LIGHTNING DAMAGE RESISTANT ONE SIDED INSTALLATION

A fastener assembly (10) includes a bolt (12) having a head (14) and having a shank (16). The shank defines threads, the bolt defines a channel (20) which extends circumferentially about the bolt, and the head defines multiple head channels (22) with a first end of each of the multiple head channels...

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Bibliographische Detailangaben
1. Verfasser:	KHOSRAVANI, SHAHRIAR
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:	A fastener assembly (10) includes a bolt (12) having a head (14) and having a shank (16). The shank defines threads, the bolt defines a channel (20) which extends circumferentially about the bolt, and the head defines multiple head channels (22) with a first end of each of the multiple head channels in communication with the channel (20) and a second end of each of the multiple head channels in communication with an outside of the head positioned at a top surface of the head (14). The fastener assembly further includes a sleeve (32) having threads compatible for engaging the threads of the bolt. The sleeve includes a portion of the sleeve including an annealed material (36) and multiple slots (38) defined through the sleeve. With the bolt positioned within the sleeve, each of the multiple slots (38) defined through the sleeve is positioned in communication with the channel (20).