| 发明名称 |
COMPONENT AND METHOD OF FABRICATING THE SAME |
| 摘要 |
A component for a gas turbine engine (100) is provided. The component includes a cooling aperture (194, 196) and a plug (204) filling at least a portion of the cooling aperture to prevent airflow through the cooling aperture. The plug is configured to melt at a predetermined temperature during operation of the gas turbine engine to permit airflow through the cooling aperture.
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| 申请公布号 |
CA2793232(A1) |
申请公布日期 |
2013.04.30 |
| 申请号 |
CA20122793232 |
申请日期 |
2012.10.25 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
CORREIA, VICTOR HUGO SILVA;MANNING, ROBERT FRANCIS |
| 分类号 |
F01D25/12;F01D5/18;F01D9/02;F01D21/12;F02C7/12;F02K1/00 |
主分类号 |
F01D25/12 |
| 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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