LOAD INTRODUCTION SYSTEM AND METHOD FOR MANUFACTURING A LOAD INTRODUCTION SYSTEM

A load introduction system comprising an aerodynamic component having a skin section with an outer surface and a first protrusion, and an attachment unit for movably coupling the aerodynamic component to a base unit. The attachment unit is attached to the skin section of the aerodynamic component an...

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Bibliographische Detailangaben
Hauptverfasser:	ENDER, Tobias, DAANDELS, Dort, STUBBE, Kathrin, SEACK, Oliver
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A load introduction system comprising an aerodynamic component having a skin section with an outer surface and a first protrusion, and an attachment unit for movably coupling the aerodynamic component to a base unit. The attachment unit is attached to the skin section of the aerodynamic component and to the first protrusion, wherein the first protrusion extends away from the aerodynamic outer surface, thereby separating a space adjacent the aerodynamic outer surface into a front space and a rear space. The attachment unit extends over the first protrusion such that the attachment unit comprises a front portion in the front space and a rear portion in the rear space. Also a method for manufacturing a load introduction system.