FUEL DAMS, AIRCRAFT WING BOXES, AIRCRAFT, AND METHODS OF ASSEMBLING AIRCRAFT WINGS

Methods of assembling an aircraft wing comprise adhering fuel dams to stringers and adhering the fuel dams to ribs. Fuel dams comprise a fuel-dam body that defines a channel shaped to receive a portion of a stringer of an aircraft wing. The fuel-dam body comprises a stringer adherent surface, a rib...

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Bibliographische Detailangaben
Hauptverfasser:	WHITMER, Matthew McKinley, PEREZ DIAZ, Fernando L, TALCOTT, Kristopher William, SUKHOMLINOV, Alexander S, ABDOUCH, Mark, RICHARDSON, Mark Edmund
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	Methods of assembling an aircraft wing comprise adhering fuel dams to stringers and adhering the fuel dams to ribs. Fuel dams comprise a fuel-dam body that defines a channel shaped to receive a portion of a stringer of an aircraft wing. The fuel-dam body comprises a stringer adherent surface, a rib adherent surface, and a pair of spaced-apart flanges extending from the rib adherent surface and positioned to project from the rib adherent surface on opposing sides of a notch of a rib.