发明名称 |
GEARED TURBOFAN WITH THREE CO-ROTATING TURBINES |
摘要 |
<p>A gas turbine engine has a fan rotor, a first compressor rotor and a second compressor rotor. The second compressor rotor compresses air to a higher pressure than the first compressor rotor. A first turbine rotor drives the second compressor rotor and a second turbine rotor. The second turbine drives the compressor rotor. A fan drive turbine is positioned downstream of the second turbine rotor. The fan drive turbine drives the fan rotor through a gear reduction. The first compressor rotor and second turbine rotor rotate as an intermediate speed spool. The second compressor rotor and first turbine rotor together as a high speed spool. The high speed spool, the intermediate speed spool, and the fan drive turbine rotate in the same direction.</p> |
申请公布号 |
SG11201405924V(A) |
申请公布日期 |
2014.10.30 |
申请号 |
SG11201405924V |
申请日期 |
2013.03.29 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHWARZ, FREDERICK M.;KUPRATIS, DANIEL BERNARD |
分类号 |
F02K3/075;F02C7/36 |
主分类号 |
F02K3/075 |
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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