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
22.01.2025
Patent
Elektronische Ressource
Englisch
TURBINE ENGINE HAVING AN AIRFOIL ASSEMBLY WITH A TRUNNION AND A SPAR
Europäisches Patentamt | 2024
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