System for controlling combustion in a gas combustion-type turbine

Gas turbine system (50) incorporates an improved combustion system (52) having no control linkage, but instead, a pneumatically actuatable valve (58) that is mounted within a housing (56). Housing (56) does not have a plurality of holes formed therein for admitting a mechanical linkage, as does the...

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Bibliographische Detailangaben
Hauptverfasser:	ANDREW J KOSINSKI, STEPHEN E MUMFORD
Format:	Patent
Sprache:	eng
Schlagworte:	ACTUATING-FLOATS AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COCKS COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DEVICES FOR VENTING OR AERATING ENGINEERING ELEMENTS AND UNITS GAS-TURBINE PLANTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING TAPS THERMAL INSULATION IN GENERAL VALVES WEAPONS
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Beschreibung
Zusammenfassung:	Gas turbine system (50) incorporates an improved combustion system (52) having no control linkage, but instead, a pneumatically actuatable valve (58) that is mounted within a housing (56). Housing (56) does not have a plurality of holes formed therein for admitting a mechanical linkage, as does the housing in a conventional gas turbine system.