Method for making a laminated structure and aeroplane provided with such a structure

The process involves presenting a panel and a plate (3) in stack, and piercing the stack to form a fixation hole. A fixing rod (8) is inserted into the fixation hole. A negative clearance between diameters of the fixation hole and the rod is created during the piercing process. The rod is inserted o...

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Bibliographische Detailangaben
Hauptverfasser:	CABANAC, JEAN-PIERRE, GUITTARD, DOMINIQUE, ROGER, JANY
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES 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 GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The process involves presenting a panel and a plate (3) in stack, and piercing the stack to form a fixation hole. A fixing rod (8) is inserted into the fixation hole. A negative clearance between diameters of the fixation hole and the rod is created during the piercing process. The rod is inserted over the panel and drawn in a direction of a reacting plate while assembling the rod onto the hole. An independent claim is also included for an aircraft including a laminated structure.