公告)日：2004-05-06

申请号：PCT/US2003/013589

申请日：2003-05-01

Applicant: POWER SYSTEMS MFG., LLC

Inventor： JORGENSEN, Stephen, W. ,  RESOS, John, C. ,  XIAO, Zhenhua ,  JOHNSTON, Heather

IPC: F02C1/00

CPC classification number: F01D9/023

Abstract: A transition duct (20) having a panel assembly (23) with an inlet end (21) of generally circular cross section and an outlet end (22) having a generally rectangular arc-like cross section is disclosed. The panel assembly has an uncoated internal profile substantially in accordance with coordinate values X, Y, and Z as set forth in Table 1 carried only to three decimal places wherein the coordinates are taken at a sweep angle θ wherein θ is an angle measured from said inlet end and X, Y, and Z are coordinates defining the panel assembly profile at each angle θ from the inlet end. An alternate embodiment is also disclosed defining an envelope for the uncoated internal profile of the panel assembly.

Abstract translation: 公开了具有具有大致圆形横截面的入口端（21）的面板组件（23）和具有大致矩形的弧形横截面的出口端（22）的过渡管道（20）。 面板组件具有基本上根据如表1所示的坐标值X，Y和Z的未涂覆的内部轮廓，其仅承载在三位小数位置，其中坐标是以扫描角θ拍摄的，其中θ是从所述 入口端和X，Y和Z是在入口端的每个角度θ处限定面板组件轮廓的坐标。 还公开了一种替代实施例，其限定面板组件的未涂覆内部轮廓的包络。

公开(公告)号：WO2019025996A1

公开(公告)日：2019-02-07

申请号：PCT/IB2018/055776

申请日：2018-08-01

Applicant: POWER SYSTEMS MFG., LLC

Inventor： VOGEL, Gregory Edwin ,  METTERNICH, Jeremy ,  KAWECKI, Edwin John ,  SNYDER, Jacob

IPC: B22F3/24 ,  B22F5/00 ,  B22F5/04 ,  C22F1/10 ,  B33Y40/00

CPC classification number: B22F3/1028 ,  B22F3/1055 ,  B22F3/24 ,  B22F5/009 ,  B22F5/04 ,  B22F2003/248 ,  B22F2998/10 ,  B33Y10/00 ,  B33Y40/00 ,  B33Y80/00 ,  C22F1/10 ,  F01D5/187 ,  F05D2230/22 ,  F05D2230/31

Abstract: A method for manufacturing and heat treating a component formed from an alloy or superalloy. The component may be part of a gas turbine engine, such as an airfoil of a gas turbine engine turbine, or a combustor fuel nozzle, that includes internal cooling passages. At least part of the component is formed from the alloy or superalloy using an additive manufacturing process. The method includes determining an incipient melting point range and a recrystallization temperature of the alloy or superalloy. The component is then heated to at least the recrystallization temperature and within the incipient melting point range for a predetermined time, and ultimately cooled.

公开(公告)号：WO2007053323A3

公开(公告)日：2007-08-02

申请号：PCT/US2006040903

申请日：2006-10-19

Applicant: POWER SYSTEMS MFG LLC

IPC: F02C1/00

CPC classification number: F01D9/023 ,  F23R3/04 ,  F23R3/54

Abstract: An apparatus and method of providing a gas turbine combustor having increased combustion stability and reducing pressure drop across a gas turbine combustor is disclosed. A plurality of vanes is fixed to a flow sleeve radially between the flow sleeve and a combustion liner. The plurality of vanes serve to direct a flow of air entering the region between the flow sleeve and combustion liner in a substantially axial direction, such that components of tangential velocity are removed thereby providing a more uniform flow of air the combustion chamber and reducing the amount of pressure lost due attempting to straighten the airflow by pressure drop alone.

Abstract translation: 公开了一种提供具有增加的燃烧稳定性和降低通过燃气轮机燃烧器的压降的燃气轮机燃烧器的设备和方法。 多个叶片在流动套筒和燃烧衬套之间径向地固定到流动套筒。 多个叶片用于引导进入流动套筒和燃烧衬套之间的区域的基本轴向方向的空气流，使得切向速度分量被去除，由此提供燃烧室的更均匀的空气流动并且减少 由于试图仅通过压力降低气流而造成的压力损失。

公开(公告)号：WO2007053323A2

公开(公告)日：2007-05-10

申请号：PCT/US2006/040903

申请日：2006-10-19

Applicant: POWER SYSTEMS MFG., LLC

IPC: F02C3/06

CPC classification number: F01D9/023 ,  F23R3/04 ,  F23R3/54

Abstract: An apparatus and method of providing a gas turbine combustor having increased combustion stability and reducing pressure drop across a gas turbine combustor is disclosed. A plurality of vanes is fixed to a flow sleeve radially between the flow sleeve and a combustion liner. The plurality of vanes serve to direct a flow of air entering the region between the flow sleeve and combustion liner in a substantially axial direction, such that components of tangential velocity are removed thereby providing a more uniform flow of air the combustion chamber and reducing the amount of pressure lost due attempting to straighten the airflow by pressure drop alone.

Abstract translation: 公开了一种提供具有增加的燃烧稳定性并减少跨越燃气轮机燃烧器的压降的燃气轮机燃烧器的装置和方法。 多个叶片在流动套筒和燃烧衬套之间径向固定到流动套管。 多个叶片用于引导进入流动套筒和燃烧衬套之间的区域的空气流在大致轴向方向上，从而去除切向速度的分量，从而提供更均匀的空气流，并减少燃烧室的量 由于试图通过单独的压力降低气流而导致的压力损失。

公开(公告)号：WO2004013465A1

公开(公告)日：2004-02-12

申请号：PCT/US2003/013280

申请日：2003-05-01

Applicant: POWER SYSTEMS MFG., LLC

Inventor： JORGENSEN, Stephen, W.

IPC: F01D25/26

CPC classification number: F01D25/26 ,  F01D9/023 ,  Y10S138/04

Abstract: A transition duct with a thermally free aft frame for use in a gas turbine engine is disclosed. The transition duct includes an aft frame that is thermally free through the use of a plurality of retention lugs, bushings, and bulkhead assemblies. The aft frame is allowed to adjust from thermal changes as a result of relative sizing between the bushings and retention lugs of the aft frame. An additional feature of this invention is the use of radially extending ribs along the sidewalls of the aft frame, to form an interlocking sealing means with adjacent transition ducts to reduce the amount compressor air leakage into the turbine inlet.

Abstract translation: 公开了一种用于燃气涡轮发动机的具有无热后视框架的过渡管道。 过渡管道包括通过使用多个保持凸耳，衬套和隔板组件而无热的后框架。 由于后框架的衬套和保持凸耳之间的相对尺寸，后框架被允许从热变化调节。 本发明的一个附加特征是沿着后部框架的侧壁使用沿径向延伸的肋条，以形成具有相邻过渡管道的互锁密封装置，以减少压缩机空气泄漏到涡轮机入口中的量。

公开(公告)号：WO2008091377A3

公开(公告)日：2008-12-24

申请号：PCT/US2007074320

申请日：2007-07-25

Applicant: POWER SYSTEMS MFG LLC

Inventor： BIONDO CHARLES ,  STROHL J PAGE ,  SAMUELSON JEFFERY W ,  FUCHS GERHARD E ,  WLODEK STANLEY T ,  WLODEK RAMONA T

IPC: C22C19/03

CPC classification number: C22F1/10 ,  C22C19/03 ,  C22C19/05 ,  C22C19/056

Abstract: A nickel-based alloy suitable for casting gas turbine components having a lower density and basic heat treating process while achieving improved strength is disclosed. Multiple embodiments of the alloy are disclosed capable of providing both directionally-solidified and equiaxed castings. Also disclosed is a method of making a cast and heat treated article utilizing the improved nickel-base alloy.

Abstract translation: 公开了一种适用于铸造具有较低密度和基础热处理工艺的燃气轮机部件同时实现改进的强度的镍基合金。 公开了能够提供定向凝固和等轴铸件的合金的多个实施例。 还公开了利用改进的镍基合金制造铸造和热处理制品的方法。

公开(公告)号：WO2003029616A1

公开(公告)日：2003-04-10

申请号：PCT/US2002/023263

申请日：2002-07-23

Applicant: POWER SYSTEMS MFG, LLC

Inventor： SELESKI, Richard ,  CHIURATO, Remo

IPC: F01D5/22

CPC classification number: F01D5/187 ,  F01D5/147 ,  F01D5/225 ,  F05D2260/232 ,  F05D2260/2322

Abstract: An improved gas turbine blade (40) is disclosed that utilizes a blade tip shroud (46) with tapered shroud pockets (52) to remove excess weight from the shroud (46) while not compromising shroud bending stresses. Excess shroud weight removed by the tapered pockets (52) reduces overall blade pull while maintaining material necessary to increase shroud stiffness. The resulting rib (53) created between the tapered pockets (52) provides a surface, away from possible areas of stress concentration, for drilling radial cooling holes (54).

Abstract translation: 公开了一种改进的燃气轮机叶片（40），其利用具有锥形护罩袋（52）的叶片护罩（46），以从护罩（46）移除多余的重量，同时不损害护罩弯曲应力。 通过锥形凹部（52）去除的过多的护罩重量降低了整体刀片拉动，同时保持了增加护罩刚度所需的材料。 在锥形凹部（52）之间产生的所得肋（53）提供远离可能的应力集中区域的表面，用于钻出径向冷却孔（54）。

公开(公告)号：WO2023091306A2

公开(公告)日：2023-05-25

申请号：PCT/US2022/048862

申请日：2022-11-03

Applicant: POWER SYSTEMS MFG., LLC ,  KALB, Bryan ,  YAQUINTO, Matthew ,  CHONG, Gene ,  PARADES, David ,  BRACKETT, James ,  VOGEL, Gregory ,  RIZKALLA, Hany ,  SAM, Bernard Tam Yen ,  KESHAVA-BHATTU, Ramesh ,  HERNANDEZ, Fred ,  MCNALLY, Joshua R.

Inventor： KALB, Bryan ,  YAQUINTO, Matthew ,  CHONG, Gene ,  PARADES, David ,  BRACKETT, James ,  VOGEL, Gregory ,  RIZKALLA, Hany ,  SAM, Bernard Tam Yen ,  KESHAVA-BHATTU, Ramesh ,  HERNANDEZ, Fred ,  MCNALLY, Joshua R.

Abstract: An injector for a combustor of a gas turbine engine is provided with a plurality of air/fuel mixing tubes divided into radially outer and radially inner subsets of air/fuel mixing tubes with a first fuel manifold in fluid communication with the radially outer subset of air/fuel mixing tubes and a second fuel manifold in fluid communication with the radially inner subset of air/fuel mixing tubes. A blocker is provided at an outlet portion of each of the air/fuel mixing tubes of the radially outer subset of air/fuel mixing tubes and/or the radially inner subset of air/fuel mixing tubes to form a flame anchoring surface.

公开(公告)号：WO2004040108A1

公开(公告)日：2004-05-13

申请号：PCT/US2003/013204

申请日：2003-05-01

Applicant: POWER SYSTEMS MFG., LLC

Inventor： LEAHY, James, H.

IPC: F02C3/14

CPC classification number: F01D9/023 ,  F05D2260/202

Abstract: An effusion cooled transition duct (40) with angled film cooling holes in the axial and optionally transverse directions is disclosed.

Abstract translation: 公开了一种在轴向和任选地横向上具有成角度的薄膜冷却孔的渗出冷却的过渡管道（40）。