发明名称 |
TWIN TIP TURBINE PROPULSORS POWERED BY A SINGLE GAS TURBINE GENERATOR |
摘要 |
A gas turbine engine has a core engine incorporating a turbine, and a manifold positioned downstream of the turbine. The manifold delivers gas downstream of the turbine into at least two nacelles, with each of the nacelles receiving a fan rotor. The fan rotor is fixed to rotate with a tip turbine mounted at a radially outer location of the fan rotor, with the tip turbine being in the path of gases from the manifold. An aircraft is also disclosed. |
申请公布号 |
WO2014109811(A2) |
申请公布日期 |
2014.07.17 |
申请号 |
WO2013US66531 |
申请日期 |
2013.10.24 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;CHANDLER, JESSE M.;STAUBACH, JOSEPH B.;SUYDAM, ADAM JOSEPH |
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