| 发明名称 |
HARDENED TITANIUM ALLOY AND METHOD OF MAKING THE SAME |
| 摘要 |
According to an exemplary embodiment, a gas turbine element made of a hardened titanium alloy may be provided. The hardened titanium alloy may be made by a process which may include but may not be limited to, obtaining an element made of titanium alloy, treating a surface of the element made of titanium alloy with beryllium using diffusion process, and forming a titanium beryllide diffusion layer to a predetermined depth from the surface. |
| 申请公布号 |
US2017101720(A1) |
申请公布日期 |
2017.04.13 |
| 申请号 |
US201514878031 |
申请日期 |
2015.10.08 |
| 申请人 |
CSA Group LLC. |
发明人 |
HURST William D.;CAUTHREN Glenn E. |
| 分类号 |
C25D3/66;C23C16/06;C22C14/00;C25D11/00 |
主分类号 |
C25D3/66 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine element for a gas turbine engine comprising:
a hardened titanium alloy comprise a titanium beryllide layer diffused to a predetermined depth from the surface of the turbine element of from approximately 0.0005 inch to approximately 0.001 inch. |
| 地址 |
Port St. Lucie FL US |
