| 发明名称 |
CERAMIC MATRIX COMPOSITE AIRFOIL STRUCTURES FOR A GAS TURBINE ENGINE |
| 摘要 |
A Ceramic Matrix Composite (CMC) airfoil segment for a gas turbine engine includes a box-shape fiber geometry which defines a rectilinear pressure side bond line and a rectilinear suction side bond line.
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| 申请公布号 |
US2012301312(A1) |
申请公布日期 |
2012.11.29 |
| 申请号 |
US201113116093 |
申请日期 |
2011.05.26 |
| 申请人 |
|
发明人 |
BERCZIK DOUGLAS M.;SUCIU GABRIEL L.;MERRY BRIAN D.;IOANNIS ALVANOS;DYE CHRISTOPHER M. |
| 分类号 |
F01D5/14;B21K25/00 |
主分类号 |
F01D5/14 |
| 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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