| 发明名称 |
LOW COMPRESSOR HAVING VARIABLE VANES |
| 摘要 |
An example gas turbine engine compressor includes a first compressor section. The first compressor section includes rotating stage that includes rotating blades and a stationary stage upstream thereof that includes stationary guide vanes. The stationary vanes controllably pivot about respective pivot axises for providing flow control into the rotating stage. |
| 申请公布号 |
US2015260054(A1) |
申请公布日期 |
2015.09.17 |
| 申请号 |
US201314431953 |
申请日期 |
2013.01.28 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Blake Sean DJ;Tempelman William G.;Teicholz Matthew D.;Gendron John R.;Wojcik Kerri A.;Spiesman Paul H.;Hatch Stewart B.;Daentl Wyatt S.;Bartkowski Glenn D. |
| 分类号 |
F01D17/16 |
主分类号 |
F01D17/16 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine compressor, comprising:
a first compressor section, the first compressor section including: at least one rotating stage that includes rotating blades and at least one stationary stage upstream thereof that includes stationary guide vanes, which controllably pivot about respective pivot axises for providing flow control into the rotating stage. |
| 地址 |
Hartford CT US |
