Abstract: A first shock isolator is provided that includes an axial compression element, a first disc spring, a disc spring system, and an annular stand-off. The first disc spring has a non-linear load-deflection response. The disc spring system is configured to be deflected by the first disc spring and has a linear load-deflection response. A second shock isolator is provided that includes an axial compression element, first and second disc springs and corresponding first and second annular stand-offs. The first and second disc springs have non-linear load-deflection responses. The first and second annular stand-offs hold the first disc and second disc springs in a spaced apart parallel configuration. The second disc spring is configured to be deflected by the first disc spring. The first and second shock isolators exhibit first and second combined load-deflection curves that include a constant load region.

Abstract: A first shock isolator is provided that includes an axial compression element, a first disc spring, a disc spring system, and an annular stand-off. The first disc spring has a non-linear load-deflection response. The disc spring system is configured to be deflected by the first disc spring and has a linear load-deflection response. A second shock isolator is provided that includes an axial compression element, first and second disc springs and corresponding first and second annular stand-offs. The first and second disc springs have non-linear load-deflection responses. The first and second annular stand-offs hold the first disc and second disc springs in a spaced apart parallel configuration. The second disc spring is configured to be deflected by the first disc spring. The first and second shock isolators exhibit first and second combined load-deflection curves that include a constant load region.

Abstract: A first shock isolator is provided that includes an axial compression element, a first disc spring, a disc spring system, and an annular stand-off. The first disc spring has a non-linear load-deflection response. The disc spring system is configured to be deflected by the first disc spring and has a linear load-deflection response. A second shock isolator is provided that includes an axial compression element, first and second disc springs and corresponding first and second annular stand-offs. The first and second disc springs have non-linear load-deflection responses. The first and second annular stand-offs hold the first disc and second disc springs in a spaced apart parallel configuration. The second disc spring is configured to be deflected by the first disc spring. The first and second shock isolators exhibit first and second combined load-deflection curves that include a constant load region.

Abstract: Embodiments are directed towards a helmet adapted for use by a human being for a variety of activities. The helmet includes a shell, a plurality of FAEs, and at least one rigid component. The shell maybe configured and arranged to cover a portion of a wearer's head. The plurality of FAEs may be separately positioned adjacent to the shell's interior surface. Each FAE may include at least one disc spring that is adapted for absorbing forces. The at least one rigid component may be disposed within the shell and adjacent to the plurality of FAEs. In this way, the FAEs may be between the shell's interior surface and the at least one rigid component. When a force is applied to a location on the shell's exterior surface, it may be substantially absorbed by at least one of the FAEs positioned adjacent to the location on the shell's interior surface.

Abstract: Embodiments are directed towards a helmet adapted for use by a human being for a variety of activities. The helmet includes a shell, a plurality of FAEs, and at least one rigid component. The shell maybe configured and arranged to cover a portion of a wearer's head. The plurality of FAEs may be separately positioned adjacent to the shell's interior surface. Each FAE may include at least one disc spring that is adapted for absorbing forces. The at least one rigid component may be disposed within the shell and adjacent to the plurality of FAEs. In this way, the FAEs may be between the shell's interior surface and the at least one rigid component. When a force is applied to a location on the shell's exterior surface, it may be substantially absorbed by at least one of the FAEs positioned adjacent to the location on the shell's interior surface.

Abstract: A fiber-reinforced resin composite and method of making the same. The fiber-reinforced resin composite includes a polymeric resin matrix and a plurality of fibers coated with a first distortional polymeric resin. The polymeric resin matrix has a first von Mises strain. The first distortional polymeric resin has a second von Mises strain in a range of approximately 0.25 to approximately 0.45. The plurality of fibers coated with the first distortional polymeric resin are disposed in the polymeric resin matrix. The second von Mises strain is greater than the first von Mises strain.

Abstract: A fiber-reinforced resin composite and method of making the same. The fiber-reinforced resin composite includes a polymeric resin matrix and a plurality of fibers coated with a first distortional polymeric resin. The polymeric resin matrix has a first von Mises strain. The first distortional polymeric resin has a second von Mises strain in a range of approximately 0.25 to approximately 0.45. The plurality of fibers coated with the first distortional polymeric resin are disposed in the polymeric resin matrix. The second von Mises strain is greater than the first von Mises strain.