发明名称 High bypass multi-fan engine
摘要 A turbofan jet engine having a housing and an engine core disposed in the housing. The engine core includes at least a compressor, turbine, and a drive shaft. The drive shaft defines a drive shaft axis. A plurality of fans are disposed in the housing and each is rotatable about a separate fan axis. Each of the fan axes are axially offset from the drive shaft axis. The turbofan jet engine further includes a drive system operably interconnecting the engine core and fans so as to rotatably drive the fans and selectively disengage select fans from the engine core.
申请公布号 US2004025493(A1) 申请公布日期 2004.02.12
申请号 US20020216263 申请日期 2002.08.09
申请人 WOJCIECHOWSKI PAUL M. 发明人 WOJCIECHOWSKI PAUL M.
分类号 F02K3/06;F02K3/077;(IPC1-7):F02K3/06 主分类号 F02K3/06
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