公开(公告)号：US09784215B2

公开(公告)日：2017-10-10

申请号：US14536273

申请日：2014-11-07

申请人： ROHR, INC.

发明人： Jacques Jinqiu Lu ,  Chad Franks ,  Richard S. Alloway

IPC分类号： F02K1/00 ,  F02K1/80 ,  F01D25/24 ,  F01D25/30 ,  F02K1/04

CPC分类号： F02K1/80 ,  F01D25/243 ,  F01D25/30 ,  F02K1/04 ,  F05D2220/30 ,  F05D2230/642 ,  F05D2300/176 ,  F05D2300/177 ,  F05D2300/20 ,  F05D2300/6033 ,  Y02T50/672

摘要： A ceramic turbine engine exhaust component, such as a ceramic matrix composite (“CMC”) exhaust center body may be positioned around a metallic attachment ring. The attachment ring may have a greater coefficient of thermal expansion than the CMC center body. A plurality of bolts radially-spaced around the circumference of the attachment ring may be inserted through apertures in the center body with a sliding fit, and may be coupled to the attachment ring. The bolts may slide within the apertures, allowing the attachment ring to thermally expand without applying extra loads on the exhaust center body due to the expansion.

公开(公告)号：US09617856B2

公开(公告)日：2017-04-11

申请号：US13971460

申请日：2013-08-20

申请人： Mitsubishi Hitachi Power Systems, Ltd.

发明人： Takashi Shibayama ,  Shinya Imano ,  Hironori Kamoshida ,  Hidetoshi Kuroki ,  Jun Sato

IPC分类号： F01D5/14 ,  C22C19/05 ,  F01D5/28 ,  F01D5/02 ,  F01D5/06

CPC分类号： F01D5/147 ,  C22C19/055 ,  C22C19/056 ,  F01D5/02 ,  F01D5/066 ,  F01D5/28 ,  F05D2300/176 ,  Y02T50/671

摘要： An Ni base forged alloy is easy to make hot forging and miniaturization of crystal grains while excellent high-temperature strength and segregation property are compatible. The Ni base forged alloy has solid solution temperature of a precipitation strengthening phase lower than or equal to 970° C., difference in the solid solution temperature between a δ-phase and the precipitation strength phase larger than or equal to 50° C., Al of 0.5 to 1.0%, Cr of 17 to 21%, Fe of 17 to 19%, Nb of 4.5 to 5.5%, Ti of 0.8 to 1.3%, W of 3.0 to 6.0%, B of 0.001 to 0.03%, C of 0.001 to 0.1% and Mo of 1.0% or less in mass percentage [%] and remainder made of Ni and inevitable impurities.

公开(公告)号：US09416671B2

公开(公告)日：2016-08-16

申请号：US13645092

申请日：2012-10-04

申请人： GENERAL ELECTRIC COMPANY

发明人： Bill Damon Johnston ,  Daniel Anthony Nowak ,  Srikanth Chandrudu Kottilingam ,  Melbourne J Myers ,  Joe Timothy Nowak

IPC分类号： F01D25/24 ,  F01D9/02 ,  F01D11/08

CPC分类号： F01D9/02 ,  F01D11/08 ,  F05D2230/232 ,  F05D2240/11 ,  F05D2300/171 ,  F05D2300/175 ,  F05D2300/176 ,  Y10T29/49236

摘要： A bimetallic ring for use as a turbine shroud in a gas turbine engine. The bimetallic ring forms a sealing surface as a hot gas flow path boundary in the engine. The ring is comprised of two materials. The first material, a wrought, oxidation resistant metal alloy comprises a first portion, which is the hot gas flow path sealing surface. The second material, a low cost low alloy steel, comprises a second portion that may be at least a pair of supporting side plates. A dissimilar weld joint joins the sealing surface to the second portion, the at least pair of supporting side plates.

摘要翻译： 用作燃气涡轮发动机中的涡轮机罩的双金属环。 双金属环在发动机中形成作为热气流路边界的密封面。 该环由两种材料组成。 第一种材料，锻造的抗氧化金属合金包括作为热气体流路密封表面的第一部分。 第二种材料，低成本低合金钢，包括可以是至少一对支撑侧板的第二部分。 不同的焊接接头将密封表面连接到第二部分，至少一对支撑侧板。

公开(公告)号：US20150345307A1

公开(公告)日：2015-12-03

申请号：US14290237

申请日：2014-05-29

申请人： GENERAL ELECTRIC COMPANY

发明人： Dwight Eric DAVIDSON ,  Stephen Joseph BALSONE ,  Brian Denver POTTER

IPC分类号： F01D5/22

CPC分类号： F01D5/225 ,  C22C14/00 ,  C22C19/055 ,  C22C19/07 ,  C22C21/00 ,  F01D5/10 ,  F01D5/147 ,  F01D5/28 ,  F01D5/282 ,  F01D5/284 ,  F01D5/288 ,  F01D5/3007 ,  F05C2251/046 ,  F05D2300/174 ,  F05D2300/175 ,  F05D2300/176 ,  F05D2300/5021 ,  F05D2300/522

摘要： A turbine bucket assembly and turbine system are disclosed. The assembly includes a multi-lobe joint having an integral platform, the joint having a first axial length; a segmented airfoil having a root segment extending radially outward from the platform and a tip segment coupled to the root segment, the tip segment having a second axial length less than the first axial length; and a turbine wheel defining a receptacle with a geometry corresponding to the multi-lobe joint and being coupled to the multi-lobe joint. A tip segment material, a root segment material, and a turbine wheel material are selected, such that the turbine wheel material and the root segment material have a lower heat resistance and a higher thermal expansion than the tip segment material.

摘要翻译： 公开了一种涡轮机桶组件和涡轮机系统。 组件包括具有整体平台的多叶节接头，该接头具有第一轴向长度; 具有从所述平台径向向外延伸的根部段的分段翼型件和联接到根部段的尖端段，所述尖端段具有小于所述第一轴向长度的第二轴向长度; 以及涡轮机叶轮，其限定具有对应于所述多叶节接头的几何形状并且连接到所述多叶节接头的容器。 选择尖端段材料，根部段材料和涡轮机叶轮材料，使得涡轮机叶轮材料和根部材料具有比尖端段材料更低的耐热性和更高的热膨胀。

公开(公告)号：US20150132110A1

公开(公告)日：2015-05-14

申请号：US14400648

申请日：2013-06-14

申请人： United Technologies Corporation ,  GKN Aerospace Sweden AB

发明人： Daryl B. Mountz ,  Theodore W. Kapustka ,  Glenn Levasseur ,  Marcus Borg ,  Joakim Berglund ,  Anders Svahn ,  Johan Ockborn ,  Bengt Pettersson

IPC分类号： F01D25/24 ,  F02C9/18

CPC分类号： F01D25/005 ,  F01D21/045 ,  F01D25/162 ,  F01D25/24 ,  F01D25/30 ,  F02C9/18 ,  F02K1/386 ,  F05D2220/32 ,  F05D2230/21 ,  F05D2230/232 ,  F05D2230/25 ,  F05D2230/54 ,  F05D2260/941 ,  F05D2300/175 ,  F05D2300/176 ,  F05D2300/177 ,  F05D2300/502

摘要： A turbine exhaust case has an outer housing to be secured within a gas turbine engine and a central hub. Struts extend between the outer housing and the central hub. The struts are formed at least in part of a first material. The central hub is formed at least in part of a second material.

公开(公告)号：US20180209026A1

公开(公告)日：2018-07-26

申请号：US15743767

申请日：2015-09-14

申请人： Mitsubishi Hitachi Power Systems, Ltd.

发明人： Atsuo OTA ,  Shinya IMANO

IPC分类号： C22F1/10 ,  F01D5/28 ,  C22C19/05

CPC分类号： C22F1/10 ,  B23K20/122 ,  B23K2103/26 ,  B23P15/04 ,  C22C19/056 ,  C22F1/00 ,  F01D5/147 ,  F01D5/18 ,  F01D5/28 ,  F05D2230/12 ,  F05D2230/14 ,  F05D2230/239 ,  F05D2230/25 ,  F05D2230/41 ,  F05D2240/24 ,  F05D2240/307 ,  F05D2260/20 ,  F05D2300/176 ,  F05D2300/607 ,  F05D2300/701

摘要： In a manufacturing method of a turbine rotor blade using an Ni-based forged alloy, provided is a manufacturing method of a turbine rotor blade having an excellent workability and a high degree of freedom in the design of a cooling structure. A manufacturing method of a turbine rotor blade according to the present invention is, in a manufacturing method of a turbine rotor blade, using an Ni-based forged alloy, characterized by including: a softening process of increasing a γ′ phase incoherent with a γ phase that is a matrix phase in the Ni-based forged alloy; a first working process of forming at least two members constituting a rotor blade by using the Ni-based forged alloy after subjected to the softening process; a second working process of forming cooling structural parts in the respective members; and a third working process of joining the members.

公开(公告)号：US09611760B2

公开(公告)日：2017-04-04

申请号：US14305766

申请日：2014-06-16

申请人： SOLAR TURBINES INCORPORATED

发明人： Christopher Anthony Marino ,  Nathan James Bohney

IPC分类号： F01D25/30 ,  F01D11/00 ,  F01D25/24

CPC分类号： F01D25/30 ,  F01D11/003 ,  F01D25/243 ,  F01D25/246 ,  F05D2300/176

摘要： An aft clamp ring for a gas turbine engine is disclosed. The aft clamp ring includes a body, a forward sealing face, and an aft sealing face. The body includes an annular shape extending between an outer end and an inner end. The forward sealing face faces in a second axial direction. The aft sealing face is adjacent the outer end facing in a first axial direction and is at least partially radially aligned with the forward sealing face. The forward sealing face and the aft sealing face are each an annular surface with a surface area from 105.50 cm2 to 165.19 cm2.

公开(公告)号：US09506350B1

公开(公告)日：2016-11-29

申请号：US15009940

申请日：2016-01-29

申请人： Robert L Memmen

发明人： Robert L Memmen

IPC分类号： F01D5/18 ,  F01D5/14 ,  F01D5/28 ,  B23P15/04

CPC分类号： F01D5/147 ,  B23P15/04 ,  F01D5/18 ,  F01D5/28 ,  F01D5/284 ,  F05D2220/323 ,  F05D2230/21 ,  F05D2240/30 ,  F05D2260/30 ,  F05D2300/175 ,  F05D2300/176 ,  F05D2300/182 ,  F05D2300/2283 ,  Y02T50/673 ,  Y02T50/676

摘要： A turbine rotor blade of the spar and shell construction, where a one piece shell is secured to a hollow spar using a plurality of chordwise extending shear ties that are cast into a space formed between the shell interior and the spar exterior. A fill pipe is inserted into the hollow spar and is used to deliver the liquid retainer material to the hard to reach slots formed in which the shear ties solidify.

摘要翻译： 翼梁和壳体结构的涡轮机转子叶片，其中使用多个弦向延伸的剪切连接件将单件壳体固定到中空翼梁，所述多个弦向延伸的剪切连接件被铸造到形成在壳体内部和翼梁外部之间的空间中。 填充管插入中空翼梁中，用于将液体保持器材料输送到难以到达形成的剪切段固化的槽。

公开(公告)号：US20160115809A1

公开(公告)日：2016-04-28

申请号：US14830689

申请日：2015-08-19

申请人： United Technologies Corporation

发明人： Timothy M. Davis ,  Paul M. Lutjen

IPC分类号： F01D11/00 ,  F16J15/08

CPC分类号： F01D11/005 ,  F01D11/003 ,  F02C7/28 ,  F05D2220/32 ,  F05D2220/323 ,  F05D2240/55 ,  F05D2260/38 ,  F05D2300/176 ,  F05D2300/6033 ,  F16J15/0806 ,  F16J15/0887 ,  Y02T50/672

摘要： The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the first seal section and/or the second seal section, are disposed between the first and second seal sections, and bias the first and second seal sections away from one another.

摘要翻译： 本公开总体上涉及两个部件之间的滑动密封。 滑动密封件包括第一密封部分和非耦合的第二密封部分，其允许第一和第二密封部分在两个部件之间相对移动期间相对于彼此移动。 从第一密封部分和/或第二密封部分延伸的一个或多个弹簧片设置在第一和第二密封部分之间，并且将第一和第二密封部分彼此偏离。

公开(公告)号：US20130299467A1

公开(公告)日：2013-11-14

申请号：US13945214

申请日：2013-07-18

申请人： Bernd Burbaum ,  Selim Mokadem ,  Norbert Pirch

发明人： Bernd Burbaum ,  Selim Mokadem ,  Norbert Pirch

IPC分类号： B23K26/32

CPC分类号： B23K26/32 ,  B23K26/24 ,  B23K26/342 ,  B23K2101/001 ,  B23K2103/02 ,  B23K2103/26 ,  B23P6/045 ,  F01D5/005 ,  F05D2230/232 ,  F05D2300/175 ,  F05D2300/176 ,  Y10T428/12389

摘要： During welding, frequently cracks develop at the end of the weld seam. A method is provided in which the power is reduced at the end of the weld seam, reducing the development of cracks. For the method, a welding appliance is used wherein the welding appliance may be a laser.

摘要翻译： 在焊接过程中，焊缝末端会出现裂纹扩展。 提供了一种方法，其中在焊缝的端部处的功率减小，减少了裂纹的发展。 对于该方法，使用焊接设备，其中焊接设备可以是激光器。