发明名称 |
Method for making a compositionally graded gas turbine disk |
摘要 |
<p>A compositionally graded gas turbine disk (20) is made by preparing a rotationally symmetric radially inner segment (28) of a gas turbine disk preform, rotating the inner segment about a central axis (24), spray applying a radially outer-segment material onto the radially inner segment (28) as it rotates about the central axis (24), preferably achieving a gradual transition in composition, and thereafter further processing the gas turbine disk preform to produce the compositionally graded gas turbine disk (20).</p> |
申请公布号 |
EP1724439(A2) |
申请公布日期 |
2006.11.22 |
申请号 |
EP20060252482 |
申请日期 |
2006.05.11 |
申请人 |
THE GENERAL ELECTRIC COMPANY |
发明人 |
GROH, JOHN RAYMOND;OTT, ERIC ALLEN;SCHAFRIK, ROBERT EDWARD;KRUEGER, DANIEL DONALD |
分类号 |
F01D5/02;B22F3/00;B22F3/12;B22F5/00;B22F7/06;B23P15/00;F01D25/00 |
主分类号 |
F01D5/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|