Shock mitigation apparatus and system
View Patent ↗Embodiments employ venting features and damping components both inside and concentric to a fuzewell to improve munition fuze survivability. Damping components are selected based on their densities and stiffness properties. A shock damping liner with longitudinal grooves is affixed to an inner surface of the fuzewell and envelops the fuze. At least one shock damping collar constrains and attenuates shock experienced by the fuze. A shock damping ring is concentric about the outer surface of the fuzewell and attenuates shock between the outermost munition system layer (the casing) and the fuzewell. Longitudinal vents in the fuzewell wall and radial apertures oriented transverse to the longitudinal vents are used for off-gassing. The venting and component orientation combination provides increased damping, resulting in impedance mismatches across multiple interface surfaces in the munition, which reduces shock vibrational pressures and stresses transferred to the fuze.
1. A shock mitigation apparatus, comprising:
a hollow fuzewell having a proximal end, a distal end, an inner surface, an outer surface, and a wall defined by said inner surface and said outer surface, said hollow fuzewell centered about a central longitudinal axis;
wherein said outer surface having a first outer portion and a second outer portion, said first outer portion corresponding to said proximal end, said second outer portion corresponding to said distal end, said first and second outer portions separated by a flared region;
a booster housing inside said hollow fuzewell at said proximal end, wherein said booster housing is concentric about a thermally-softening booster cup;
a plurality of longitudinal vents circumferentially-spaced at equal distance in said wall, said plurality of longitudinal vents spanning longitudinally, parallel to said central longitudinal axis, from said outer surface at said flared region and through said wall to said distal end;
a shock damping liner affixed to said inner surface, said shock damping liner having a plurality of longitudinal grooves parallel to said central longitudinal axis; and
a shock damping ring concentric about said hollow fuzewell.
2. The apparatus according to claim 1 , wherein said outer surface is threaded along said second outer portion.
3. The apparatus according to claim 1 , further comprising an air gap conduit adjacent to said inner surface at said proximal end, wherein said air gap conduit is concentric about said booster housing and separates said booster housing from said inner surface.
4. The apparatus according to claim 1 , wherein said inner surface defining a fuzewell inner envelope having a first inner portion, a second inner portion, and a third inner portion, wherein said first inner portion is located at said proximal end, said third inner portion is located at said distal end, wherein said second inner portion separates said first and third inner portions.
5. The apparatus according to claim 4 , further comprising at least one shock damping collar affixed to said third inner portion.
6. The apparatus according to claim 5 , wherein said at least one shock damping collar is plastic.
7. The apparatus according to claim 4 , wherein said shock damping liner is affixed to said second inner portion.
8. The apparatus according to claim 1 , wherein said shock damping liner is selected from the group of materials consisting of a plastic-carbon mix, conductive ultra high molecular weight polyethylene, low density polyethylene mixed with carbon, high density polyethylene mixed with carbon, polyamides, and polytetrafluoroethylene (PTFE).
9. The apparatus according to claim 1 , wherein said booster housing is a metal sleeve.
10. The apparatus according to claim 1 , wherein said thermally-softening booster cup is a polymer.
11. The apparatus according to claim 1 , wherein said booster housing having a plurality of circumferentially-spaced holes.
12. The apparatus according to claim 1 , wherein said shock damping ring is a reinforced polymer.
13. The apparatus according to claim 1 , further comprising a plurality of radial apertures, each radial aperture in said plurality of radial apertures having a proximal end at said inner surface and a distal end at said flared region of said outer surface.