GAS TURBINE ENGINE VARIABLE GEOMETRY FLOW COMPONENT

A variable geometry mechanism suitable for use in a gas turbine engine is disclosed in which movable vane segments (64,66) which are coupled to a rotatable ring, or rings (68,70), are used to change an aerodynamic property of a working fluid flowing through the gas turbine engine. The movable vane s...

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Bibliographische Detailangaben

Hauptverfasser:	FORD, ADAM D, BLOXHAM, MATTHEW J, GORMAN, THOMAS I, HEATHCO, CRAIG E, DUGE, ROBERT T
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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