METHOD FOR APPLYING A COVER TO AN AIRCRAFT WING AND AIRCRAFT WING OBTAINED BY SAID METHOD

A method for applying a cover to an aircraft wing including placing a skin provided with one or more manholes on the aircraft wing; placing a gasket for the, or each, manhole of the skin; placing a plug in the, or each, manhole; and curing the aircraft wing with the cover, the cover comprising the s...

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Bibliographische Detailangaben
Hauptverfasser:	GALERA CORDOBA, Georgina, VAZQUEZ SANCHEZ, Pablo, NOGUEROLES VIÑES, Pedro, TORRES ESTEBAN, Antonio, BLANCO SAIZ, Jose Maria, MARTIN MORENO, Zulima, BELLIDO FUENTETAJA, Oscar
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS CYLINDERS ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS PISTONS SEALINGS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A method for applying a cover to an aircraft wing including placing a skin provided with one or more manholes on the aircraft wing; placing a gasket for the, or each, manhole of the skin; placing a plug in the, or each, manhole; and curing the aircraft wing with the cover, the cover comprising the skin, the gasket or gaskets and the plug or plugs. The aircraft wing includes a cover applied by the described method including a skin, one or more gaskets and one or more plugs.