发明名称 |
MID-SECTION OF A CAN-ANNULAR GAS TURBINE ENGINE WITH A RADIAL AIR FLOW DISCHARGED FROM THE COMPRESSOR SECTION |
摘要 |
A midframe portion (213) of a gas turbine engine (210) is presented, and includes a compressor section (212) configured to discharge an air flow (211) directed in a radial direction from an outlet of the compressor section (212). Additionally, the midframe portion (213) includes a manifold (214) to directly couple the air flow (211) from the compressor section (212) outlet to an inlet of a respective combustor head (218) of the midframe portion (213).
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申请公布号 |
US2013224009(A1) |
申请公布日期 |
2013.08.29 |
申请号 |
US201213408147 |
申请日期 |
2012.02.29 |
申请人 |
LITTLE DAVID A.;MCQUIGGAN GERARD;WASDELL DAVID L. |
发明人 |
LITTLE DAVID A.;MCQUIGGAN GERARD;WASDELL DAVID L. |
分类号 |
F01D1/04;F01D25/00 |
主分类号 |
F01D1/04 |
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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