Pulse detonation engine system for driving turbine

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,...

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Bibliographische Detailangaben
Hauptverfasser:	TOH HIDEMI, MURAYAMA MOTOHIDE, YAMAWAKI SHIGEMICHI, OHYAGI SHIGEHARU, CHIBA KAORU, KOBAYASHI HIDEO, TAKAHASHI KATSUYOSHI
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	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 ).