发明授权
US07718280B2 Method for the treatment of the tip of a turbine blade and a turbine blade treated with a method such as this 有权
用这种方法处理涡轮叶片和涡轮叶片的尖端的方法

  • 专利标题: Method for the treatment of the tip of a turbine blade and a turbine blade treated with a method such as this
  • 专利标题(中): 用这种方法处理涡轮叶片和涡轮叶片的尖端的方法
  • 申请号: US11485387
    申请日: 2006-07-13
  • 公开(公告)号: US07718280B2
    公开(公告)日: 2010-05-18
  • 发明人: Scott Wilson
  • 申请人: Scott Wilson
  • 申请人地址: US NY Westbury
  • 专利权人: Sulzer Metco (US), Inc.
  • 当前专利权人: Sulzer Metco (US), Inc.
  • 当前专利权人地址: US NY Westbury
  • 代理机构: Greenblum & Bernstein, P.L.C.
  • 优先权: EP05405436 20050714
  • 主分类号: B32B9/00
  • IPC分类号: B32B9/00
Method for the treatment of the tip of a turbine blade and a turbine blade treated with a method such as this
摘要:
A surface having an abrasive coating which includes silicon carbide (SiC) particles bound to the surface so as to form the abrasive coating. The SiC particles include a self-healing barrier layer that is in contact with an outer surface of the SiC particles. The self-healing barrier layer prevents degradation of the SiC particles.
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