There is provided a fastener able to prevent damage due to environmental factors such as ultraviolet rays, and impact from sanddust, lumps of ice, and raindrops without obstructing a flow of electric shock current that flows along a top surface of an outer skin. The fastener connects an outer skin of an aircraft to a structural member positioned inside this outer skin, and is provided with a dielectric layer arranged to cover one end surface of a head section, and a conductive layer arranged to cover one end surface of this dielectric layer.

 
Web www.patentalert.com

< Translating active Gurney flap to alleviate aircraft wake vortex hazard

< Aircraft flight control systems and methods

> Hybrid fiberglass composite structures and methods of forming the same

> Method and device for varying a flight path of a projectile by intentional tumbling of the projectile

~ 00616