GAS TURBINE ENGINE WITH RING DAMPER

PROBLEM TO BE SOLVED: To provide a gas turbine disk that reduces vibration amplitude and can reduce a risk of disk failure due to high cycle fatigue.SOLUTION: A gas turbine engine comprises: at least one disk 104 rotatable about a rotational axis and having a disk neutral axis 106 extending radially...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	JEFFREY MILES MCMILLEN PRESCOTT, PETER ANDREW SIMEONE, WESLING RICHARD ALAN
Format:	Patent
Sprache:	eng ; jpn
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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