A turbine engine has a case with an axis. A fan is mounted for rotation about the axis. A turbine is mechanically coupled to the fan to drive rotation of the fan about the axis. A number of compressor/turbine units are downstream of the fan and upstream of the turbine along a core flowpath. A number of compressors are coupled to the compressor/turbine units to receive air and deliver combustion gas to drive the turbine.
申请公布号
US2007277500(A1)
申请公布日期
2007.12.06
申请号
US20060445977
申请日期
2006.06.01
申请人
JONES JAMES E;PERKINS GARY M;ROBERGE GARY D;THONEBE DOUGLAS A;PERKINS MARSHA E
发明人
JONES JAMES E.;PERKINS GARY M.;ROBERGE GARY D.;THONEBE DOUGLAS A.;PERKINS MARSHA E.