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公开(公告)号:US07575418B2
公开(公告)日:2009-08-18
申请号:US10955056
申请日:2004-09-30
申请人: Michael Francis Xavier Gigliotti , Canan Uslu Hardwicke , Liang Jiang , Don Mark Lipkin , Samuel Vinod Thamboo
发明人: Michael Francis Xavier Gigliotti , Canan Uslu Hardwicke , Liang Jiang , Don Mark Lipkin , Samuel Vinod Thamboo
CPC分类号: B23K20/08 , B23P6/005 , B23P6/007 , C23C4/08 , C23C4/18 , C23C24/087 , C23C24/106 , C23C28/021 , C23C28/023 , C23C30/00 , F01D5/288 , F05D2230/90 , F05D2300/133 , F05D2300/611 , Y02T50/671 , Y10S428/937 , Y10S428/938 , Y10S428/939 , Y10S428/94 , Y10T428/12639 , Y10T428/12806 , Y10T428/12868 , Y10T428/12944 , Y10T428/31953
摘要: Disclosed herein is a turbine component comprising a substrate; and a protective structure formed on the substrate, wherein the protective structure comprises an α-β titanium alloy, a β-titanium alloy or a near-β titanium alloy. Disclosed herein too is a process for providing a protective structure to a turbine component, comprising affixing a protective structure on a turbine component; wherein the protective structure comprises an α-β titanium alloy, a near-β titanium alloy or a β-titanium alloy.
摘要翻译: 本文公开了一种包括基底的涡轮机部件; 以及形成在基底上的保护结构,其中保护结构包括α-β钛合金,β-钛合金或近β钛合金。 本文还公开了一种用于向涡轮机部件提供保护结构的方法,包括将保护结构固定在涡轮机部件上; 其中保护结构包括α-β钛合金,近β钛合金或β-钛合金。