发明名称 Pulse detonation engine system for driving turbine
摘要 A pulse detonation engine system ( 1 ) for driving a turbine is comprises a detonation generator section ( 5 ) including a detonation tube ( 7 ) having a tubular hollow section for permitting detonation to be generated therein during combustion stage of a mixture gas combined with a gas and a fuel, a gas supply section ( 17 ) for feeding the gas into the tubular hollow section of the detonation tube ( 7 ) at given time intervals, a fuel valve ( 19 ) for feeding the fuel into the tubular hollow section of the detonation tube ( 7 ) at the given time intervals, and an ignition plug ( 15 ) for igniting the mixture gas in the tubular hollow section of the detonation tube ( 7 ), and a pulse detonation driven turbine ( 9 ) driven directly or indirectly by energy of detonations that are intermittently generated in the tubular hollow section of the detonation tube ( 7 ).
申请公布号 US7367194(B2) 申请公布日期 2008.05.06
申请号 US20040511906 申请日期 2004.10.20
申请人 ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD. 发明人 MURAYAMA MOTOHIDE;YAMAWAKI SHIGEMICHI;TOH HIDEMI;KOBAYASHI HIDEO;TAKAHASHI KATSUYOSHI;CHIBA KAORU;OHYAGI SHIGEHARU
分类号 F02C7/22;F02C3/28;F02C5/10;F02C6/18;F02C7/26 主分类号 F02C7/22
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