BOLTED JOINT OF THE COVER OF AN ACCESS OPENING IN AN AIRCRAFT LIFTING SURFACE

A bolted joint for connecting a cover (11) of an opening in a primary structure (13) of a lifting surface of an aircraft to said primary structure (13) is provided. The bolted joint comprises two first bolted joints (21, 21') on either side of the symmetry axis (A-A) of the cover arranged witho...

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Bibliographische Detailangaben
Hauptverfasser:	ALAZRAKI, MARCOS, SANZ TORRIJOS, JOSE
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS 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 EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A bolted joint for connecting a cover (11) of an opening in a primary structure (13) of a lifting surface of an aircraft to said primary structure (13) is provided. The bolted joint comprises two first bolted joints (21, 21') on either side of the symmetry axis (A-A) of the cover arranged without any clearance, two second bolted joints on either side of the symmetry axis (A-A) on the side of the cover opposite to that of the two first bolted joints arranged without any clearance in the holes of the primary structure (13) and with a linear clearance in the holes (30) of the cover (11); a plurality of third bolted joints (25, 25', 25", ...) along the border of the cover (11) arranged without any clearance in the holes of the primary structure (13) and with a radial clearance in the holes (30) of the cover (11).