Decoupler system for rotor assemblies

A rotor decoupler system for a gas turbine engine is disclosed, comprising a load reduction system disposed between a bearing system and the bearing support. The load reduction system comprises a fuse and a damper such that the damper transfers at least a part of the radial load from the rotor to th...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: Storace, Albert Frank
Format: Patent
Sprache:eng
Online-Zugang:Volltext bestellen
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