发明名称 |
Gas turbine engine component having wavy cooling channels with pedestals |
摘要 |
A gas turbine engine component (40;82) comprises a plurality of walls, a cooling channel (54;92), a plurality of ribs (58A-F;94A-D) and a plurality of pedestals (64A-F;96A-F). The plurality of walls has a pair of major surfaces (56A;56B) opposed to define an interior chamber. The cooling channel (54;92) extends through the interior chamber of the plurality of walls between the major surfaces (56A;56B). The plurality of ribs (58A-F;94A-D) extends through the cooling channel to form a plurality of wavy passages (65A-E;98A-B) having bowed-out sections (68A-B;102A-B). The plurality of pedestals (64A-F;96A-F) is positioned between adjacent ribs (58A-F;94A-D), each pedestal (64A-F;96A-F) being positioned in a bowed-out section (68A-B;102A-B). |
申请公布号 |
EP2586981(A2) |
申请公布日期 |
2013.05.01 |
申请号 |
EP20120186707 |
申请日期 |
2012.09.28 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
PIGGUSH, JUSTIN D.;TRINDADE, RICARDO |
分类号 |
F01D5/18;F01D5/20;F01D11/24 |
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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