Gas turbine engine

A bypass turbofan gas turbine engine is started by an electric starter motor that is mounted directly about a downstream end or upstream of the low pressure spool of the engine. This causes air to be driven by a fan through a bypass duct around the engine casing. Closures close to substantially seal...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Bradbrook, Stephen John, Davis, Brian, Wilson, Richard James
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A bypass turbofan gas turbine engine is started by an electric starter motor that is mounted directly about a downstream end or upstream of the low pressure spool of the engine. This causes air to be driven by a fan through a bypass duct around the engine casing. Closures close to substantially seal an outlet of the bypass duct, and the air is directed into a combustion chamber of the engine and through the turbines causing the high pressure spool to pick up speed for starting.