CONTROL DEVICE OF GAS TURBINE ENGINE

PROBLEM TO BE SOLVED: To provide a control device of a gas turbine engine capable of promptly suppressing surging. SOLUTION: A control device of a gas turbine engine for causing air of which flow rate has been adjusted by performing angular control on a variable inlet guide vane provided in an inlet...

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Bibliographische Detailangaben
1. Verfasser:	OTANI NORIAKI
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 NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a control device of a gas turbine engine capable of promptly suppressing surging. SOLUTION: A control device of a gas turbine engine for causing air of which flow rate has been adjusted by performing angular control on a variable inlet guide vane provided in an inlet flow path of a compressor, to flow into the compressor, causing air compressed by the compressor to flow into a combustor, thereby causing a turbine to rotate by combustion gas in the combustor, wherein angle holding of the variable inlet guide vane is released, in a case where surging occurs in the compressor. COPYRIGHT: (C)2010,JPO&INPIT