发明名称 AUGMENTOR
摘要 A turbine engine has a centerbody within a gas flowpath and a downstream tailcone and a pilot at an upstream end of the tailcone. A flameholder is positioned in the flowpath outboard of the centerbody. The pilot has a first surface diverging in a downstream direction.
申请公布号 CA2458280(A1) 申请公布日期 2004.09.13
申请号 CA20042458280 申请日期 2004.02.23
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BUEY, JOHN R.;BONNELL, JOHN M.
分类号 F02C3/16;F02K1/04;F02K3/10;F23D14/74;F23R3/34;(IPC1-7):F02K3/10 主分类号 F02C3/16
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