FUEL OIL FOR GAS TURBINE

PROBLEM TO BE SOLVED: To obtain a fuel oil for gas turbines low in metal (ash) content, sulfur content, soot emission, fine grain impurities and suppressing corrosion of a turbine blade and having high calorific power. SOLUTION: The fuel oil for gas turbines has a 90% distilling temperature of =3976...

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Bibliographische Detailangaben
Hauptverfasser:	SAWADA TADANORI, HIRANO HIROSHI, KOMATSU ISAO, KOIDE KIEMON
Format:	Patent
Sprache:	eng
Schlagworte:	ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE ORUNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL CHEMISTRY FIRELIGHTERS FUELS FUELS NOT OTHERWISE PROVIDED FOR LIQUEFIED PETROLEUM GAS LUBRICANTS METALLURGY NATURAL GAS PEAT PETROLEUM, GAS OR COKE INDUSTRIES SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BYSUBCLASSES C10G, C10K TECHNICAL GASES CONTAINING CARBON MONOXIDE
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To obtain a fuel oil for gas turbines low in metal (ash) content, sulfur content, soot emission, fine grain impurities and suppressing corrosion of a turbine blade and having high calorific power. SOLUTION: The fuel oil for gas turbines has a 90% distilling temperature of =39760 KJ/liter, content of dibenzothiophene derivatives as sulfur content of