GAS TURBINE ENGINE WITH RING DAMPER

A damper seat 118 for a ring damper 116 that redirects axial loads and is disposed within a gas turbine engine 10 with at least one disk 104 rotatable about a rotational axis 12 and having a disk neutral axis 106 extending radially from the rotational axis 12.

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Bibliographic Details
Main Authors PRESCOTT, Jeffrey Miles McMillen, SIMEONE, Peter Andrew, WESLING, Richard Alan
Format Patent
LanguageEnglish
French
German
Published 16.08.2017
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
ENGINEERING ELEMENTS AND UNITS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MEANS FOR DAMPING VIBRATION
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
SHOCK-ABSORBERS
SPRINGS
STEAM ENGINES
THERMAL INSULATION IN GENERAL
WEAPONS
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Summary:A damper seat 118 for a ring damper 116 that redirects axial loads and is disposed within a gas turbine engine 10 with at least one disk 104 rotatable about a rotational axis 12 and having a disk neutral axis 106 extending radially from the rotational axis 12.
Bibliography:Application Number: EP20160202431