| 发明名称 |
Compressor's vane in particular for a gas turbine engine |
| 摘要 |
A compressor airfoil (12) includes pressure and suction sides (18,20) extending from root (22) to tip (24) and between leading and trailing edges (26,28). Transverse sections have respective chords and camber lines. Centers of gravity (34) of the sections are aligned along a double bowed stacking axis for improving performance. <IMAGE> |
| 申请公布号 |
PL196777(B1) |
申请公布日期 |
2008.01.31 |
| 申请号 |
PL20000342227 |
申请日期 |
2000.08.29 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
LIU HSIN-TUAN;DICKMAN ROBERT D.;KRABACHER KENNETH WILLIAM;STEINMETZ GREGORY TODD;BEACHER BRENT FRANKLIN;DOLORESCO BRYAN KEITH |
| 分类号 |
F01D5/00;F01D5/14;F04D29/32;F04D29/38 |
主分类号 |
F01D5/00 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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