发明名称 |
LOW LEAKAGE MULTI-DIRECTIONAL INTERFACE FOR A GAS TURBINE ENGINE |
摘要 |
<p>An interface within a gas turbine engine includes a multiple of segmented components, each with a segment flange with a multiple of apertures, at least one of the multiple of apertures a first slot aperture. A full ring component with a ring flange that defines a multiple ring of apertures, at least one of the multiple of ring apertures a second slot aperture, the second slot aperture transverse to the first slot aperture.</p> |
申请公布号 |
WO2014123965(A1) |
申请公布日期 |
2014.08.14 |
申请号 |
WO2014US14811 |
申请日期 |
2014.02.05 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
ROGERS, MARK J.;BROOMER, MARK;MCGARRAH, CRAIG R.;DAVIS, TIMOTHY M.;SWIFT, ANTHONY B.;KEENE, RUSSELL E.;ROY THILL, CARSON A.;DUNBAR, TIMOTHY A. |
分类号 |
F01D11/08;F01C7/00;F01D5/12 |
主分类号 |
F01D11/08 |
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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