发明名称 Gas turbine with catalytic burner - which contains thermally stable, oxidn. resistant metal monolith with through holes in which catalytic combustion occurs
摘要 <p>A gas turbine is fitted with a catalytic burner contg. a thermally stable and oxidn. resistant metallic monolith which has many through passages for the catalytic combustion of the combustion gaes and of the injected fuel. The passages are so designed that the pressure drop of the gas/fuel mixt. is 10%. Catalytic combustion of a part of, or of all fuel can now be utilised in a gas turbine without requiring an excessively high throughput of air and fuel. The concn. of pollutants in the exhaust gas is reduced considerably.</p>
申请公布号 FR2382584(A1) 申请公布日期 1978.09.29
申请号 FR19780005951 申请日期 1978.03.02
申请人 JOHNSON MATTHEY AND CO LTD 发明人 BERNARD EDVARD ENGA ET ALLIN SIDNEY PRATT;PRATT ALLIN SIDNEY
分类号 F23C13/00;F23R3/40;(IPC1-7):02C7/00;02M27/02 主分类号 F23C13/00
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