公开(公告)号：US20170314410A1

公开(公告)日：2017-11-02

申请号：US15140903

申请日：2016-04-28

Applicant: United Technologies Corporation

Inventor： Xuan Liu ,  Christopher W. Strock ,  Russell A. Beers

IPC: F01D11/12 ,  C23C4/131 ,  C23C4/073 ,  F01D25/00 ,  F01D25/18 ,  C23C4/126 ,  C23C4/134

CPC classification number: F01D11/122 ,  B22F2998/10 ,  B22F2999/00 ,  C22C1/08 ,  C22C1/10 ,  C22C19/058 ,  C23C4/073 ,  C23C4/126 ,  C23C4/131 ,  C23C4/134 ,  F01D5/288 ,  F01D25/005 ,  F01D25/18 ,  F05D2220/32 ,  F05D2230/311 ,  F05D2230/60 ,  F05D2240/11 ,  F05D2300/175 ,  F05D2300/177 ,  F05D2300/2282 ,  F05D2300/509 ,  F05D2300/514 ,  F05D2300/6032 ,  F05D2300/612 ,  F05D2300/613 ,  F05D2300/614 ,  Y02T50/672 ,  B22F5/009 ,  B22F7/06 ,  B22F7/002 ,  B22F2003/248 ,  B22F3/115 ,  B22F3/11 ,  C22C1/0433 ,  B22F1/0059 ,  B22F3/1121

Abstract: A blade outer airseal has a body comprising: an inner diameter (ID) surface; an outer diameter (OD) surface; a leading end; and a trailing end. The airseal body has a metallic substrate and a coating system atop the substrate along at least a portion of the inner diameter surface. At least over a first area of the inner diameter surface, the coating system comprises an abradable layer comprising a metallic matrix and a solid lubricant; and the metallic matrix comprises, by weight, ≧35% nickel, 12.0-20.0% cobalt, 5.0-15.0% aluminum, and 5.0-15.0% chromium.

公开(公告)号：US09746085B2

公开(公告)日：2017-08-29

申请号：US13510052

申请日：2010-11-18

Applicant: Ralf Bode

Inventor： Ralf Bode

IPC: F16J15/44 ,  F01D11/02 ,  F16J15/453

CPC classification number: F16J15/445 ,  F01D11/02 ,  F05D2300/121 ,  F05D2300/171 ,  F05D2300/43 ,  F05D2300/509 ,  F16J15/453

Abstract: A labyrinth seal for sealing a sealing region between a rotor and stator of a rotary machine includes, a base, and a plurality of sealing rings. The sealing rings are formed on the base, project into the sealing region and form, between them labyrinth valleys bounded, laterally, by the sealing rings and, in the floor of the valleys, by the base. The sealing rings, in at least one region, include at least one material which is different from that of the base.

公开(公告)号：US20120195754A1

公开(公告)日：2012-08-02

申请号：US13389155

申请日：2010-07-05

Applicant: Bernd Hein ,  Christoph Heier

Inventor： Bernd Hein ,  Christoph Heier

IPC: F04D29/04

CPC classification number: F04D29/026 ,  F04D29/0462 ,  F04D29/047 ,  F05D2300/171 ,  F05D2300/43 ,  F05D2300/509 ,  F05D2300/512 ,  F05D2300/603

Abstract: The invention relates to an implementation of a fluid pump 1, particularly a water pump 1, wherein an impeller 11 comprising a plain bearing bush 12 is rotatably supported on a bearing pin 13. The impeller 11 and the plain bearing bush 12 are thereby made of an identical base material in one or more pieces. A further material is mixed into the base material of the plain bearing bush 12, improving the sliding properties of the plain bearing bush 12 on the bearing pin 13.

Abstract translation: 本发明涉及流体泵1，特别是水泵1的实施例，其中包括滑动轴承衬套12的叶轮11可旋转地支撑在轴承销13上。因此，叶轮11和滑动轴承衬套12由 一个或多个相同的基材。 将另外的材料混合到滑动轴承衬套12的基材中，从而改善滑动轴承衬套12在轴承销13上的滑动性能。

公开(公告)号：US08083469B1

公开(公告)日：2011-12-27

申请号：US12408016

申请日：2009-03-20

Applicant: Alex Pinera

Inventor： Alex Pinera

IPC: F01D11/00

CPC classification number: F01D25/18 ,  F01D25/16 ,  F05D2260/20 ,  F05D2300/509 ,  Y02T50/671 ,  Y02T50/676 ,  Y10S384/907

Abstract: A bearing lubrication system for a high temperature bearing, such as in a small gas turbine engine for a UAV, in which the bearing and lubricant requires a long shelf life, where the bearing includes a solid lubricant movable within a chamber formed within a housing and located adjacent to the bearing. The solid lubricant is biased by a spring toward the bearing and abuts against a runner that rotates along with the rotor shaft during engine operation. A cooling air passage opens into a space formed between the bearing and the solid lubricant to supply cooling air through the bearing. When the engine operates, heat is transferred through the runner to the solid lubricant to melt the lubricant. Rubbing of the runner against the biased solid lubricant will also melt the lubricant. The melting lubricant is carried by the cooling air through the bearing to provide both cooling and lubrication for the bearing.

Abstract translation: 一种用于高温轴承的轴承润滑系统，例如在用于UAV的小型燃气涡轮发动机中，其中轴承和润滑剂需要较长的保质期，其中轴承包括在形成于壳体内的室内可移动的固体润滑剂， 位于轴承附近。 固体润滑剂由弹簧朝向轴承偏置，并与发动机运转期间与转子轴一起转动的转轮抵接。 冷却空气通道通向轴承和固体润滑剂之间形成的空间，以通过轴承供应冷却空气。 当发动机运转时，热量通过流道传递到固体润滑剂以熔化润滑剂。 将润滑剂摩擦偏压的固体润滑剂也会使润滑剂熔化。 熔化润滑剂由冷却空气通过轴承承载，为轴承提供冷却和润滑。

公开(公告)号：US07823889B2

公开(公告)日：2010-11-02

申请号：US11663808

申请日：2005-03-30

Applicant: Kei Komukai ,  Tetsuya Iguchi ,  Hidetoshi Kasahara

Inventor： Kei Komukai ,  Tetsuya Iguchi ,  Hidetoshi Kasahara

IPC: F16J15/02

CPC classification number: F16J15/123 ,  F01D9/023 ,  F05D2230/311 ,  F05D2230/90 ,  F05D2300/14 ,  F05D2300/509 ,  F05D2300/611 ,  F16J15/065 ,  F16J15/0881 ,  Y02T50/671

Abstract: A seal part having a base material, a porous coating layer formed by flame spraying a hard material on a seal surface of the base material, and a lubricating film containing one or more types of materials selected from silver, gold, and tin and a gold-cobalt alloy on the porous coating layer. The seal part of the present invention has superior durability and sealability and further a long life and high reliability even when used in a high temperature (for example 400° C. or more, in particular 400 to 600° C.) and high pressure (for example 2 MPa or more) environment.

Abstract translation: 具有基材的密封部分，通过在基材的密封表面上火焰喷涂硬质材料形成的多孔涂层，以及含有选自银，金，锡和金的一种或多种材料的润滑膜 钴合金在多孔涂层上。 本发明的密封部分具有优异的耐久性和密封性，并且即使在高温（例如400℃以上，特别是400〜600℃）和高压（例如400℃以上）下使用时，寿命长， 例如2MPa以上）环境。

公开(公告)号：US20100086398A1

公开(公告)日：2010-04-08

申请号：US12558950

申请日：2009-09-14

Applicant: Hiroyuki Ochiai ,  Mitsutoshi Watanabe ,  Mikiya Arai ,  Shigeru Saburi ,  Eiji Nakayama ,  Akihiro Goto ,  Masao Akiyoshi

Inventor： Hiroyuki Ochiai ,  Mitsutoshi Watanabe ,  Mikiya Arai ,  Shigeru Saburi ,  Eiji Nakayama ,  Akihiro Goto ,  Masao Akiyoshi

IPC: F01D9/00 ,  F01D5/14 ,  F02C7/00

CPC classification number: C23C26/00 ,  B32B15/04 ,  C22C19/07 ,  C23C4/06 ,  C23C30/00 ,  F01D5/288 ,  F05D2300/509 ,  Y02T50/67 ,  Y10T428/12937

Abstract: A sliding surface of a high-temperature portion is subjected to an electro-discharge surface treatment with one or both of a high-temperature hard material (4) and a material having a lubricating property at a high temperature (6). The high-temperature hard material (4) is any or a mixture of cBN, TiC, TiN, TiAlN, TiB2, WC, Cr3C2, SiC, ZrC, VC, B4C, Si3N4, ZrO2, and Al2O3. The material having the lubricating property at the high temperature (6) contains chromium and/or chromium oxide (Cr2O3) and/or hexaboron nitride (hBN). An electrode formed by compression molding of the high-temperature hard material, and the high-temperature lubricating material containing at least one of Cr and hBN and having the lubricating property at the high temperature is used as the electrode for the electro-discharge surface treatment.

Abstract translation: 用高温硬质材料（4）和具有高温润滑性的材料（6）中的一种或两种对高温部分的滑动表面进行放电表面处理。 高温硬质材料（4）是cBN，TiC，TiN，TiAlN，TiB 2，WC，Cr 3 C 2，SiC，ZrC，VC，B 4 C，Si 3 N 4，ZrO 2和Al 2 O 3的任何或混合物。 具有高温润滑性的材料（6）含有铬和/或氧化铬（Cr 2 O 3）和/或六氮化硼（hBN）。 使用通过高温硬质材料的压缩成型而形成的电极以及含有Cr和hBN中的至少一种且具有高温润滑性的高温润滑材料作为放电表面处理用电极 。

公开(公告)号：US07572313B2

公开(公告)日：2009-08-11

申请号：US11127524

申请日：2005-05-10

Applicant: Thirumalai G. Palanisamy ,  Surojit Gupta ,  Michel Barsoum ,  Chien-Wei Li

Inventor： Thirumalai G. Palanisamy ,  Surojit Gupta ,  Michel Barsoum ,  Chien-Wei Li

IPC: C22C29/02 ,  C22C29/16

CPC classification number: F01D5/28 ,  B22F2998/10 ,  C22C29/06 ,  C22C29/16 ,  F05D2220/40 ,  F05D2230/90 ,  F05D2300/509 ,  F05D2300/603 ,  F05D2300/611 ,  F16C17/02 ,  F16C33/121 ,  F16C2360/24 ,  Y10T428/12576 ,  B22F3/02 ,  B22F3/1035 ,  B22F3/15

Abstract: A turbomachinery component includes a substrate having a surface, the surface consisting essentially of at least one composite of at least one metal and at least one compound having the chemical formula Mn+1AXn, wherein M is at least one early transition metal selected from groups IIIB, IVB, VB, and VIB, A is at least one element selected from groups IIIA, IVA, VA, VIA, and VIIA, X is one or both of carbon and nitrogen, and n is an integer between 1 and 3. The component is made by compressing a powdered material to form a substrate that consists essentially of the composite and sintering the substrate, or by coating a substrate with the composite.

Abstract translation: 涡轮机械部件包括具有表面的基底，该表面基本上由至少一种金属和至少一种具有化学式Mn + 1AXn的化合物的复合材料组成，其中M是选自IIIB族的至少一种早期过渡金属 ，IVB，VB和VIB，A是选自IIIA，IVA，VA，VIA和VIIA族中的至少一种元素，X是碳和氮之一或两者，n是1和3之间的整数。 通过压缩粉末材料以形成基本上由复合材料组成并烧结基材，或通过用复合材料涂覆基材来制备。

公开(公告)号：US20070284828A1

公开(公告)日：2007-12-13

申请号：US11663808

申请日：2005-03-30

Applicant: Kei Komukai ,  Tetsuya Iguchi ,  Hidetoshi Kasahara

Inventor： Kei Komukai ,  Tetsuya Iguchi ,  Hidetoshi Kasahara

IPC: F16J15/06

CPC classification number: F16J15/123 ,  F01D9/023 ,  F05D2230/311 ,  F05D2230/90 ,  F05D2300/14 ,  F05D2300/509 ,  F05D2300/611 ,  F16J15/065 ,  F16J15/0881 ,  Y02T50/671

Abstract: A seal part having a base material, a porous coating layer formed by flame spraying a hard material on a seal surface of the base material, and a lubricating film containing one or more types of materials selected from silver, gold, and tin and a gold-cobalt alloy on the porous coating layer. The seal part of the present invention has superior durability and sealability and further a long life and high reliability even when used in a high temperature (for example 400° C. or more, in particular 400 to 600° C.) and high pressure (for example 2 MPa or more) environment.

Abstract translation: 具有基材的密封部分，通过在基材的密封表面上火焰喷涂硬质材料形成的多孔涂层，以及含有选自银，金，锡和金的一种或多种材料的润滑膜 钴合金在多孔涂层上。 本发明的密封部分具有优异的耐久性和密封性，并且即使在高温（例如400℃以上，特别是400〜600℃）和高压（例如400℃以上）下使用时，寿命长， 例如2MPa以上）环境。

公开(公告)号：US20070140853A1

公开(公告)日：2007-06-21

申请号：US11314147

申请日：2005-12-21

Applicant: Michael McCann ,  Sang Park

Inventor： Michael McCann ,  Sang Park

IPC: F01D11/00

CPC classification number: F01D5/3092 ,  C23C4/04 ,  C23C30/00 ,  F04D29/023 ,  F04D29/322 ,  F05D2220/326 ,  F05D2220/327 ,  F05D2230/90 ,  F05D2300/1723 ,  F05D2300/509 ,  F05D2300/611 ,  Y02T50/673 ,  Y10T29/49327 ,  Y10T29/49336

Abstract: A gas turbine engine blade having a dovetail with an enhanced surface for durability is disclosed. The blade includes an airfoil section and a dovetail section disposed opposite the airfoil section. The dovetail section has an outer surface, at least a portion of which has residual compressive stresses resulting from a plurality of peening operations. The dovetail section also includes a copper-nickel-indium wear coating layer disposed over the outer surface having residual compressive stresses and a lubricant coating layer disposed over the copper-nickel-indium wear coating layer, wherein the lubricant coating layer is lead-free.

Abstract translation: 公开了一种具有燕尾形的燃气涡轮发动机叶片，其具有增强的耐久性表面。 叶片包括翼型部分和与翼型部分相对设置的燕尾部分。 燕尾部分具有外表面，其至少一部分具有由多个喷丸操作产生的残余压应力。 燕尾部分还包括设置在具有残余压缩应力的外表面上的铜镍铟耐磨涂层和设置在铜 - 镍 - 铟耐磨涂层上的润滑剂涂层，其中润滑剂涂层是无铅的。

公开(公告)号：US07094022B2

公开(公告)日：2006-08-22

申请号：US10445428

申请日：2003-05-27

Applicant: Robert W. Bruce

Inventor： Robert W. Bruce

IPC: F01D17/16

CPC classification number: F01D17/162 ,  F05D2230/90 ,  F05D2300/21 ,  F05D2300/2283 ,  F05D2300/509 ,  F05D2300/611 ,  F16C33/043 ,  F16C2360/23 ,  Y02T50/671

Abstract: Materials, heretofore unknown for use in bearing assemblies, which produce equal or better wear resistance at reduced materials cost have been identified. These alternatives fall into three general categories: (1) solid materials from which bushings and washers can be fabricated, (2) coatings bonded to metallic bushings and/or vanes to minimize total system wear, and (3) solid lubricant coatings placed on any bushing or vane stem to reduce friction.

Abstract translation: 已经确定了迄今为止未知的用于轴承组件的材料，其以降低的材料成本产生相等或更好的耐磨性。 这些替代品分为三个一般类别：（1）可以制造衬套和垫圈的固体材料，（2）粘合到金属衬套和/或叶片上的涂层以最小化系统的总体磨损，以及（3）固体润滑剂涂层放置在任何 衬套或叶片杆以减少摩擦。