发明名称 Bypass jet engine for primary drive of aircraft has bypass acceleration fan turbines with connected working turbine
摘要 The bypass jet engine has bypass acceleration fan turbines to accelerate the bypass flow and a working turbine (3) able to transmit torque to them.
申请公布号 DE10116535(A1) 申请公布日期 2002.02.21
申请号 DE20011016535 申请日期 2001.04.03
申请人 SEEFLUTH, U. CHRISTIAN 发明人
分类号 F02C3/045;F02C3/06;F02C3/073;F02C3/10;F02C3/13;F02C6/02;F02K3/04;F02K3/06;(IPC1-7):F02K3/04;F02K1/54 主分类号 F02C3/045
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