公开(公告)号：EP1035326B1

公开(公告)日：2006-06-07

申请号：EP00104789.3

申请日：2000-03-06

Applicant: KABUSHIKI KAISHA TOYOTA JIDOSHOKKI

Inventor： Takenaka, Kenji ,  Kato, Keiichi ,  Kurita, Hajime ,  Kurakake, Hirotaka

IPC: F04B27/08 ,  F04B27/10

CPC classification number: F04B27/0886 ,  F04B27/0878 ,  F04B27/1054 ,  F05C2201/0469 ,  F05C2201/0493 ,  F05C2203/0804 ,  F05C2203/0808 ,  F05C2203/0856 ,  F05C2203/086 ,  F05C2225/04 ,  F05C2253/12

公开(公告)号：EP1375701A1

公开(公告)日：2004-01-02

申请号：EP03253256.6

申请日：2003-05-23

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Bruce, Robert William

IPC: C23C28/00 ,  F01D5/28

CPC classification number: C23C28/321 ,  C23C14/083 ,  C23C28/3215 ,  C23C28/325 ,  C23C28/345 ,  C23C28/3455 ,  F01D5/288 ,  F05C2201/0469 ,  F05D2230/90 ,  F05D2300/134 ,  F05D2300/15 ,  F05D2300/611 ,  Y10T428/12611 ,  Y10T428/12944

Abstract: A coating material, particularly a thermal barrier coating (26), for a component comprising a substrate (22) and a bond coat (24) intended for use in a hostile environment, such as the superalloy turbine, combustor and augmentor components of a gas turbine engine. The coating material is zirconia that is partially stabilized with yttria and to which lanthana, neodymia and/or tantala are alloyed to increase the impact resistance of the coating.

Abstract translation: 一种用于包括用于恶劣环境的基底（22）和粘合涂层（24）的部件的涂层材料，特别是热障涂层（26），例如超级合金涡轮，燃烧器和气体的增强部件 涡轮发动机。 涂层材料是用氧化钇部分稳定的氧化锆，并且将氧化镧，钕和/或钽酸铝合金化以增加涂层的耐冲击性。

公开(公告)号：EP1292656A1

公开(公告)日：2003-03-19

申请号：EP01940643.8

申请日：2001-05-30

Applicant: GE Energy Products France SNC

Inventor： MOLIERE, Michel ,  ROCCA, Emmanuel ,  STEINMETZ, Pierre

IPC: C10L1/12 ,  C10L1/24 ,  C10L1/18 ,  C10L1/10 ,  C10L10/04 ,  C10L3/00 ,  F02C7/30 ,  F01D25/00 ,  F02B77/04

CPC classification number: C10L1/1828 ,  C10L1/10 ,  C10L1/12 ,  C10L1/1233 ,  C10L1/125 ,  C10L1/1266 ,  C10L1/1275 ,  C10L1/1616 ,  C10L1/188 ,  C10L1/1881 ,  C10L1/1985 ,  C10L1/2437 ,  C10L3/003 ,  C10L10/04 ,  F01D25/002 ,  F01D25/007 ,  F02B77/04 ,  F02C7/30 ,  F05C2201/0466 ,  F05C2201/0469

Abstract: The invention concerns inhibition of vanadium corrosion of thermal equipment materials burning vanadium-contaminated liquid fuels using nickel compounds. The invention is applicable in particular to liquid fuel combustion in gas turbines.

公开(公告)号：EP1116881A1

公开(公告)日：2001-07-18

申请号：EP00946476.9

申请日：2000-07-25

Applicant: Kabushiki Kaisha Toyoda Jidoshokki Seisakusho

Inventor： HIRAYAMA, Seizo KK Toyoda Jidoshokki Seisakusho ,  SUGIURA, Manabu, KK Toyoda Jidoshokki Seisakusho ,  IWAMA, Kazuaki KK Toyoda Jidoshokki Seisakusho ,  SUZAKI, Seiji Izumi Machine Mfg, Co., Ltd.

IPC: F04B27/08 ,  C23C26/00

CPC classification number: C23C26/02 ,  C23C24/02 ,  F04B27/1054 ,  F05C2201/0469 ,  F05C2253/12

Abstract: A method of forming a coating on a work surface of a machine component. The method includes a preparatory step of preparing a feed form formed of a metal material that is softer than at least a work surface of a machine component, a pressure-welding step of pressure-welding an end face of the feed form to the work surface of the machine component while causing relative rotation between the machine component and the feed form, to join the feed form to the machine component, and a cutting step of cutting the feed form in a direction substantially orthogonal to an axis of the relative rotation at a portion near a joining position at which the machine component and the feed form are joined, to add a soft metal layer having a predetermined thickness to the work surface of the machine component.

Abstract translation: 一种在机器部件的工作表面上形成涂层的方法。 该方法包括准备步骤，准备由比机械部件的至少工作面更软的金属材料形成的进给形式，将进给形式的端面压焊到工作表面的压接步骤 的机器部件，同时引起机器部件和进给形式之间的相对旋转，以将进给形式连接到机器部件;以及切割步骤，其在基本上垂直于相对旋转的轴线的方向上切割进给形式 在机器部件和进给形式接合的接合位置附近的部分，将具有预定厚度的软金属层添加到机器部件的工作表面。