Austenempering produces a bainite structure with a yield ratio of at least 0.95, enabling precise yield point detection and consistent clamp load maintenance.
Partially threaded pins secure inserts during composite curing, resolving alignment and extraction contradictions.
Rounded terminal surfaces on injection-molded roofing plates prevent punctures and minimize wear by eliminating sharp edge stress concentrations.
Embedded elongated limiters with higher compressive modulus bear fastener loads, reducing weight by 95% compared to steel.
A sealing screw uses an elastomer washer and sealant to maintain thread engagement.
A breakaway bushing maintains a securing member in an upright position, then separates to enable direct metal-on-metal contact and prevent stripping.
A plastic fastening element incorporates a cast metal threaded bush to secure facade components without forming cold bridges.
Pre-applied dielectric coatings on fasteners eliminate time-consuming sealant curing while reducing aircraft weight and preventing lightning-induced arcing.
Radial expansion of a multi-piece tubular section accommodates varying workpiece opening lengths, eliminating the need for multiple bracket sizes.