发明名称 Premix Burner for operating a combustion chamber with a liquid and/or gaseous fuel
摘要 A premix burner for a gas turbine engine having a pair of partial conical bodies stacked inside each other to form a conical interior chamber is disclosed. The conical bodies are offset laterally to form tangential air flow openings. The width of the openings is varied in a prescribed manner to induce rotational disorder.
申请公布号 US6098406(A) 申请公布日期 2000.08.08
申请号 US19970992473 申请日期 1997.12.17
申请人 ASEA BROWN BOVERI AG 发明人 BOLIS, GIACOMO;FRUTSCHI, HANS ULRICH
分类号 F23C7/00;F23D17/00;(IPC1-7):F23D17/00 主分类号 F23C7/00
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