Main connector for an airfoil or wing

Details Main connector for an airfoil or wing Main connector for an airfoil or wing

B - Operations, Transporting

64

C

244/120

B64C 3/00 (2006.01) B64C 1/26 (2006.01)

Patent

CA 1084028

TITLE OF THE INVENTION: MAIN CONNECTOR FOR AN AIRFOIL OR WING ABSTRACT OF THE DISCLOSURE: An airfoil or wing is connected to the body of an aircraft or spacecraft through a main connector comprising metal and nonmetal components. Tension load take-up loops and a pressure load take-up core are arranged or held in a metal grommet which in turn is centered relative to and integrated with a main connector bushing. Thus, the tension loads are solely introduced into the wing structure through said ten- sion loops and pressure loads are taken up solely by said pressure core, whereby the advantages of fiber compount materials are optimally utilized.

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