BELLY BAND SEALS AND METHOD

BELLY BAND SEALS AND METHOD

The present application provides a rotor (155) for use in a turbine engine (10). The rotor (155) may include a first rotor disc (130), a second rotor disc (150) adjacent to the first rotor disc (130), and a belly band seal (100) positioned between the first rotor disc (130) and the second rotor disc...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: PAWLOWSKI, Marco Christof, SIMONET, Christophe, CATALDI, Giovanni
Format: Patent
Sprache:eng ; fre ; ger
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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Beschreibung
Zusammenfassung:The present application provides a rotor (155) for use in a turbine engine (10). The rotor (155) may include a first rotor disc (130), a second rotor disc (150) adjacent to the first rotor disc (130), and a belly band seal (100) positioned between the first rotor disc (130) and the second rotor disc (150). The belly band seal (100) may include a band seal (105) with a locking tab (170) brazed thereon.