Shock attenuation device with stacked nonviscoelastic layers

US9835429B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9835429-B2
Application numberUS-201514918677-A
CountryUS
Kind codeB2
Filing dateOct 21, 2015
Priority dateOct 21, 2015
Publication dateDec 5, 2017
Grant dateDec 5, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A shock attenuation device is used to reduce the effect of a blast shock by both disrupting the propagation of the shock and by spreading, deflecting, and/or redirecting the shock. The device includes multiple layers of different materials, having different shock transmission impedances, stacked in a direction in which the blast shock travels through the device. At least one of the layers includes a material that crumples in response to the shock, undergoing an inelastic deformation in response to the shock. Also, at least one of the layers includes a material that has a directional shock transmission impedance that provides different shock transmission impedance within different directions within the material. The directional shock transmission material may be oriented such that the preferred direction of shock transmission within the material is oriented away from the direction of in which the multiple layers of material are stacked.

First claim

Opening claim text (preview).

What is claimed is: 1. A munition comprising: a shock attenuation device that includes a pair of stacked layers of non-viscoelastic shock-attenuation material in contact with one another; wherein the stacked layers include at least one layer of crushable material; wherein the layers have different shock transmission impedances; and wherein the layers have different directional shock transmission characteristics; wherein the shock attenuation device is located at least in part between a warhead of the munition and a penetrator of the munition; and wherein the layers divert around the penetrator an incipient shock from detonation of the warhead. 2. The munition of claim 1 , wherein one of the layers has ordered directional shock transmission characteristics that divert an incipient shock in a first direction. 3. The munition of claim 2 , wherein the other of the layers has non-directional shock transmission characteristics. 4. The munition of claim 2 , wherein the other of the layers has ordered directional shock transmission characteristics that divert an incipient shock in a second direction that is different than the first direction. 5. The munition of claim 1 , wherein the layers include a third layer, stacked on the pair of stacked layers, that has one or more of a different shock transmission impedance than the shock transmission impedances of the pair of stacked layers, and different directional shock transmission characteristics that the shock transmission characteristics of the pair of stacked layers. 6. The munition of claim 1 , wherein the layers include additional layers on the pair of stacked layers, with the additional layers repeating a pattern set by the pair of stacked layers. 7. The munition of claim 1 , wherein at least one of the layers has voids therein. 8. The munition of claim 7 , wherein the at least one of the layers has pillars of material surrounded by the voids. 9. The munition of claim 1 , wherein at least one of the layers has pillars therein. 10. The munition of claim 1 , wherein one of the layers is a wood layer. 11. The munition of claim 10 , wherein the wood layer has ordered directional shock transmission characteristics. 12. The munition of claim 1 , wherein one of the layers is a composite fiber material layer. 13. The munition of claim 12 , wherein the composite fiber material layer has ordered directional shock transmission characteristics. 14. The munition of claim 1 , wherein one of the layers is a corrugated material layer. 15. The munition of claim 1 , wherein one of the layers is a honeycomb material layer. 16. The munition of claim 1 , wherein one of the layers is a metal layer.

Assignees

Inventors

Classifications

  • F42D5/045Primary

    Detonation-wave absorbing or damping means · CPC title

  • using plastic deformation of members {(F16F9/30 takes precedence; yieldable means for mounting bumpers on vehicles B60R19/26; yieldable or collapsible steering columns B62D1/192)} · CPC title

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What does patent US9835429B2 cover?
A shock attenuation device is used to reduce the effect of a blast shock by both disrupting the propagation of the shock and by spreading, deflecting, and/or redirecting the shock. The device includes multiple layers of different materials, having different shock transmission impedances, stacked in a direction in which the blast shock travels through the device. At least one of the layers inclu…
Who is the assignee on this patent?
Raytheon Co
What technology area does this patent fall under?
Primary CPC classification F42D5/045. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 05 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).