发明名称 |
GAS TURBINE ENGINE COMPONENT WITH TWISTED INTERNAL CHANNEL |
摘要 |
<p>A gas turbine engine component includes a component body that defines an internal micro-channel that extends in a lengthwise direction along a reference line. The internal micro-channel extends between a first reference position along the reference line and a second reference position along the reference line. The internal micro-channel twists at least 180 with respect to the reference line between the first reference position and the second reference position.</p> |
申请公布号 |
WO2014175951(A3) |
申请公布日期 |
2015.01.29 |
申请号 |
WO2014US17661 |
申请日期 |
2014.02.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
LAMSON, SCOTT |
分类号 |
F01D5/14;F01D5/18;F02C7/18;F15D1/00 |
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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