Method of starting gas turbine engine

A method of starting a gas turbine engine (10) having a rotor (12) comprising at least a shaft (14) mounted compressor (16) and turbine (18) is disclosed, with a casing (24) surrounding the rotor (12). 种启动具有至少包括安装在轴(14)上的压缩机(16)和涡轮(18)的转子(12)的燃气涡轮发动机(10)的方法，其中壳(24)包绕转子(12)。...

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Bibliographische Detailangaben
Hauptverfasser:	MARK EDWARD LINZ, STEVEN ALAN ROSS, JOSEPH DANIEL GARRETT, III
Format:	Patent
Sprache:	chi ; 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 (10) having a rotor (12) comprising at least a shaft (14) mounted compressor (16) and turbine (18) is disclosed, with a casing (24) surrounding the rotor (12). 种启动具有至少包括安装在轴(14)上的压缩机(16)和涡轮(18)的转子(12)的燃气涡轮发动机(10)的方法，其中壳(24)包绕转子(12)。