公开(公告)号：US06886327B1

公开(公告)日：2005-05-03

申请号：US10627107

申请日：2003-07-22

Applicant: Michael V. Nathal ,  John Gayda ,  Ronald D. Noebe

Inventor： Michael V. Nathal ,  John Gayda ,  Ronald D. Noebe

IPC: C23C28/02 ,  F02K9/62 ,  F02K9/68 ,  B32B15/01

CPC classification number: B32B15/01 ,  C23C28/021 ,  F02K9/62 ,  F02K9/68 ,  F05C2201/0466 ,  F05D2300/121 ,  F05D2300/506 ,  Y10T428/12937 ,  Y10T428/12944

Abstract: A multi-layered component, such as a rocket engine combustion chamber, includes NiAl or NiAl-based alloy as a structural layer on the “hot” side of the component. A second structural layer is formed of material selected from Ni-based superalloys, Co-based alloys, Fe-based alloys, Cu, and Cu-based alloys. The second material is more ductile than the NiAl and imparts increased toughness to the component. The second material is selected to enhance one or more predetermined physical properties of the component. Additional structural layers may be included with the additional material(s) being selected for their impact on physical properties of the component.

Abstract translation: 诸如火箭发动机燃烧室的多层组件包括NiAl或NiAl基合金作为组件的“热”侧上的结构层。 第二结构层由选自Ni基超级合金，Co基合金，Fe基合金，Cu和Cu基合金的材料形成。 第二种材料比NiAl更具延展性，并且赋予组分更高的韧性。 选择第二材料以增强部件的一个或多个预定的物理性质。 另外的结构层可以包括在附加材料中，以选择它们对组件的物理性质的影响。

公开(公告)号：US20050069440A1

公开(公告)日：2005-03-31

申请号：US10948245

申请日：2004-09-24

Applicant: Yoshihiro Naito

Inventor： Yoshihiro Naito

IPC: F04B39/00 ,  F04C18/08 ,  F04C18/12 ,  F04C18/18 ,  F04C23/00 ,  F04C25/02 ,  F04C27/00 ,  F04C29/00 ,  F03C2/00

CPC classification number: F04C18/126 ,  F04C18/084 ,  F04C23/003 ,  F04C25/02 ,  F04C2220/12 ,  F04C2230/21 ,  F04C2230/231 ,  F04C2230/60 ,  F05C2201/021 ,  F05C2201/0439 ,  F05C2201/0442 ,  F05C2201/046 ,  F05C2201/0466 ,  F05C2201/903 ,  F05C2203/06 ,  F05C2251/042

Abstract: A multistage dry pump includes a pump housing having plural pump chambers aligned in parallel, a rotational shaft extending along a parallel alignment direction of the plural pump chambers and rotatably supported by the pump housing, and plural rotors parallelly aligned in an axial direction of the rotational shaft and furnished in the respective plural pump chambers. The rotational shaft is formed with a base material of which linear expansion coefficient is less than 6×10−6 m/m·K inclusive, and the respective plural rotors is made of a material which is more easily machined than the material of the rotational shaft.

Abstract translation: 多级干式泵包括：泵壳体，其具有平行排列的多个泵室，沿着多个泵室的平行排列方向延伸并由泵壳体可旋转地支撑的旋转轴，以及沿旋转轴线方向平行排列的多个转子 并设置在相应的多个泵室中。 旋转轴形成有线膨胀系数小于6×10 -6 m / m·K的基材，并且各个转子由比旋转轴的材料更容易加工的材料制成。

公开(公告)号：US20050042124A1

公开(公告)日：2005-02-24

申请号：US10885239

申请日：2004-07-07

Applicant: Naoki Miyagi ,  Fujio Yamamoto ,  Yuichi Murai ,  Koji Miyazaki ,  Futoshi Matsui ,  Yuji Aoyagi

Inventor： Naoki Miyagi ,  Fujio Yamamoto ,  Yuichi Murai ,  Koji Miyazaki ,  Futoshi Matsui ,  Yuji Aoyagi

IPC: F04C2/08 ,  F04C2/10 ,  F04C15/00 ,  F01C1/02

CPC classification number: F04C2/084 ,  F04C2/102 ,  F04C15/008 ,  F05C2201/0406 ,  F05C2201/0409 ,  F05C2201/046 ,  F05C2201/0466 ,  F05C2203/08 ,  F05C2203/0882 ,  F05C2225/04 ,  F05C2225/10 ,  F05C2225/12 ,  F05C2253/20

Abstract: A circular disc shape case 11 includes a motor rotor chamber 12, a bearing chamber 13 and a gear chamber 14 piled sequentially and being communicated with each other. A suction port 15 is connected to the motor rotor chamber 12, and a discharge port 16 is connected to the gear chamber 14, which communicate with outside respectively. A rotating shaft 18 having an end positioned in the motor rotor chamber 13 and the other end extending to the gear chamber 14. A rotor 22 is fixed around the rotation shaft 18 in the motor rotor chamber 13. A first bearing 19 is provided for supporting the end of the rotating shaft 18 in radial and thrust directions. A second bearing 20 is provided in the bearing chamber 13 for supporting an intermediate portion of the rotating shaft 18 in radial direction. A trochoid gear 25 is provided in the gear chamber 14, having an outer rotor 26 and an inner rotor 27, which functions as a pump, taking in a fluid through the suction port pipe 15, and discharging the fluid from the discharge port 16.

Abstract translation: 圆盘形壳体11包括依次堆叠并且彼此连通的马达转子室12，轴承室13和齿轮室14。 吸入口15连接到电动机转子室12，排出口16连接到与外部连通的齿轮室14。 旋转轴18，其一端位于电动机转子室13中，另一端延伸到齿轮室14.转子22围绕电动机转子室13中的旋转轴18固定。第一轴承19设置成用于支撑 旋转轴18的端部在径向和推力方向上。 第二轴承20设置在轴承室13中，用于沿径向支撑旋转轴18的中间部分。 摆动齿轮25设置在齿轮室14中，具有外转子26和内转子27，其用作泵，通过吸入口管15吸入流体，并从排出口16排出流体。

公开(公告)号：US20040223850A1

公开(公告)日：2004-11-11

申请号：US10775139

申请日：2004-02-11

Inventor： Thomas Kramer ,  Andreas Kuenzler ,  Mohamed Yousef Nazmy ,  Markus Staubli

IPC: F03B003/12

CPC classification number: F01D5/28 ,  F01D5/147 ,  F04D29/023 ,  F04D29/322 ,  F05C2201/0466 ,  F05D2300/171 ,  F05D2300/174 ,  F05D2300/18 ,  Y02T50/672 ,  Y02T50/673

Abstract: The invention relates to a hybrid blade (1) for thermal turbomachines, having an airfoil (2) made of a metallic material of a certain density, and having a blade root (3). It is characterized in that the blade root (3), compared with the airfoil (2), is made of a different metallic material having a lower density, and in that the airfoil (20) is connected to the blade root (3) in a positive-locking manner. The blade in this case is advantageously a compressor blade, in particular a high-pressure compressor blade, in which the airfoil (2) is made of a stainless CrNi steel and the blade root (3) is made of a high-temperature titanium alloy or an intermetallic gamma titanium aluminide alloy or an intermetallic orthorhombic titanium aluminide alloy.

Abstract translation: 本发明涉及一种用于热涡轮机的混合叶片（1），具有由一定密度的金属材料制成并具有叶根（3）的翼型（2）。 其特征在于，与翼型件（2）相比，叶片根部（3）由具有较低密度的不同的金属材料制成，并且翼型件（20）以与叶片根部（3）相连的方式连接到叶片根部 积极的方式。 在这种情况下，叶片有利地是压缩机叶片，特别是高压压缩机叶片，其中翼型件（2）由不锈钢CrNi钢制成，叶片根部（3）由高温钛合金制成 或金属间化合物γ铝铝合金或金属间斜方晶钛铝化合物。

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：US06755619B1

公开(公告)日：2004-06-29

申请号：US09709010

申请日：2000-11-08

Applicant: Richard John Grylls ,  Curtiss Mitchell Austin ,  Jerry Donald Schell

Inventor： Richard John Grylls ,  Curtiss Mitchell Austin ,  Jerry Donald Schell

IPC: F01D1108

CPC classification number: F01D11/08 ,  F01D5/20 ,  F05C2201/0466 ,  F05D2300/121 ,  F05D2300/2112 ,  F05D2300/222 ,  F05D2300/612 ,  Y02T50/67 ,  Y02T50/672 ,  Y10T428/249953 ,  Y10T428/249955 ,  Y10T428/249956 ,  Y10T428/249957 ,  Y10T428/249967

Abstract: A turbine blade has an airfoil section with a root end and a tip end, and an attachment at the root end of the airfoil section. A blade tip seal is joined to the tip end of the airfoil section. The blade tip seal is formed as an open-cell solid aluminum oxide foam made of aluminum oxide cell walls having intracellular volume therebetween. The blade tip seal has a blade interface region adjacent to the tip end of the airfoil section. The blade interface region is formed of the aluminum oxide foam and a nickel-base alloy within the intracellular volume. The blade tip seal also has a contact region remote from the blade interface region and comprising the aluminum foam wherein the intracellular volume is porosity.

Abstract translation: 涡轮叶片具有具有根端和尖端的翼型部分，以及在翼型部分的根端处的附件。 叶片末端密封件连接到翼型部分的末端。 刀片密封件形成为由其间具有细胞内体积的氧化铝细胞壁制成的开孔固体氧化铝泡沫。 叶片尖端密封件具有与翼型部分的尖端相邻的叶片接口区域。 叶片界面区域由细胞内体积内的氧化铝泡沫体和镍基合金形成。 叶片尖端密封件还具有远离叶片界面区域的接触区域，并且包括铝泡沫体，其中细胞内体积是孔隙率。

公开(公告)号：US20040058191A1

公开(公告)日：2004-03-25

申请号：US10455830

申请日：2003-06-06

Inventor： Dave Narasimhan ,  Alexander S. Kozlov ,  Margaret Eagan ,  Milton Ortiz

IPC: B32B015/00

CPC classification number: F01D5/288 ,  C23C8/02 ,  C23C26/00 ,  F01D5/3084 ,  F01D5/3092 ,  F05C2201/0466 ,  F05D2300/143 ,  F05D2300/607 ,  Y02T50/67 ,  Y10T428/12611 ,  Y10T428/12771 ,  Y10T428/12778 ,  Y10T428/12847 ,  Y10T428/12854 ,  Y10T428/12875 ,  Y10T428/12889 ,  Y10T428/12937 ,  Y10T428/12944 ,  Y10T428/265

Abstract: A nickel base single crystal compliant layer on a ceramic blade has the capability to sustain high stresses and high operating temperature. Layers of nickel and platinum bonded on a single crystal superalloy over a sputtered gold-chromium layer support the high stress levels at elevated temperature without extrusion of the soft platinum or nickel layer and without destruction of an NiO compliant surface. The compliant layers have survived stress and temperature conditions without failure to the ceramic blade and the system can be stressed/heated and unloaded/cooled repeatedly without damage to the ceramic blades. A single crystal nickel base superalloy (i.e., SC180) has high strength properties at elevated temperature. Thin layers of chromium followed by gold are e-beam evaporated on one side of a polished surface of the alloy. Pure nickel is electroplated over this e-beam gold-chromium layer. Platinum is either electroplated or plated electrolessly over the nickel layer. The structure is annealed in vacuum or inert atmosphere to allow the diffusion of gold-chromium alloy into the superalloy and permit the nickel layer and diffusion of nickel into platinum to form a multilayer structure which is metallurgically bonded. The sheet is oxidized in air to allow diffusion of the nickel layer through the platinum to come to the surface and oxidize forming nickel oxide. This nickel oxide layer acts as the load distribution layer which does not extrude and the structural integrity of the compliant layer is maintained by the high-strength single crystal superalloy.

Abstract translation: 陶瓷刀片上的镍基单晶柔性层具有维持高应力和高工作温度的能力。 在溅射的金 - 铬层上结合在单晶超合金上的镍和铂层在升高的温度下支持高应力水平，而不会挤出软的铂或镍层，并且不破坏NiO柔顺表面。 柔性层在应力和温度条件下已经存活，而不会损坏陶瓷刀片，并且系统可以被重复地加压/加热和卸载/冷却，而不损坏陶瓷刀片。 单晶镍基超级合金（即SC180）在升高的温度下具有高强度性能。 在合金的抛光表面的一侧上电子束蒸发薄铬层后面的金。 在该电子束金 - 铬层上电镀纯镍。 将铂电镀或电镀在镍层上。 该结构在真空或惰性气氛中进行退火，以允许金 - 铬合金扩散到超合金中，并允许镍层和镍扩散到铂中以形成冶金结合的多层结构。 该片材在空气中被氧化以允许镍层通过铂的扩散进入表面并氧化形成的氧化镍。 该氧化镍层用作不挤出的载荷分布层，并且由高强度单晶超耐热合金维持柔顺层的结构完整性。

公开(公告)号：US20040013521A1

公开(公告)日：2004-01-22

申请号：US10398941

申请日：2003-04-11

Inventor： Takeshi Yamada

IPC: F03B011/00

CPC classification number: F01D5/3061 ,  F01D5/025 ,  F01D5/048 ,  F03B11/00 ,  F05B2230/21 ,  F05B2230/211 ,  F05B2230/23 ,  F05B2280/10304 ,  F05C2201/0466 ,  F05D2230/21 ,  F05D2230/211 ,  F05D2230/23 ,  F05D2300/133 ,  Y02E10/226 ,  Y02P70/525

Abstract: A hybrid rotor, a manufacturing method thereof and a gas turbine realize reduced manufacturing cost and reduced weight of parts. An impeller part 31 as a rotor main part comprises a bore portion 32, impellers 34 provided therearound and a shaft bore 33 provided centrally of the bore portion 32. An enlarged shaft bore portion 35 is coaxially provided in the shaft bore 33. The impeller part 31 is made of Ti or Ni alloy by precision casting. A ring member 10 made of a metal base composite material is inserted into the enlarged shaft bore portion 35 and is bonded together by friction bonding or diffusion bonding to thereby strengthen the rotor. The rotor main part is manufactured by precision casting without need of machining. The ring member 10 is separately manufactured from the impeller part 11. By strengthening the rotor, the bore portion 32 can be made thin. Thus, manufacturing cost is remarkably reduced and weight of the rotor is also reduced.

Abstract translation: 混合式转子，其制造方法和燃气轮机实现了制造成本的降低，部件重量的减轻。 作为转子主体的叶轮部31包括孔部32，设置在其周围的叶轮34和设置在孔部32的中央的轴孔33.在轴孔33中同轴地设置有扩大的轴孔部35。 31由精密铸造的Ti或Ni合金制成。 将由金属基复合材料制成的环件10插入到扩大轴孔部分35中，并通过摩擦粘合或扩散接合结合在一起，从而加强转子。 转子主体采用精密铸造而无需加工。 环形构件10分别由叶轮部11制造。通过加强转子，可以使孔部32变薄。 因此，制造成本显着降低，转子的重量也降低。

公开(公告)号：US06606983B2

公开(公告)日：2003-08-19

申请号：US09954842

申请日：2001-09-18

Applicant: Tom Bedwell ,  Carmo Ribeiro ,  Miguel N. D. De Azevedo

Inventor： Tom Bedwell ,  Carmo Ribeiro ,  Miguel N. D. De Azevedo

IPC: F02B5102

CPC classification number: F02F3/10 ,  F05C2201/0448 ,  F05C2201/0466 ,  F05C2253/12

Abstract: A corrosion resistant piston for use in an exhaust gas recirculation diesel engine. The piston includes a crown portion having ring grooves formed around a periphery of the crown portion. The ring grooves are separated by ring lands. The piston also includes a piston rod connecting portion that extends from the crown portion. The piston is made of steel and includes an electroless coating of nickel having a maximum thickness of 8 micrometers.

Abstract translation: 用于废气再循环柴油发动机的耐腐蚀活塞。 所述活塞包括冠部，所述冠部具有围绕所述冠部的周边形成的环形槽。 环形槽由环形环分开。 活塞还包括从冠部延伸的活塞杆连接部分。 活塞由钢制成并且包括最大厚度为8微米的镍的无电涂层。

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