发明名称 Pulsed combustion turbine engine
摘要 A turbine engine has a circumferential array of combustion chamber conduits downstream of the compressor and upstream of the turbine. Means are provided for directing oxygen-containing gas from the compressor to the conduits so as to cyclically feed a gas charge into each conduit through its first port and permit discharge of combustion products of the charge and fuel through both the first and second ports.
申请公布号 US6901738(B2) 申请公布日期 2005.06.07
申请号 US20030608939 申请日期 2003.06.26
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SAMMANN BRADLEY C.;TWELVES, JR. WENDELL V.;JONES GARY D.
分类号 F02C3/16;F02C5/02;F02C5/04;F02C5/11;(IPC1-7):F02C5/00;F02K3/06 主分类号 F02C3/16
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