ELECTRICALLY-INSULATING WASHER AND STRUCTURAL ASSEMBLY FOR AN AIRCRAFT WITH SUCH A WASHER

Disclosed is a method of manufacturing an electrical isolation component which comprises overlaying an electrically-insulating outer ply comprising glass fibers on a core preform comprising reinforcing fibers and a thermoplastic matrix material and applying pressure to said outer ply and core prefor...

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Bibliographische Detailangaben
Hauptverfasser:	BALLOCCHI, Paolo, DONALDSON, Nigel, WALSH, Robert
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	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 LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	Disclosed is a method of manufacturing an electrical isolation component which comprises overlaying an electrically-insulating outer ply comprising glass fibers on a core preform comprising reinforcing fibers and a thermoplastic matrix material and applying pressure to said outer ply and core preform, thereby causing consolidation of said reinforcing fibers and matrix material. Pressure is removed and said thermoplastic material hardens, thereby forming a laminate structure from the outer ply and the consolidated reinforcing fibers and matrix material. The reinforcing fibers and said glass fibers are formed of different materials. Also disclosed is an electrical isolation component having a core formed of reinforcing fibers embedded in a thermoplastic matrix material; and an electrically-insulating outer ply overlaying said core.