FUEL DAM, AIRCRAFT MAIN WING BOX, AIRCRAFT, AND METHOD FOR ASSEMBLING AIRCRAFT MAIN WING

To provide fuel dams, an aircraft main wing box, an aircraft, and a method for assembling an aircraft main wing.SOLUTION: A method for assembling an aircraft main wing 12 includes: fastening fuel dams 100 to stringers 18; and fastening the fuel dams to ribs 16. The fuel dam comprises a fuel dam body...

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Bibliographische Detailangaben
Hauptverfasser:	FERNANDO L PEREZ DIAZ, KRISTOPHER WILLIAM TALCOTT, MARK EDMUND RICHARDSON, ALEXANDER S SUKHOMLINOV, MARK ABDOUCH, MATTHEW MCKINLEY WHITMER
Format:	Patent
Sprache:	eng ; jpn
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:	To provide fuel dams, an aircraft main wing box, an aircraft, and a method for assembling an aircraft main wing.SOLUTION: A method for assembling an aircraft main wing 12 includes: fastening fuel dams 100 to stringers 18; and fastening the fuel dams to ribs 16. The fuel dam comprises a fuel dam body that defines a channel molded so as to receive one portion of the stringer of the aircraft main wing. The fuel dam body comprises a stringer fastening surface, a rib fastening surface, and a pair of separated flanges 112 that extend from the rib fastening surface and project from the rib fastening surface on both sides of a notch of the rib.SELECTED DRAWING: Figure 3 【課題】燃料ダム、航空機主翼ボックス、航空機、及び航空機主翼を組み立てる方法を提供する。【解決手段】航空機主翼１２を組み立てる方法が、燃料ダム１００をストリンガ１８に固着させること、及び燃料ダムをリブ１６に固着させることを含む。燃料ダムは、航空機主翼のストリンガの一部分を受け入れるように成形されたチャネルを画定する燃料ダム本体を備える。燃料ダム本体は、ストリンガ固着面、リブ固着面、及び、リブ固着面から延在し、リブの切り欠きの両側でリブ固着面から突出する一対の離隔されたフランジ１１２を備える。【選択図】図３