conjunto de rolamento amortecedor, método de montagem de um conjunto e conjunto de rotor

A damper bearing assembly for a gas turbine engine is disclosed. The damper bearing assembly is designed to define forward and aft axial gaps which allow for normal deflection under standard operating thrust loads, but then close during a fan blade out event to allow the increased load to transfer t...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BRUCE ALAN CARTER, VIVEK NEMA, RAVINDRA SHANKAR GANIGER, STEPHANIE FRANCES DRUMMOND
Format:	Patent
Sprache:	por
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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