公开(公告)号：US20070141374A1

公开(公告)日：2007-06-21

申请号：US11311035

申请日：2005-12-19

申请人： David P. Mourer ,  Kenneth R. Bain

发明人： David P. Mourer ,  Kenneth R. Bain

IPC分类号： B05D3/00 ,  B05D3/04 ,  B05D3/10 ,  B22F7/00

CPC分类号： B22F1/025 ,  B22F2003/248 ,  B22F2998/10 ,  B22F2999/00 ,  C22C1/0416 ,  C22C1/0433 ,  C22C1/0458 ,  C22C19/03 ,  C22C19/051 ,  C22C33/0285 ,  Y10T428/12021 ,  Y10T428/12028 ,  Y10T428/12944 ,  B22F3/02 ,  B22F3/24 ,  B22F9/28

摘要： An environmentally resistant gas turbine engine disk is disclosed. The disk includes a substrate metal having locally enriched surface regions, the locally enriched surface regions comprising alloying elements present in a higher percentage than found in the substrate metal. A method for making the disk and other articles is also disclosed. The method includes furnishing a plurality of powder particle substrates made of a substrate metal, providing a nonmetallic precursor of a metallic coating material, wherein the metallic coating material includes an alloying element that is thermophysically melt incompatible with the substrate metal, contacting the powder particle substrates with the nonmetallic precursor, and chemically reducing the nonmetallic precursor to form coated powder particles comprising the powder particle substrates having a surface-enriched layer of the metallic coating material thereon, wherein the step of chemically reducing is performed without melting the powder particle substrates.

摘要翻译： 公开了一种耐环境燃气涡轮发动机盘。 盘包括具有局部富集的表面区域的基底金属，局部富集的表面区域包含比在底物金属中发现的百分比更高的合金元素。 还公开了制造盘和其它制品的方法。 该方法包括提供由基底金属制成的多个粉末颗粒基底，提供金属涂层材料的非金属前体，其中该金属涂层材料包括与该基底金属不相容的热物理熔融的合金元素，使该粉末颗粒基片 与非金属前驱体一起化学还原非金属前体，形成包含其上具有金属涂层材料的表面富集层的粉末颗粒基底的涂覆粉末颗粒，其中化学还原步骤不熔化粉末颗粒基底。

公开(公告)号：US06521175B1

公开(公告)日：2003-02-18

申请号：US09021040

申请日：1998-02-09

申请人： David P. Mourer ,  Eric S. Huron ,  Kenneth R. Bain ,  Enrique E. Montero ,  Paul L. Reynolds ,  John J. Schirra

发明人： David P. Mourer ,  Eric S. Huron ,  Kenneth R. Bain ,  Enrique E. Montero ,  Paul L. Reynolds ,  John J. Schirra

IPC分类号： C22C1905

CPC分类号： C22C19/057 ,  B22F2998/10 ,  C22C1/0441 ,  C22C19/056 ,  B22F3/17 ,  B22F9/082 ,  B22F3/02 ,  B22F3/20

摘要： A superalloy has a composition of, in weight percent, from about 16.0 percent to about 22.4 percent cobalt, from about 6.6 percent to about 14.3 percent chromium, from about 1.4 percent to about 3.5 percent tantalum, from about 1.9 percent to about 4.0 percent tungsten, from about 1.9 percent to about 3.9 percent molybdenum, from about 0.03 percent to about 0.10 percent zirconium, from about 0.9 percent to about 3.0 percent niobium, from about 2.4 percent to about 4.6 percent titanium, from about 2.6 percent to about 4.8 percent aluminum, from 0 to about 2.5 percent rhenium, from about 0.02 percent to about 0.10 percent carbon, from about 0.02 percent to about 0.10 percent boron, balance nickel and minor amounts of impurities. The superalloy is advantageously utilized in aircraft gas turbine disks.

摘要翻译： 超级合金的重量百分比为约16.0％至约22.4％的钴，约6.6％至约14.3％的铬，约1.4％至约3.5％的钽，约1.9％至约4.0％的钨 ，约1.9％至约3.9％的钼，约0.03％至约0.10％的锆，约0.9％至约3.0％的铌，约2.4％至约4.6％的钛，约2.6％至约4.8％的铝 ，0至约2.5％的铼，约0.02％至约0.10％的碳，约0.02％至约0.10％的硼，余量为镍和少量杂质。 超级合金有利地用于飞机燃气轮机盘。