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公开(公告)号：US20020044870A1
公开(公告)日：2002-04-18
申请号：US09813626
申请日：2001-03-19
Applicant: Honeywell International, Inc.
Inventor： Joseph Simonetti , Bruce Wilson
IPC: F01D005/32
CPC classification number: F01D5/28 , F01D5/3092 , F05C2201/0463 , F05D2230/90 , F05D2250/71 , F05D2260/30 , F05D2300/611
Abstract: A compliant shim for use between the root of a gas turbine fan blade and a dovetail groove in a gas turbine rotor disk to reduce fretting therebetween. The compliant shim has first and second slots for engaging tabs extending from the fan blade root. The slots and tabs cooperate to hold the shim during engine operation. An oxidation layer covers the compliant shim. The shim is augmented with an upstanding wall and a seal element to seal the gap that exists between platform edges of adjacent fan blades. This simple combination solves two complex problems, fatigue of fan assembly parts and loss of operating efficiency caused by fluid flow leakage.
Abstract translation: 用于在燃气轮机风扇叶片的根部和燃气涡轮机转子盘中的燕尾槽之间使用的柔性垫片以减少它们之间的微动。 顺应垫片具有第一和第二槽，用于接合从风扇叶片根延伸的突出部。 在发动机运行期间，槽和接头配合起来保持垫片。 氧化层覆盖柔顺垫片。 垫片被增强了一个直立的墙壁和密封元件，以密封相邻风扇叶片的平台边缘之间存在的间隙。 这种简单的组合解决了两个复杂的问题，风扇组件的疲劳和流体泄漏导致的运行效率的损失。
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72.发明授权In-situ formation of multiphase electron beam physical vapor deposited barrier coatings for turbine components 有权用于涡轮机部件的多相电子束物理气相沉积阻挡涂层的原位形成公开(公告)号：US06296945B1
公开(公告)日：2001-10-02
申请号：US09393415
申请日：1999-09-10
Applicant: Ramesh Subramanian
Inventor： Ramesh Subramanian
IPC: B32B900
CPC classification number: C23C14/5846 , C23C14/083 , C23C28/3215 , C23C28/345 , C23C28/3455 , F01D5/288 , F05C2201/0463 , F05C2201/0466 , F05D2230/90 , F05D2300/21 , F05D2300/611 , Y02E20/16 , Y10S428/937
Abstract: A turbine component (10), such as a turbine blade, is provided which is made of a metal alloy (22) and a base columnar thermal barrier coating (20) on the alloy surface, where a heat resistant ceramic oxide sheath material (32′ or 34′) covers the columns (28), and the sheath material is the reaction product of a precursor ceramic oxide sheath material and the base thermal barrier coating material.
Abstract translation: 提供涡轮机部件（10），例如涡轮叶片，其由合金表面上的金属合金（22）和基体柱状热障涂层（20）制成，其中耐热陶瓷氧化物护套材料（32 '或34'）覆盖柱（28），护套材料是前体陶瓷氧化物护套材料与基底热障涂层材料的反应产物。
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公开(公告)号：US06207295B1
公开(公告)日：2001-03-27
申请号：US09353031
申请日：1999-07-13
Applicant: William R. Stowell , Ching-Pang Lee , John F. Ackerman , George A. Durgin , Robert W. Harris
Inventor： William R. Stowell , Ching-Pang Lee , John F. Ackerman , George A. Durgin , Robert W. Harris
IPC: B32B1500
CPC classification number: C23C28/3215 , C23C28/321 , C23C28/345 , C23C28/3455 , C23C28/36 , C23C28/42 , F01D5/288 , F05C2201/0463 , F05C2201/0466 , F05D2230/90 , F05D2300/121 , F05D2300/132 , F05D2300/211 , F05D2300/2112 , F05D2300/611 , Y02T50/672 , Y02T50/673 , Y10T428/12493 , Y10T428/12576 , Y10T428/12674 , Y10T428/12771 , Y10T428/12826 , Y10T428/12833
Abstract: A coated article comprises a substrate, an inner environmental resistant coating portion including Al on the substrate, and an outer heat energy reflecting and oxygen diffusion inhibiting coating portion outward of the inner portion. The outer coating portion is multi-layer, comprising 6-48 discrete stacked layers and a total outer coating portion thickness in the range of about 2.5-25 microns.
Abstract translation: 涂布制品包括基材，在基材上包含Al的内部耐环境涂层部分和外部热能反射和氧扩散抑制涂层部分在内部外部。 外涂层部分是多层的，包括6-48个分立的堆叠层，总外涂层部分厚度在约2.5-25微米的范围内。
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公开(公告)号：US6136454A
公开(公告)日：2000-10-24
申请号：US317460
申请日：1999-05-24
Applicant: Carl Edward Cordy
Inventor： Carl Edward Cordy
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: An aluminum or aluminum alloy surface which during use is exposed to sliding friction is coated to provide a chemical conversion coating of tin comprising 0.2-10.0 wt. % cobalt. For example, a swash plate type compressor has 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 has a coating preferably between 0.8 to 2.5 microns. 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: 在使用期间暴露于滑动摩擦的铝或铝合金表面被涂覆以提供包含0.2-10.0重量％的锡的化学转化涂层。 ％钴。 例如，斜盘式压缩机具有气缸体，缸体具有平行于气缸体的轴线设置的气缸孔。 可旋转地安装在气缸体内的旋转轴携带铝斜盘。 旋转斜盘具有优选在0.8至2.5微米之间的涂层。 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。
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75.发明授权Structural component made of metal or ceramic having a solid outer shell and a porous core and its method of manufacture 失效由具有固体外壳和多孔芯的金属或陶瓷制成的结构部件及其制造方法
公开(公告)号：US5634189A
公开(公告)日：1997-05-27
申请号：US339394
申请日：1994-11-14
Applicant: Axel Rossmann , Wilfried Smarsly
Inventor： Axel Rossmann , Wilfried Smarsly
CPC classification number: B22F7/004 , B22F3/1109 , B22F3/1112 , F01D5/147 , F01D5/28 , B22F2998/00 , B22F2999/00 , F05C2201/0463 , F05C2201/0466 , F05D2300/612 , Y10T428/12021 , Y10T428/12028 , Y10T428/12035 , Y10T428/12042 , Y10T428/12049 , Y10T428/12056 , Y10T428/12063 , Y10T428/12069 , Y10T428/1209 , Y10T428/12097 , Y10T428/12153
Abstract: A structural component is formed with an outer shell of sintered, solid, powder particles, and a porous core of sintered, hollow, bodies arranged in layers. The hollow bodies are of increased diameter in the layers in a direction from the outer periphery of the core towards the center of the core. The material of the outer shell and of the core is a metal or ceramic.
Abstract translation: 结构部件由烧结的，固体的粉末颗粒的外壳和被排列成层的烧结的中空的多孔芯形成。 中空体在从芯的外周向芯的中心的方向上在层中具有增加的直径。 外壳和芯的材料是金属或陶瓷。
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Patent Agency Ranking
公开(公告)号：US20160341249A1
公开(公告)日：2016-11-24
申请号：US15156418
申请日：2016-05-17
Inventor： Eunsoo YANG , Bumdong SA , Byeongchul LEE , Eunsoo PARK , Wookha RYU
CPC classification number: F16C33/1095 , C22C45/001 , C22C45/04 , C22C45/10 , F04C18/0215 , F04C18/34 , F04C23/008 , F04C29/0021 , F04C29/02 , F04C29/023 , F04C2230/91 , F05C2201/021 , F05C2201/0412 , F05C2201/0415 , F05C2201/0463 , F05C2201/0466 , F05C2203/0813 , F05C2203/083 , F05C2253/06 , F05C2253/08 , F05C2253/12 , F16C17/02 , F16C33/121 , F16C33/124 , F25B31/002 , F25B31/026
Abstract: A lubricating layer having wear resistance and reliability on the wear resistance, and a compressor including a lubricating layer are provided. The compressor may include a lubricating layer coated on a frictional portion between a rotational shaft and a bearing. The lubricating layer may include at least one metal phase selected from a group consisting of Titanium (Ti); and Copper (Cu), Cobalt (Co), Nickel (Ni), and Zirconium (Zr), and may be a composite structure of amorphous and nanocrystalline materials.
Abstract translation: 提供了具有耐磨性和耐磨性可靠性的润滑层，以及包括润滑层的压缩机。 压缩机可以包括涂覆在旋转轴和轴承之间的摩擦部分上的润滑层。 润滑层可以包括至少一种金属相，其选自钛（Ti）; 和铜（Cu），钴（Co），镍（Ni）和锆（Zr），并且可以是非晶和纳米晶体材料的复合结构。
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77.发明授权公开(公告)号：US08808872B2
公开(公告)日：2014-08-19
申请号：US13638938
申请日：2011-04-06
Applicant: Michael Ott , Sebastian Piegert , Peter Randelzhofer , Robert Singer
Inventor： Michael Ott , Sebastian Piegert , Peter Randelzhofer , Robert Singer
CPC classification number: F01D5/005 , B23K35/22 , B23K35/3033 , F05C2201/025 , F05C2201/0463 , F05C2201/0466 , F05D2300/131 , Y02T50/67 , Y10T428/12931 , Y10T428/12944
Abstract: A germanium containing nickel-based solder having a similar composition to a nickel-based superalloy is provided. As a result of which the proportion of γ′ formed in the solder is reduced. The solder also includes chromium, cobalt, molybdenum, tungsten, aluminum, and titanium. A component including the solder is also provided.
Abstract translation: 提供了与镍基超级合金具有相似组成的含锗镍基焊料。 结果，焊料中形成的γ'的比例降低。 焊料还包括铬，钴，钼，钨，铝和钛。 还提供了包括焊料的部件。
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公开(公告)号：US20130206287A1
公开(公告)日：2013-08-15
申请号：US13816905
申请日：2011-08-15
Applicant: Jun Sato , Shinya Imano , Mototsugu Osaki , Shigeki Ueta , Kiyohito Ishida , Toshihiro Omori , Hiroaki Nishida , Masahiro Hayashi , Tomoki Shiota
Inventor： Jun Sato , Shinya Imano , Mototsugu Osaki , Shigeki Ueta , Kiyohito Ishida , Toshihiro Omori , Hiroaki Nishida , Masahiro Hayashi , Tomoki Shiota
CPC classification number: C22F1/10 , C22C19/055 , C22C19/056 , C22C19/057 , C22C30/00 , F01D5/28 , F05C2201/0463 , F05D2300/17 , Y02T50/671
Abstract: A Co-based alloy containing not less than 0.001 mass % and less than 0.100 mass % of C, not less than 9.0 mass % and less than 20.0 mass % of Cr, not less than 2.0 mass % and less than 5.0 mass % of Al, not less than 13.0 mass % and less than 20.0 mass % of W, and not less than 39.0 mass % and less than 55.0 mass % of Ni, with the remainder being made up by Co and unavoidable impurities, wherein the contents of Mo, Nb, Ti and Ta which are included in the unavoidable impurities are as follows: Mo
Abstract translation: 含有不小于0.001质量％且小于0.100质量％的C，不小于9.0质量％且小于20.0质量％的Cr的Co基合金，不小于2.0质量％且小于5.0质量％的Al ，不小于13.0质量％且小于20.0质量％的W，不小于39.0质量％且小于55.0质量％的Ni，其余由Co和不可避免的杂质构成，其中Mo， 包含在不可避免的杂质中的Nb，Ti和Ta如下：Mo <0.010质量％，Nb <0.010质量％，Ti <0.010质量％，Ta <0.010质量％。
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79.发明申请GERMANIUM-CONTAINING SOLDER, A COMPONENT COMPRISING A SOLDER AND A PROCESS FOR SOLDERING 有权含锗的焊接机，包括焊接件的组件和焊接工艺公开(公告)号：US20130029179A1
公开(公告)日：2013-01-31
申请号：US13638938
申请日：2011-04-06
Applicant: Michael Ott , Sebastian Piegert , Peter Randelzhofer , Robert Singer
Inventor： Michael Ott , Sebastian Piegert , Peter Randelzhofer , Robert Singer
CPC classification number: F01D5/005 , B23K35/22 , B23K35/3033 , F05C2201/025 , F05C2201/0463 , F05C2201/0466 , F05D2300/131 , Y02T50/67 , Y10T428/12931 , Y10T428/12944
Abstract: A germanium containing nickel-based solder having a similar composition to a nickel-based superalloy is provided. As a result of which the proportion of γ′ formed in the solder is reduced. The solder also includes chromium, cobalt, molybdenum, tungsten, aluminum, and titanium. A component including the solder is also provided.
Abstract translation: 提供了与镍基超级合金具有相似组成的含锗镍基焊料。 结果，焊料中形成的γ'的比例降低。 焊料还包括铬，钴，钼，钨，铝和钛。 还提供了包括焊料的部件。
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公开(公告)号：US20120084980A1
公开(公告)日：2012-04-12
申请号：US12902902
申请日：2010-10-12
Applicant: Warren Miglietti , John Roderick
Inventor： Warren Miglietti , John Roderick
IPC: B23P6/00
CPC classification number: B23P6/045 , B23K35/007 , B23K35/3046 , C21D6/007 , C21D9/50 , C22C19/07 , C22F1/10 , C22F1/18 , F01D5/286 , F01D9/02 , F05C2201/0463 , F05D2230/40 , F05D2300/13 , Y10T29/49318
Abstract: A method of extending the useable life of a gas turbine component fabricated from a cobalt-based alloy is disclosed. The method includes applying a rejuvenation process to the alloy where the alloy is placed in a protected atmosphere and heated to three different elevated temperatures and held at the elevated temperatures for approximately four hours each. Application of the rejuvenation process allows gas turbine components to be returned to service for at least one more service interval of approximately 24,000 operating hours.
Abstract translation: 公开了一种延长由钴基合金制成的燃气轮机部件的使用寿命的方法。 该方法包括将合金置于受保护的气氛中并加热到三种不同的升高温度并在高温下保持大约四个小时的合金应用复原过程。 复原过程的应用使得燃气轮机组件能够返回服务至少一个更多的服务间隔大约24,000个工作小时。
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