METHOD OF STARTING A GAS TURBINE ENGINE

A method of starting a gas turbine engine having a rotor comprising at least a shaft mounted compressor and turbine, with a casing surrounding the rotor.

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Bibliographische Detailangaben
Hauptverfasser:	Swager Thomas Charles, Garrett, III Joseph Daniel, Linz Mark Edward, Ansari Amid, Kirchmayer Kenneth, Kiracofe Daniel Roy, Steen Tod Robert, Broda Joseph Roger, Graziano Kevin Richard, Lehmann Andrew Todd, McCambrige Michael Scott, Hon Robert Charles, Ross Steven Alan, Gillingham Thomas Earl
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 method of starting a gas turbine engine having a rotor comprising at least a shaft mounted compressor and turbine, with a casing surrounding the rotor.