An airfoil assembly (130) and a method of forming the airfoil assembly (130), the airfoil assembly (130) having a trunnion (134), a spar (136), a skin (180), and an insert (172). The trunnion (134) having a flared socket (164) with an open top (170). The spar (136) extending from the flared socket (164) and through the open top (170). The spar (136) having a first end (160) located within the flared socket (164). The skin (180) having a braided or woven fiber.
AIRFOIL ASSEMBLY WITH A TRUNNION AND SPAR
SCHAUFELANORDNUNG MIT EINEM ZAPFEN UND HOLM
ENSEMBLE DE PROFIL AÉRODYNAMIQUE AVEC UN TOURILLON ET UN LONGERON
2025-01-22
Patent
Electronic Resource
English
TURBINE ENGINE HAVING AN AIRFOIL ASSEMBLY WITH A TRUNNION AND A SPAR
European Patent Office | 2024
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