发明名称 Gas turbine engine augmentor.
摘要 <p>The pilot section (12) of a flameholder (10) of an augmentor for a gas turbine engine is modified to improve the ignition and stability characteristics by judiciously locating aperture(s) or slot(s) (32) in the pilot section (12) wherein their orientation is critical so as to create a vortical flow field.</p>
申请公布号 EP0224429(A2) 申请公布日期 1987.06.03
申请号 EP19860630174 申请日期 1986.11.20
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CLEMENTS, THOMAS RUSH;BLEVINS, JAMES DALE
分类号 F02C7/00;F02C7/22;F02C7/264;F23R3/18;(IPC1-7):F23R3/18 主分类号 F02C7/00
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