A gas generator (22) has at least one compressor rotor (24), at least one gas generator turbine rotor (30) and a combustion section (32). A fan drive turbine (36) is positioned downstream of a path of the products of combustion having passed over the at least one gas generator turbine rotor (30). The fan drive turbine (36) drives a shaft (40) and the shaft engages gears to drive at least three fan rotors (42,44,46,48).
申请公布号
EP2905429(A1)
申请公布日期
2015.08.12
申请号
EP20150153711
申请日期
2015.02.03
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
SUCIU, GABRIEL L.;MCCUNE, MICHAEL E.;CHANDLER, JESSE M.;EPSTEIN, ALAN H.;O'FLARITY, STEVEN M.;HANLON, CHRISTOPHER J.;SCHNEIDER, WILLIAM F.;STAUBACH, JOSEPH B.;KENYON, JAMES A.
