METHOD FOR ATTACHING A COMPONENT TO AN INTERNAL PORTION OF AN AIRCRAFT FUSELAGE

A method for attaching a component to an internal portion of an aircraft fuselage is disclosed herein. The method includes, but is not limited to, mounting a vibration isolator assembly to the internal portion of the aircraft fuselage. The vibration isolator assembly has a protruding engagement port...

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Bibliographische Detailangaben
1. Verfasser:	LUCAS, MICHAEL EUGENE
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COMBINED OPERATIONS 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 GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HELICOPTERS LIGHTING MACHINE TOOLS MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR OTHER WORKING OF METAL PERFORMING OPERATIONS SHOCK-ABSORBERS SPRINGS TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS THERMAL INSULATION IN GENERAL TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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Beschreibung
Zusammenfassung:	A method for attaching a component to an internal portion of an aircraft fuselage is disclosed herein. The method includes, but is not limited to, mounting a vibration isolator assembly to the internal portion of the aircraft fuselage. The vibration isolator assembly has a protruding engagement portion having a flange. The method further includes, but is not limited to defining an opening in a vibration-deadening body. The method further includes, but is not limited to positioning the vibration-deadening body over the vibration isolator such that the protruding engagement portion is received within the opening. The method further includes, but is not limited to pressing a retaining member onto the protruding engagement portion such that the retaining member engages the flange. L'invention porte sur un procédé pour attacher un composant à une partie interne d'un fuselage d'aéronef. Le procédé met en oeuvre, mais sans y être limité, le montage d'un ensemble d'isolateur vis-à-vis des vibrations sur la partie interne du fuselage d'aéronef. L'ensemble d'isolateur vis-à-vis des vibrations a une partie de prise saillante ayant une bride. Le procédé met de plus en oeuvre, mais sans y être limité, la définition d'une ouverture dans un corps d'étouffement des vibrations. Le procédé met de plus en oeuvre, mais sans y être limité, le positionnement du corps d'étouffement des vibrations sur l'isolateur vis-à-vis des vibrations de telle sorte que la partie de prise saillante est reçue à l'intérieur de l'ouverture. Le procédé met de plus en oeuvre, mais sans y être limité, le pressage d'un élément de retenue dans la partie de prise saillante de telle sorte que l'élément de retenue vient en prise avec la bride.