| 发明名称 |
COOLED AIRFOIL STRUCTURE CORRESPONDING COOLING METHOD |
| 摘要 |
An airfoil structure (60) for a gas turbine engine includes an airfoil (62) that includes a suction side cooling circuit (86) with at least two segments (90a,90b,90c,90d) that are connected by at least one impingement passage (100). A corresponding method of cooling an airfoil is also provided. |
| 申请公布号 |
EP2977557(A1) |
申请公布日期 |
2016.01.27 |
| 申请号 |
EP20150178080 |
申请日期 |
2015.07.23 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SLAVENS, THOMAS N.;SNYDER, BROOKS E.;BURDICK, ANDREW D. |
| 分类号 |
F01D5/18 |
主分类号 |
F01D5/18 |
| 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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