发明名称 COMBUSTION CHAMBER HAVING SWIRLING FLOW
摘要 A combustion chamber is arranged so that swirling flow is formed therein to improve the manner and rate of burning above that which is normally obtainable. Swirl inducing means are provided at the entrance to the burner and flameholding means are provided around the outer circumference of the burner. Fuel is injected rearwardly of the swirl inducing means.
申请公布号 US3675419(A) 申请公布日期 1972.07.11
申请号 USD3675419 申请日期 1970.10.26
申请人 UNITED AIRCRAFT CORP. 发明人 GEORGE D. LEWIS
分类号 F23R3/16;(IPC1-7):F02C3/24 主分类号 F23R3/16
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