A turbine engine (10) comprising a fan section (18), a compressor section (22), a combustion section (28), and a turbine section (32) in serial flow arrangement and defining a stator portion and a rotor portion, which rotates about an engine centerline (12). The rotor portion comprising a variable pitch airfoil assembly (130). The variable pitch airfoil assembly (130) having an airfoil (132) and a balancing insert (170).
TURBINE ENGINE HAVING A VARIABLE PITCH AIRFOIL ASSEMBLY
TURBINENMOTOR MIT EINER SCHAUFELANORDNUNG MIT VARIABLER NEIGUNG
MOTEUR À TURBINE AYANT UN ENSEMBLE DE PROFIL AÉRODYNAMIQUE À PAS VARIABLE
19.03.2025
Patent
Elektronische Ressource
Englisch
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