Process for installing fatigue-rated rivets
AssigneeThe Boeing Company
InventorDavid Lee Wagner
Life of this patent
Estimating the term…
Loading patent…
AssigneeThe Boeing Company
InventorDavid Lee Wagner
Estimating the term…
A process of forming an interference fit between a rivet and the perimeter of an aperture through which the rivet shank is inserted finds particular application in the aircraft industry where sheets of component materials are joined together as a sheet assembly by a plurality of rivets. The process utilizes a high energy impact gun which forms a button on one end of a rivet shank, the other end of the rivet shank protruding a predetermined distance from a sheet surface and prevented from longitudinal movement by a bucking bar. The impact gun is then activated against the other end to rapidly form a second button. The rivet shank is radially expanded during the riveting process to thereby swell against the perimeter of the rivet hole for compression stressing which serves to stress relieve the area adjacent to the hole during cyclic loading of a sheet assembly.
A method of forming an interference fit between a rivet shank and the perimeter of an aperture through which the rivet shank is inserted comprising:
A method of forming an interference fit between a rivet shank and the perimeter of apertures arranged in components to be assembled together comprising:
Dependencies are inferred from the claim text.