Fuel dam, aircraft wing box, aircraft and method of assembling aircraft wing

A method of assembling an aircraft wing includes adhering a fuel dam to a stringer and adhering a fuel dam to a wing rib. The fuel dam includes a fuel dam body defining a channel designed to receive a portion of a stringer of an aircraft wing. The fuel dam body includes a stringer adhesion surface,...

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Bibliographische Detailangaben
Hauptverfasser:	PEREZ DIAZ FRANCISCO LUIS, ABDULKI MOHAMED, WHITMER MATTHEW M, SUKHOMINOV ALEXEY SERGEEVICH, RICHARDSON MARK E, TALCOTT, KENNETH, W
Format:	Patent
Sprache:	chi ; eng
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:	A method of assembling an aircraft wing includes adhering a fuel dam to a stringer and adhering a fuel dam to a wing rib. The fuel dam includes a fuel dam body defining a channel designed to receive a portion of a stringer of an aircraft wing. The fuel dam body includes a stringer adhesion surface, a rib adhesion surface, and a pair of spaced apart flanges extending from the rib adhesion surface and positioned to protrude from the rib adhesion surface on opposite sides of the notch of the rib. 本申请公开组装飞机机翼的方法，该方法包括将燃料坝粘附到纵梁以及将燃料坝粘附到翼肋。燃料坝包括限定通道的燃料坝主体，该通道被设计形状为接收飞机机翼的纵梁的一部分。燃料坝主体包括纵梁粘附表面、翼肋粘附表面和一对间隔开的法兰，所述一对间隔开的法兰从翼肋粘附表面延伸并且定位成在翼肋的凹口的相反侧上从翼肋粘附表面突出。