| 发明名称 |
Process for machining axial blade slots in turbine disks for jet engines |
| 摘要 |
A process for machining axial blade slots in turbine disks used in jet engines is provided. The process broadly includes the steps of providing a turbine disk, forming a roughened slot having a plurality of joined rectangular areas in the turbine disk, and machining the roughened slot to a finished slot.
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| 申请公布号 |
US2005086804(A1) |
申请公布日期 |
2005.04.28 |
| 申请号 |
US20040899886 |
申请日期 |
2004.07.26 |
| 申请人 |
PACKMAN ALLAN B.;VAILLETTE BERNARD D. |
发明人 |
PACKMAN ALLAN B.;VAILLETTE BERNARD D. |
| 分类号 |
B21D28/28;B23C3/30;B23C3/34;B23P13/02;B23P15/00;B24B1/00;B24B19/02;B24B19/14;F01D5/02;F01D5/28;F01D5/30;F02C7/00;(IPC1-7):B21C37/30;B24B39/00 |
主分类号 |
B21D28/28 |
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