发明名称 |
APPARATUS AND METHODS FOR COOLING PLATFORM REGIONS OF TURBINE ROTOR BLADES |
摘要 |
A platform cooling configuration in a turbine rotor blade that includes platform slot formed through at least one of the pressure side slashface and the suction side slashface; a removably-engaged impingement insert that separates the platform into two radially stacked plenums, a first plenum that resides inboard of a second plenum; a high-pressure connector that connects the first plenum to the high-pressure coolant region of the interior cooling passage; a low-pressure connector that connects the second plenum to the low-pressure coolant region of the interior cooling passage.
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申请公布号 |
US2012082550(A1) |
申请公布日期 |
2012.04.05 |
申请号 |
US20100895035 |
申请日期 |
2010.09.30 |
申请人 |
HARRIS, JR. JOHN WESLEY;ELLIS SCOTT EDMOND;FU XIAOYONG;SCOTT ADRIAN LIONAL;GENERAL ELECTRIC COMPANY |
发明人 |
HARRIS, JR. JOHN WESLEY;ELLIS SCOTT EDMOND;FU XIAOYONG;SCOTT ADRIAN LIONAL |
分类号 |
F01D5/08;B23P15/04 |
主分类号 |
F01D5/08 |
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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