Methods and tools for facilitating the installation and/or removal of a rotor (94) on a shaft (32) of a gas turbine engine (10) are provided. The tool (44) includes a stabilizer (46) attachable to the shaft (32) and including a first guide counterpart. The tool (44) also includes a holder (48) attachable to the rotor (94) and including a second guide counterpart for engagement with the first guide counterpart of the stabilizer (46). Engagement of the first and second guide counterparts guides movement of the holder (48) relative to the stabilizer (46) along a guide axis (GA) and prevents movement of the holder (48) relative to the stabilizer (46) transverse to the guide axis (GA).
ASSEMBLY AND METHOD FOR INSTALLING A BLADED ROTOR ON A SHAFT OF A GAS TURBINE ENGINE OR REMOVING A BLADED ROTOR FROM THE GAS TURBINE ENGINE
ANORDNUNG UND VERFAHREN ZUM ANBRINGEN EINES SCHAUFELROTORS AN EINER WELLE EINES GASTURBINENTRIEBWERKS ODER ZUM ENTFERNEN EINES SCHAUFELROTORS VOM GASTURBINENTRIEBWERK
AGENCEMENT ET PROCÉDÉ POUR INSTALLER UN ROTOR AUBAGÉ SUR UN ARBRE D'UN MOTEUR À TURBINE À GAZ OU POUR RETIRER UN ROTOR AUBAGÉ DU MOTEUR À TURBINE À GAZ
2024-05-15
Patent
Elektronische Ressource
Englisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Dynamics of steam turbine rotor blading ; Pt. 2: Bladed discs
TIBKAT | 1998
|Engineering Index Backfile | 1940
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