公开(公告)号：US07252477B2

公开(公告)日：2007-08-07

申请号：US11340510

申请日：2006-01-27

Applicant: Yasuoki Tomita ,  Kouji Watanabe ,  Masamitsu Okuzono ,  Masaki Ono

Inventor： Yasuoki Tomita ,  Kouji Watanabe ,  Masamitsu Okuzono ,  Masaki Ono

IPC: F01D11/00

CPC classification number: F01D5/081 ,  F01D5/22 ,  F01D11/008 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2250/29 ,  F05D2260/20 ,  Y02T50/671 ,  Y02T50/676 ,  Y10S416/50

Abstract: A rotating blade body is provided that can restrain vibrations of rotating blades effectively. The rotating blade body comprises a rotor disc, a plurality of rotating blades being assembled so as to extend from the outer circumference of the rotor disc in a radial pattern, and sealing pins extending along the direction of the rotating shaft in the gaps between the platforms of the rotating blades being adjacent in a circumferential direction. The sealing pins have a through-hole made therein, penetrating axially from one end surface to the other end surface.

Abstract translation: 提供了可以有效地抑制旋转叶片的振动的旋转叶片体。 旋转叶片本体包括转子盘，多个旋转叶片组装成以径向图案从转子盘的外圆周延伸，并且在平台之间的间隙中沿着旋转轴的方向延伸的密封销 的旋转叶片在圆周方向上相邻。 密封销具有形成在其中的通孔，其从一个端面轴向穿透到另一端面。

公开(公告)号：US20060179838A1

公开(公告)日：2006-08-17

申请号：US11350108

申请日：2006-02-09

Applicant: Hiroshi Nakagawa ,  Yasuaki Jinnai ,  Isamu Inamura

Inventor： Hiroshi Nakagawa ,  Yasuaki Jinnai ,  Isamu Inamura

IPC: F02D23/00

CPC classification number: F01D17/165 ,  F02C6/12 ,  F05C2201/0463 ,  F05D2220/40 ,  F05D2230/232 ,  F05D2230/30 ,  F05D2300/131 ,  F05D2300/506

Abstract: The present invention provides a variable-throat exhaust turbocharger equipped with a variable-throat mechanism of which connection of constituent members can be achieved with a small number of man-hour and at low cost and which is stable in quality with firm connection of constituent members maintained under severe operating conditions. Among constituent members of the variable throat-area mechanism of the variable-throat exhaust turbocharger for varying the blade angle of a plurality of nozzle vanes supported rotatably by a members in a turbine casing, shaft members to be inserted and fixed in through-holes in a member with through-holes are produced by a method in which wear-resistant material is welded to form cladding of a certain thickness on the upper surface of a steel plate, said material being harder than the steel plate, and then crude shafts for forming drive pins are cut out from the clad plate.

Abstract translation: 本发明提供了一种可变喉排气涡轮增压器，其具有可变喉部机构，其可以以少量的工时和低成本实现组成部件的连接，并且其质量稳定并且构成部件的牢固连接 维持在恶劣的运行条件下。 在可变喉排气涡轮增压器的可变喉部区域机构的构成部件中，用于改变由涡轮机壳体中的部件可旋转地支撑的多个喷嘴叶片的叶片角度，轴构件被插入并固定在通孔中 具有通孔的构件通过焊接耐磨材料的方法制造，以在钢板的上表面上形成一定厚度的包层，所述材料比钢板硬，然后用于形成的粗制轴 驱动销从复合板切出。

公开(公告)号：US20050207896A1

公开(公告)日：2005-09-22

申请号：US10801843

申请日：2004-03-16

Applicant: Michael Gigliotti ,  Canan Hardwicke ,  Liang Jiang ,  John Short ,  Don Lipkin ,  Jonathan Blank ,  Krishnamurthy Anand

Inventor： Michael Gigliotti ,  Canan Hardwicke ,  Liang Jiang ,  John Short ,  Don Lipkin ,  Jonathan Blank ,  Krishnamurthy Anand

IPC: F01D5/28 ,  B23K20/02 ,  C22C14/00 ,  C22C19/03 ,  C22F1/00 ,  C23C26/00 ,  C23C28/00 ,  C23C30/00 ,  F01D25/00 ,  F02C7/00 ,  F23R3/42 ,  B32B15/01 ,  B32B9/00

CPC classification number: B23K20/08 ,  F01D5/28 ,  F01D5/288 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2220/31 ,  F05D2230/311 ,  F05D2230/312 ,  F05D2230/313 ,  F05D2230/80 ,  F05D2230/90 ,  F05D2300/501 ,  F05D2300/505 ,  F05D2300/611 ,  Y10S420/902 ,  Y10T428/12493 ,  Y10T428/12611 ,  Y10T428/12806 ,  Y10T428/12944

Abstract: An erosion resistant protective structure for a turbine engine component comprises a shape memory alloy. The shape memory alloy includes nickel-titanium based alloys, indium-titanium based alloys, nickel-aluminum based alloys, nickel-gallium based alloys, copper based alloys, gold-cadmium based alloys, iron-platinum based alloys, iron-palladium based alloys, silver-cadmium based alloys, indium-cadmium based alloys, manganese-copper based alloys, ruthenium-niobium based alloys, ruthenium-tantalum based alloys, titanium based alloys, iron-based alloys, or combinations comprising at least one of the foregoing alloys. Also, disclosed herein are methods for forming the shape memory alloy onto turbine component.

Abstract translation: 用于涡轮发动机部件的抗侵蚀保​​护结构包括形状记忆合金。 形状记忆合金包括镍 - 钛基合金，铟 - 钛基合金，镍 - 铝基合金，镍 - 镓基合金，铜基合金，金 - 镉基合金，铁 - 铂基合金，铁 - 钯基合金 银镉基合金，铟镉基合金，锰 - 铜基合金，钌 - 铌基合金，钌 - 钽基合金，钛基合金，铁基合金或包含至少一种上述合金的组合 。 此外，本文公开的是将形状记忆合金形成在涡轮部件上的方法。

公开(公告)号：US06926779B1

公开(公告)日：2005-08-09

申请号：US09451538

申请日：1999-12-01

Applicant: Feng Bin

Inventor： Feng Bin

IPC: B32B15/01 ,  C22C9/00 ,  C22C9/06 ,  C23C30/00 ,  F04B27/10

CPC classification number: C22C9/00 ,  B32B15/015 ,  B32B15/017 ,  C22C9/06 ,  C23C30/00 ,  F04B27/1054 ,  F05C2201/021 ,  F05C2201/0406 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05C2201/0475 ,  F05C2201/0493 ,  F05C2203/0882 ,  F05C2225/04 ,  F05C2253/12

Abstract: A surface of aluminum alloy or iron alloy coated, on at least a part, with a lead-free copper-based coating layer comprising, by weight, 0.2–15% bismuth, and at least one metal selected from the group consisting of 5–40% nickel, 1–20% chromium, 1–20% iron, and 1–10% cobalt, the balance being copper which is more than 55%. The surface may be of a swashplate used in swashplate type compressors.

Abstract translation: 在至少一部分上涂覆无铅铜基涂层的铝合金或铁合金表面，其包含重量比为0.2-15％的铋和至少一种选自以下的金属：5- 40％镍，1-20％铬，1-20％铁和1-10％钴，余量为大于55％的铜。 表面可以是斜盘式压缩机中使用的斜盘。

公开(公告)号：US06821641B2

公开(公告)日：2004-11-23

申请号：US10086150

申请日：2001-10-22

Applicant: Robert William Bruce ,  Nicholas Hamilton Burlingame

Inventor： Robert William Bruce ,  Nicholas Hamilton Burlingame

IPC: B32B1504

CPC classification number: C23C28/321 ,  C23C4/18 ,  C23C14/083 ,  C23C14/58 ,  C23C16/045 ,  C23C28/325 ,  C23C28/345 ,  C23C28/3455 ,  C23C30/00 ,  F01D5/288 ,  F05C2201/0463 ,  F05D2230/90 ,  F05D2300/161 ,  F05D2300/2112 ,  F05D2300/611 ,  Y10T428/12611 ,  Y10T428/12618 ,  Y10T428/12875 ,  Y10T428/12944

Abstract: An article protected by a thermal barrier coating system includes a substrate having a substrate surface, and a thermal barrier coating system overlying the substrate. The thermal barrier coating system has a thermal barrier coating formed of a thermal barrier coating material arranged as a plurality of columnar grains extending generally perpendicular to the substrate surface and having grain surfaces. A sintering inhibitor is within the columnar grains, either uniformly distributed or concentrated at the grain surfaces. The sintering inhibitor is lanthanum oxide, lanthanum chromate, chromium oxide, and/or yttrium chromate, mixtures thereof, mixtures thereof with aluminum oxide, modifications thereof wherein cobalt or manganese is substituted for chromium, precursors thereof, and reaction products thereof.

Abstract translation: 由热障涂层系统保护的物品包括具有基底表面的基底和覆盖基底的热障涂层系统。 热障涂层系统具有由隔热涂层材料形成的热障涂层，所述热障涂层布置为大致垂直于基板表面延伸并具有晶粒表面的多个柱状晶粒。 烧结抑制剂在柱状晶粒内，均匀分布或集中在晶粒表面。 烧结抑制剂是氧化镧，铬酸镧，氧化铬和/或铬酸钇，它们的混合物，与氧化铝的混合物，其中钴或锰代替铬的前体及其反应产物。

公开(公告)号：US06783642B2

公开(公告)日：2004-08-31

申请号：US10237696

申请日：2002-09-10

Applicant: Gérard Gueldry ,  Claude Mons

Inventor： Gérard Gueldry ,  Claude Mons

IPC: C23C1434

CPC classification number: F01D11/02 ,  F01D11/001 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2230/10 ,  F05D2300/21 ,  F05D2300/502 ,  Y02T50/67 ,  Y02T50/671

Abstract: In order to make labyrinth seal lips on the periphery of a metal moving part of a turbomachine, a thick layer of refractory material that adheres to the metal is made prior to assembling the moving part, the refractory material advantageously comprising at least one metal selected for example from Fe, Co, and Ni, together with at least one ceramic selected for example from borides, nitrides, carbides, and refractory oxides. The labyrinth seal lips that are to be made are machined to their final dimensions in the deposited thick layer.

公开(公告)号：US20030002988A1

公开(公告)日：2003-01-02

申请号：US09867489

申请日：2001-05-30

Applicant: General Electric Company

Inventor： Melvin Robert Jackson ,  Bernard Patrick Bewlay ,  Ji-Cheng Zhao

IPC: F01D001/02

CPC classification number: F01D5/28 ,  B23K35/0222 ,  B23K35/28 ,  B23K35/30 ,  B23K35/32 ,  B23K35/322 ,  B23K35/325 ,  B32B15/01 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2300/121 ,  F05D2300/13 ,  F05D2300/132 ,  F05D2300/133 ,  F05D2300/134 ,  F05D2300/142 ,  F05D2300/143 ,  F05D2300/222 ,  Y02T50/672 ,  Y10T428/12639 ,  Y10T428/12674 ,  Y10T428/12778 ,  Y10T428/12806 ,  Y10T428/12819 ,  Y10T428/12826 ,  Y10T428/12847 ,  Y10T428/12861 ,  Y10T428/12868 ,  Y10T428/12875 ,  Y10T428/12889

Abstract: An airfoil having a melting temperature of at least about 1500null C. and comprising a first piece and a second piece joined by a braze to the first piece. The first piece comprises one of a first niobium-based refractory metal intermetallic composite and a first-based refractory metal intermetallic composite, and the second piece comprises one of a second niobium-based refractory metal intermetallic composite and a second molybdenum-based refractory metal intermetallic composite. The braze joining the first piece to the second piece is a semi-solid braze that comprises a first component and a second component. The first component of the semi-solid braze comprises a first element and a second metallic element, wherein the first element is one of titanium, palladium, zirconium, niobium, germanium, silicon, and hafnium, and the second metallic element is a metal selected from the group consisting of titanium, palladium, zirconium, niobium, hafnium, aluminum, chromium, vanadium, platinum, gold, iron, nickel, and cobalt, the second metallic element being different from the first element. The second component has a melting temperature of at least about 1450null C. and comprises one of niobium, molybdenum, titanium, hafnium, silicon, boron, aluminum, tantalum, germanium, vanadium, tungsten, zirconium, and chromium. This abstract is submitted in compliance with 37 C.F.R. 1.72(b) with the understanding that it will not be used to interpret or limit the scope of or meaning of the claims.

Abstract translation: 具有至少约1500℃的熔化温度的翼型件，并且包括通过钎焊连接到第一件的第一件和第二件。 第一件包括第一铌基难熔金属金属间复合材料和第一种难熔金属金属间复合材料中的一种，第二件包括第二铌基难熔金属金属间复合物和第二种钼基难熔金属金属间化合物 综合。 将第一件连接到第二件的钎焊是包括第一部件和第二部件的半固体钎焊。 半固体钎焊的第一部件包括第一元件和第二金属元件，其中第一元件是钛，钯，锆，铌，锗，硅和铪之一，并且第二金属元素是选择的金属 从钛，钯，锆，铌，铪，铝，铬，钒，铂，金，铁，镍和钴组成的组中，第二金属元素不同于第一元素。 第二组分具有至少约1450℃的熔融温度，并且包括铌，钼，钛，铪，硅，硼，铝，钽，锗，钒，钨，锆和铬中的一种。 本摘要根据37 C.F.R. 1.72（b），但有一项谅解，即不会用于解释或限制权利要求的范围或含义

公开(公告)号：US06468669B1

公开(公告)日：2002-10-22

申请号：US09304276

申请日：1999-05-03

Applicant: Wayne Charles Hasz ,  Robert Alan Johnson ,  Ching-Pang Lee ,  Mark Gerard Rettig ,  Nesim Abuaf ,  John Howard Starkweather

Inventor： Wayne Charles Hasz ,  Robert Alan Johnson ,  Ching-Pang Lee ,  Mark Gerard Rettig ,  Nesim Abuaf ,  John Howard Starkweather

IPC: B32B1516

CPC classification number: F01D5/187 ,  B22F2998/00 ,  B23K35/0233 ,  B23K35/0244 ,  B23K35/025 ,  B23K35/3006 ,  B23K35/3033 ,  B23K35/3046 ,  B23K35/3053 ,  B23K35/322 ,  B23K37/047 ,  B23K2101/001 ,  B32B15/01 ,  C21D9/08 ,  C23C24/10 ,  C23C26/02 ,  F01D5/08 ,  F01D25/12 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2230/237 ,  F05D2240/127 ,  F05D2260/2212 ,  F05D2260/22141 ,  F05D2300/611 ,  F23R2900/03045 ,  F28F13/12 ,  F28F13/185 ,  F28F21/087 ,  Y10T29/49337 ,  Y10T29/49393 ,  Y10T428/12014 ,  Y10T428/12063 ,  Y10T428/12097 ,  Y10T428/12104 ,  Y10T428/12389 ,  Y10T428/12431 ,  Y10T428/12486 ,  Y10T428/12931 ,  Y10T428/12993 ,  B22F3/22 ,  B22F5/04

Abstract: An article includes turbulation material bonded to a surface of a substrate via a bonding agent, such as a braze alloy. In an embodiment, the turbulation material includes a particulate phase of discrete metal alloy particles having an average particle size within a range of about 125 microns to about 4000 microns. Other embodiments include methods for applying turbulation and articles for forming turbulation.

Abstract translation: 一种制品包括通过诸如钎焊合金的粘结剂粘合到基底表面的紊乱材料。 在一个实施方案中，该混浊材料包括具有约125微米至约4000微米范围内的平均粒度的离散金属合金颗粒的颗粒相。 其他实施例包括用于施加湍流和用于形成湍流的制品的方法。

公开(公告)号：US5911809A

公开(公告)日：1999-06-15

申请号：US50215

申请日：1998-03-30

Applicant: Carl Edward Cordy

Inventor： Carl Edward Cordy

IPC: C23C22/66 ,  F04B27/08 ,  F04B27/10 ,  F01B3/00

CPC classification number: F04B27/1054 ,  C23C22/66 ,  F04B27/0873 ,  F04B27/0891 ,  F04B27/0895 ,  F05C2201/021 ,  F05C2201/028 ,  F05C2201/0463 ,  F05C2201/0493 ,  F05C2203/06 ,  F05C2253/12 ,  Y10S428/926 ,  Y10S428/936 ,  Y10T428/12583 ,  Y10T428/1259 ,  Y10T428/12708 ,  Y10T428/12736 ,  Y10T428/1275

Abstract: A swash plate type compressor having a cylinder block with cylinder bores disposed parallel to the axis of the cylinder block. A rotary shaft rotatably mounted within the cylinder block carries an aluminum swash plate. The swash plate is fixed in the rotary shaft and has two facial surfaces and an end surface. The swash plate has a coating preferably between 0.8 to 2.5 microns, of a tin/cobalt coating of at least 0.2 wt% cobalt and the balance being tin. A piston reciprocally fitted within the cylinder bore contains shoes which slideably intervene between the piston and the swash plate facial surfaces and reciprocate the piston and the swash plate facial surfaces and reciprocate the pistons by rotation of the swash plate. The coating on the swash plate permits the use of low silicon alloy aluminum without the need of metal plating or high finish polishing.

Abstract translation: 一种斜盘式压缩机，其具有与气缸体的轴线平行设置的气缸孔的气缸体。 可旋转地安装在气缸体内的旋转轴携带铝斜盘。 旋转斜盘固定在旋转轴上，具有两个面和端面。 旋转斜盘具有优选为0.8至2.5微米的涂层，至少0.2重量％钴的锡/钴涂层和余量为锡的涂层。 往复配合在气缸孔内的活塞包含可滑动地插入活塞和斜盘面之间的滑块，并使活塞和旋转斜盘表面往复运动，并通过旋转斜盘的旋转使活塞往复运动。 旋转斜盘上的涂层允许使用低硅合金铝，而不需要金属电镀或高精抛光。

公开(公告)号：US5320909A

公开(公告)日：1994-06-14

申请号：US91077

申请日：1993-07-13

Applicant: Alan J. Scharman ,  Thomas M. Yonushonis

Inventor： Alan J. Scharman ,  Thomas M. Yonushonis

IPC: C23C4/02 ,  C23C28/00 ,  F02B1/04 ,  F02B3/06 ,  F02B77/02 ,  F02F3/12 ,  F02F7/00 ,  B32B15/20

CPC classification number: F02B77/02 ,  C23C28/00 ,  C23C4/02 ,  F02F3/12 ,  F02F7/0087 ,  F02B1/04 ,  F02B3/06 ,  F05C2201/021 ,  F05C2201/0436 ,  F05C2201/0448 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05C2203/08 ,  Y10T428/12493 ,  Y10T428/12542 ,  Y10T428/12549 ,  Y10T428/12611 ,  Y10T428/12618 ,  Y10T428/12639

Abstract: A thermal barrier coating for metal articles subjected to rapid thermal cycling includes a metallic bond coat deposited on the metal article, at least one MCrAlY/ceramic layer deposited on the bond coat, and a ceramic top layer deposited on the MCrAlY/ceramic layer. The M in the MCrAlY material is Fe, Ni, Co, or a mixture of Ni and Co. The ceramic in the MCrAlY/ceramic layer is mullite or Al.sub.2 O.sub.3. The ceramic top layer includes a ceramic with a coefficient of thermal expansion less than about 5.4.times.10.sup.-6 .degree.C.sup.-1 and a thermal conductivity between about 1 J sec.sup.-1 m.sup.-1 .degree.C.sup.-1 and about 1.7 J sec.sup.-1 m.sup.-1 .degree.C.sup.-1.

Abstract translation: 经受快速热循环的金属制品的热障涂层包括沉积在金属制品上的金属粘合涂层，沉积在粘合涂层上的至少一个MCrAlY /陶瓷层和沉积在MCrAlY /陶瓷层上的陶瓷顶层。 MCrAlY材料中的M是Fe，Ni，Co或Ni和Co的混合物。MCrAlY /陶瓷层中的陶瓷是莫来石或Al2O3。 陶瓷顶层包括热膨胀系数小于约5.4×10-6℃-1的陶瓷，热导率约为1J / sec-1m-1〜1m-1和约1.7Jsec-1m-1 DEG C-1。