发明名称 Turbofan aircraft engine
摘要 The turbofan aircraft engine is so arranged that the greater part of the cool air stream (13) passes through the hollow outlet scoops (15) into the inner cavity (4a) of the low pressure turbine cone (4), which has a jet-like outlet aperture (22) at its downstream free end, which thus acts as an ejector (14), via which the cool air stream is mixed with the air stream coming from the mixer (8). This end of the cone may have air overflow apertures in it.
申请公布号 DE19740228(A1) 申请公布日期 1999.03.18
申请号 DE19971040228 申请日期 1997.09.12
申请人 BMW ROLLS-ROYCE GMBH, 61440 OBERURSEL, DE 发明人 NEGULESCU, DIMITRIE, 14163 BERLIN, DE;HAARMEYER, JOERG, DR., 15834 RANGSDORF, DE
分类号 F01D5/08;F01D9/06;F01D25/12;F02K1/04;F02K3/04;(IPC1-7):F02K3/077;F02C7/18 主分类号 F01D5/08
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