AIRFOIL ASSEMBLY WITH A TRUNNION AND SPAR

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 (...

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Bibliographische Detailangaben
Hauptverfasser:	DAVIS, Tod Winton, XIE, Ming
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	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.