Ballistic resistant cap nut
AssigneeThe Boeing Company
InventorsDavid S. Melberg, James J. Kunda
Life of this patent
Estimating the term…
Loading patent…
AssigneeThe Boeing Company
InventorsDavid S. Melberg, James J. Kunda
Estimating the term…
A self locking fastener system is disclosed for light-weight ballistic resistant applications. The fastener system includes a ballistic resistant cap nut with an integral shoulder. The shoulder is formed onto the mating surface of the cap nut and is keyed to lock with a cut-out in a structural member to which the fastener system is secured. In a commercial aircraft, the cap nut is located on the passenger cabin side of the ballistic resistant flight deck door and prevents tampering therewith that might otherwise lead to disassembly or damage to the fastener system and degrade the ballistic resistance of the door assembly. Thus provided, the fastener system is resistant to removal by manipulation of the cap nut as well as damage from ballistic projectiles. The shoulder of the cap nut increases the shear area of the fastener along the plane of the mating surface thereby enhancing the fastener's resistance to shear loading. The cap nut is constructed of titanium or stainless steel.
A tamper and ballistic resistant fastener system comprising:
A ballistic resistant and tamper proof fastener assembly adapted for use on a flight deck wall, wherein the flight deck wall demarcates a flight deck area and a passenger cabin area, the fastener assembly comprising:
Dependencies are inferred from the claim text.