WING AND METHOD OF MANUFACTURING

The present invention relates to a wing, which comprises: a wing box having wing beams connected to each other; an inner system installed in the wing box; a pair of opposite skins which are coupled in the wing box to cover the wing box, and of which one finishes the wing; and a plurality of coupling...

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Bibliographische Detailangaben
1. Verfasser:	WILKERSON JEFFREY A
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The present invention relates to a wing, which comprises: a wing box having wing beams connected to each other; an inner system installed in the wing box; a pair of opposite skins which are coupled in the wing box to cover the wing box, and of which one finishes the wing; and a plurality of coupling systems coupling the skins to the wing beams, and formed to provide protection from electromagnetic effects. Each coupling system of the coupling systems comprises: a threaded fastener; and a nut plate having a main body and a cover; a nut sealed in the nut plate between the main body and the cover. The nut is restricted to perform rotation around a nut plate shaft in the nut plate, and is perpendicular to the nut plate shaft in the nut plate to be freely and linearly moved. 날개는 상호연결되는 날개보들을 포함하는 날개 박스, 날개 박스 내에 설치된 내측 시스템, 날개 박스에 체결되며 날개 박스를 덮는 대향하는 한 쌍의 스킨들 -스킨들 중 하나는 날개를 마무리지음-, 및 스킨들을 날개보들에 체결시키며, 전자기 효과들로부터의 보호를 제공하도록 구성된 복수의 체결 시스템들을 포함하며, 체결 시스템들의 각각의 체결 시스템은 스레디드 패스너, 본체 및 커버를 포함하는 너트 플레이트, 및 본체와 커버 사이에서 너트 플레이트 내에 봉입된 너트를 포함하며, 너트는 너트 플레이트 내에서 너트 플레이트 축을 중심으로 하는 회전이 제약되며, 너트 플레이트 내에서 너트 플레이트 축에 직교하여 선형으로 자유롭게 움직인다.