发明名称 |
TURBINE ENGINE AFTERBURNER |
摘要 |
A turbine engine has a centerbody (38) within a gas flowpath and a downstream tailcone (58) and a pilot (56) at an upstream end of the tailcone (58). A flameholder (82) is positioned in the flowpath outboard of the centerbody (38). The pilot (56) has a first surface (64) diverging in a downstream direction. |
申请公布号 |
PL365623(A1) |
申请公布日期 |
2004.09.20 |
申请号 |
PL20040365623 |
申请日期 |
2004.02.26 |
申请人 |
UNITED TECHNOLOGIES CORP |
发明人 |
BUEY JOHN R;BONNELL JOHN M |
分类号 |
F02C3/16;F02K1/04;F02K3/10;F23D14/74;F23R3/34 |
主分类号 |
F02C3/16 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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