Methods and apparatus for directing airflow to a compressor bore

A gas turbine engine includes a compressor rotor assembly which directs air at a sufficient pressure and temperature to a compressor rotor bore. The compressor assembly includes a compressor (12, 14) including a plurality of rotors (32) joined with a plurality of couplings (34). Each of the rotors i...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BULMAN, DAVID EDWARD, CLEMENTS, JEFFREY DONALD, BURNS, CRAIG PATRICK, SEITZER, KENNETH EDWARD
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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