FIELD OF THE INVENTION

[0001] Embodiments relate to a flame barrier, particularly to an ultra-thin, lightweight flame strike face and methods of making and using thereof.

BACKGROUND OF THE INVENTION

[0002] The present disclosure relates to an ultra-thin, lightweight flame strike face that displays improved performance over existing lightweight flame barriers.

[0003] Currently, lightweight flame barriers, as used in aircraft or vehicles, are typically designed as parasitic layers that are attached to an existing structure and optimized for weight, insulation, and direct temperature capability. Current flame barriers typically insulate the existing structure against degradation from flame exposure through the use of non-woven or thin-veil fibers, which have a melt-temperature above that of the flame they are designed to withstand. Additionally, flame barriers often have a film or foil that acts as a carrier, protective outer surface, and/or radiant barrier on one or both sides of the insulation material. However, current flame barriers remain susceptible to degradation from the combination of high temperature flames (e.g., over 2000°F), direct flame impingement, and high air/fuel velocity. Current flame barriers are also noticeably deficient against aggressive flames, molten electrolyte expulsion, hydrofluoric acid exposure, and/or burning metal particles detached from a failed battery, such as in battery thermal runaway events. Generally, the market is full of flame and fire protection barriers and apparatuses configured for use against flames of 1500-2000°F. However, fires become more complex and energetic at higher temperatures (e.g., lithium battery fires), and current solutions become exotic, complex, and expensive. There are no lightweight, cost- effective systems capable of augmenting the multitude of existing fire-resistant products against flames greater than 3000°F and/or adding front-face protection against molten electrolyte or burning metal particles present in high temperature fires.

[0004] Accordingly, there is a need for a lightweight flame barrier that acts as an initial protective layer, protects against high temperature flames, prevents flame penetration, and contains aggressive flames to reduce the severity of the flame’s impact, heat, and velocity on subsequent layers. The inventive flame barrier is an economic solution in view of current technology.

SUMMARY OF THE INVENTION

[0005] Embodiments relate to a strike face that may be adhered or mechanically fastened to a substrate to provide fire resistance and an outer protective surface. The strike face may alternatively be adhered to an existing flame barrier to provide increased fire resistance and increased protective ability against more energetic, higher temperature flame events.

[0006] In an exemplary embodiment, a flame barrier comprises a primary layer comprising a metal foil sublayer having a thickness not greater than 0.002 inches, wherein the primary layer is attached to a substrate, and wherein the flame barrier is configured to maintain a cold side temperature of 600°F or less in an environment with temperatures up to 2750°F.

[0007] In some embodiments, the metal foil sublayer has a thickness not greater than 0.001 inches.

[0008] In some embodiments, the metal foil sublayer has a thickness not greater than 0.0005 inches.

[0009] In some embodiments, the metal foil sublayer has a thickness not greater than 0.00007 inches. [0010] In some embodiments, the metal foil sublayer comprises a metal selected from the group consisting of alloy steels, aluminum (and alloys), brass, bronze, carbon steel, cobalt (and alloys), Constantan® foil (Cu55Ni), copper (and alloys), Evanohm® foil (Ni75Cr20A12.5Cu2.5), gold (and alloys), iron (and allows), magnesium (and alloys), nickel (and alloys), nickel-base super alloys (e.g., Inconel®), niobium (and alloys), stainless steel (e g., stainless steel type 309, stainless steel type 321), tantalum (and alloys), tin (and alloys), titanium (and alloys), tungsten (and alloys), yttrium (and alloys), and zinc (and alloys).

[0011] In some embodiments, the primary layer is mechanically fastened to the substrate. [0012] In some embodiments, the primary layer is attached to the substrate via an adhesive.

[0013] In some embodiments, the adhesive comprises at least one inorganic fusible salt and an aqueous binder solution.

[0014] In some embodiments, the at least one inorganic fusible salt comprises sodium silicate.

[0015] In some embodiments, the flame barrier is configured to maintain a cold side temperature of 600°F or less in an environment with temperatures up to 3250°F.

[0016] In some embodiments, the flame barrier is configured to maintain a cold side temperature of 600°F or less in an environment with temperatures up to 4500°F.

[0017] In some embodiments, the primary layer further comprises a second metal foil sublayer adhered to the metal foil sublayer, wherein the second metal foil sublayer has a thickness not greater than 0.002 inches.

[0018] In some embodiments, the metal foil sublayer consists of a first metal foil and the second metal foil sublayer consists of a second metal foil, wherein the first metal foil is different than the second metal foil. [0019] In some embodiments, the primary layer further comprises a metal sputtering sublayer positioned on the metal foil sublayer.

[0020] In some embodiments, the metal sputtering sublayer comprises a metal selected from the group consisting of alloy steels, aluminum (and alloys), brass, bronze, carbon steel, cobalt (and alloys), Constantan® foil (Cu55Ni), copper (and alloys), Evanohm® foil (Ni75Cr20A12.5Cu2.5), gold (and alloys), iron (and allows), magnesium (and alloys), nickel (and alloys), nickel-base super alloys (e.g., Inconel®), niobium (and alloys), stainless steel (e.g., stainless steel type 309, stainless steel type 321), tantalum (and alloys), tin (and alloys), titanium (and alloys), tungsten (and alloys), yttrium (and alloys), and zinc (and alloys).

[0021] In some embodiments, the primary layer further comprises an armor sublayer adhered to the metal foil sublayer.

[0022] In some embodiments, the primary layer further comprises an insulating sublayer adhered to the metal foil sublayer.

[0023] In some embodiments, the insulating sublayer comprises a material selected from the group consisting of woven silica fabric, woven vermiculite coated fiberglass, non-woven silica fiber, and woven aramids.

[0024] In an exemplary embodiment, a flame barrier comprises a primary layer comprising a metal foil sublayer having a thickness not greater than 0.002 inches; and a secondary layer adhered to the primary layer via an adhesive, wherein the secondary layer is attached to a substrate, and wherein the flame barrier is configured to maintain a cold side temperature of 600°F or less in an environment with temperatures up to 2750°F.

[0025] In some embodiments, the secondary layer is mechanically fastened to the substrate. [0026] In some embodiments, the secondary layer is attached to the substrate via an adhesive. [0027] In some embodiments, the adhesive comprises at least one inorganic fusible salt and an aqueous binder solution.

[0028] In some embodiments, the at least one inorganic fusible salt comprises sodium silicate.

[0029] In some embodiments, the flame barrier is configured to maintain a cold side temperature of 600°F or less in an environment with temperatures up to 3250°F.

[0030] In some embodiments, the flame barrier is configured to maintain a cold side temperature of 600°F or less in an environment with temperatures up to 4500°F.

[0031] In some embodiments, the secondary layer comprises at least one insulating sublayer.

[0032] In some embodiments, the at least one insulating sublayer comprises a material selected from the group consisting of woven silica fabric, woven vermiculite coated fiberglass, nonwoven silica fiber, and woven aramids.

[0033] In some embodiments, the secondary layer comprises a laminate sublayer.

[0034] In some embodiments, the laminate sublayer comprises be a material selected from the group consisting of basalt, para-aramid, meta-aramid, carbon, graphite, and glass fiber construction.

[0035] In some embodiments, the metal foil sublayer comprises a metal selected from the group consisting of alloy steels, aluminum (and alloys), brass, bronze, carbon steel, cobalt (and alloys), Constantan® foil (Cu55Ni), copper (and alloys), Evanohm® foil (Ni75Cr20A12.5Cu2.5), gold (and alloys), iron (and allows), magnesium (and alloys), nickel (and alloys), nickel-base super alloys (e.g., Inconel®), niobium (and alloys), stainless steel (e.g., stainless steel type 309, stainless steel type 321), tantalum (and alloys), tin (and alloys), titanium (and alloys), tungsten (and alloys), yttrium (and alloys), and zinc (and alloys). [0036] In some embodiments, the primary layer further comprises a second metal foil sublayer adhered to the metal foil sublayer, wherein the second metal foil sublayer has a thickness not greater than 0.002 inches.

[0037] In some embodiments, the metal foil sublayer consists of a first metal foil and the second metal foil sublayer consists of a second metal foil, wherein the first metal foil is different than the second metal foil.

[0038] In some embodiments, the primary layer further comprises an insulating sublayer adhered to the metal foil sublayer.

[0039] In some embodiments, the insulating sublayer comprises a material selected from the group consisting of woven silica fabric, woven vermiculite coated fiberglass, non-woven silica fiber, and woven aramids.

BRIEF DESCRIPTION OF THE DRAWINGS

[0040] The above and other objects, aspects, features, advantages and possible applications of the present innovation will be more apparent from the following more particular description thereof, presented in conjunction with the following drawings. Like reference numbers used in the drawings may identify like components.

[0041] FIGS. 1A-1B show exploded cross-sectional views of exemplary embodiments of the flame barrier.

[0042] FIGS. 2A-2D show exploded cross-sectional views of exemplary embodiments of the flame barrier wherein the secondary layer comprises one or more sublayers.

[0043] FIGS. 3A-3G show exploded cross-sectional views of exemplary embodiments of the flame barrier wherein the primary layer comprises one or more sublayers. [0044] FIG. 4 shows an exploded cross-sectional view of an exemplary embodiment of the flame barrier including an air gap.

[0045] FIGS. 5A-5B show exploded cross-sectional views of exemplary embodiments of the flame barrier including a thin paper facing.

[0046] FIGS. 6-8 show exploded views of exemplary uses of exemplary embodiments of the flame barrier.

[0047] FIG. 9 shows test results of exemplary embodiments of the flame barrier.

DETAILED DESCRIPTION OF THE INVENTION

[0048] The following description is of exemplary embodiments and methods of use that are presently contemplated for carrying out the present invention. This description is not to be taken in a limiting sense, but is made merely for the purpose of describing the general principles and features of various aspects of the present invention. The scope of the present invention is not limited by this description.

[0049] In an exemplary embodiment shown in FIG 1A, a strike face 100 has a primary layer 102 and a secondary layer 104. An adhesive 106 attaches the primary layer 102 to the secondary layer 104. The strike face 100 may have an inside surface 108 and an outside surface 110. The inside surface 108 may be defined as the surface configured to attach the strike face 100 to a substrate 112. The outside surface 110 may be defined as the surface configured to be exposed (e.g., to a flame). In exemplary embodiments, the secondary layer 104 comprises the inside surface 108 of the strike face 100 and the primary layer 102 comprises the outside surface 110 of the strike face 100. [0050] In an alternative embodiment shown in FIG. IB, a strike face 100 has a primary layer

102, wherein the primary layer 102 comprises both the inside surface 108 of the strike face 100 and the outside surface 110 of the strike face 100.

[0051] The strike face 100 is configured to protect a substrate 112 from high temperatures and to increase the time in which a substrate 112 may withstand flame impingement and high temperatures. The strike face 100 may protect a substrate 112 from flames of temperatures up to 2750°F, up to 3250°F, and in some embodiments, up to 4500°F. The strike face 100 is further configured to maintain a cold side temperature of less than 600°F without insulation. The cold side temperature may be defined as the temperature measured at the inside surface 108 of the strike face 100. It is contemplated that the cold-side temperature may be tailored based on the number of layers comprising the strike face 100.

[0052] It is contemplated that the strike face 100 may be lightweight to minimize any potential adverse impact on a substrate 112. The strike face 100 may have a weight of 0.03 to 0.5 lbs/ft ² . The weight of the strike face 100 may be modified and optimized depending on a particular use. For example, the strike face may have a weight of 0.08 to 0.2 lbs/ft ² for various ground vehiclebased markets, and a up to 0.5 lbs/ft ² for less weight sensitive residential applications. Generally, the strike face 100 preferably has a weight of 0.03 to 0.1 lbs/ft ² . It is surprising that the strike face 100 may have such a low weight while still maintaining the high temperature protection detailed above. It is further contemplated that the strike face 100 may be flexible, such that the strike face 100 may complement the shape of any substrate 112.

[0053] In embodiments in which the strike face 100 comprises a primary layer 102 and a secondary layer 104, the secondary layer 104 is configured to insulate the substrate 112 from a flame by reducing the rate of heat transfer to the substrate 112. The secondary layer 104 may have a thickness of 0.00069 inches or less (i.e., not greater than 0.00069 inches), 0.0005 inches or less (i.e., not greater than 0.0.0005 inches), or 0.0001 inches or less (i.e., not greater than

0.0.0001 inches). In alternative embodiments, the strike face 100 may not comprise a secondary layer 104 (e.g., the primary layer 102 is used alone).

[0054] It is contemplated that the secondary layer 104 may comprise one or more sublayers (e.g., insulating sublayer 114 and/or laminate sublayer 116).

[0055] In an exemplary embodiment shown in FIG. 2A, the secondary layer 104 may comprise an insulating sublayer 114. In some embodiments, the insulating sublayer 114 is not inherently flammable and inorganic. The insulating sublayer 114 may be a material such as, but not limited to, woven silica fabric, woven vermiculite coated fiberglass, non-woven silica fiber, woven aramids, or any other suitable material and mixtures thereof. It is contemplated that the insulating sublayer 114 may comprise the inside surface 108 of the strike face 100 and be configured to attach to a substrate 112.

[0056] In an exemplary embodiment shown in FIG. 2B, the secondary layer 104 may comprise a plurality of insulating sublayers 114 as described above. The plurality of insulating sublayers 114 may be configured as consecutive layers. An adhesive 106 may attach the plurality of insulating sublayers 114 to one another. As used herein, insulating sublayer 114 generally describes sublayers 114’ and/or 114”. It is contemplated that the insulating sublayer 114’ may comprise the same material as or a different material than the insulating sublayer 114”. It is further contemplated that the insulating sublayer 114’ may comprise the same thickness as or a different thickness than the insulating sublayer 114”.

[0057] In an exemplary embodiment shown in FIGS. 2C and 2D, the secondary layer 104 may comprise a laminate sublayer 116. In some embodiments, the laminate sublayer 116 is not inherently flammable. The laminate sublayer 116 may be a material such as, but not limited to, basalt, para-aramid, meta-aramid, carbon, graphite, glass fiber construction, or any other suitable material and mixtures thereof. It is contemplated that an adhesive 106 may attach the insulating sublayer 114 or the plurality of insulating sublayers 114 to the laminate sublayer 116, such that the laminate sublayer 116 may comprise the inside surface 108 of the strike face 100 and be configured to attach to a substrate 112.

[0058] The primary layer 102 is configured to protect against high temperature flames and prevent flame penetration. The primary layer 102 may further be configured to protect against impact.

[0059] It is contemplated that the primary layer 102 may comprise one or more sublayers (e.g., at least one metal foil sublayer 118, a metal sputtering sublayer 120, an insulating sublayer 122, or an armor sublayer 124, or any combination thereof).

[0060] In an exemplary embodiment shown in FIGS. 3A and 3B, the primary layer 102 may comprise a metal foil sublayer 118. The metal foil sublayer 118 may be any metal or refractory metal with a melting temperature greater than or equal to 2200°F. The metal foil sublayer 118 may be a foil such as, but not limited to, alloy steels, aluminum (and alloys), brass, bronze, carbon steel, cobalt (and alloys), Constantan® foil (Cu55Ni), copper (and alloys), Evanohm® foil (Ni75Cr20A12.5Cu2.5), gold (and alloys), iron (and allows), magnesium (and alloys), nickel (and alloys), nickel-base super alloys (e.g., Inconel®), niobium (and alloys), stainless steel (e.g., stainless steel type 309, stainless steel type 321), tantalum (and alloys), tin (and alloys), titanium (and alloys), tungsten (and alloys), yttrium (and alloys), zinc (and alloys), or any other suitable foil and mixtures thereof. [0061] The metal foil sublayer 118 may have a thickness of 0.002 inches or less (i.e., not greater than 0.0.002 inches), 0.001 inches or less (i.e., not greater than 0.0.001 inches), 0.0005 inches or less (i.e., not greater than 0.0005 inches), or more preferably 0.00007 inches or less (i.e., not greater than 0.00007 inches). It is noted that foil layers are not commercially available at these thicknesses and thus existing flame barrier systems do not use or teach foil layers at these thicknesses. It is contemplated that the metal foil sublayer 118 may comprise the outside surface 110 of the strike face 100 and be configured to be exposed (e.g., to a flame). It is contemplated that the metal foil sublayer 118 has a high thermal conductivity, such that the primary layer 102 may continuously resist flame penetration and move heat away from the flame zone to spread heat over a larger area. This is advantageous as it reduces both the severity of the flame impact on subsequent layers and increases the time in which the strike face 100 can withstand flame impingement.

[0062] In an exemplary embodiment shown in FIGS. 3C and 3D, the primary layer 102 may comprise a plurality of metal foil sublayers 118 as described above. The plurality of metal foil sublayers 118 may be configured as consecutive layers. An adhesive 106 may attach the plurality of metal foil sublayers to one another. As used herein, metal foil sublayer 118 generally describes sublayers 118’ and/or 118”. It is contemplated that the metal foil sublayer 118’ may comprise the same foil as or a different foil than the metal foil sublayer 118”. For example, a first metal foil sublayer may be stainless steel and a second metal foil sublayer may be aluminum, copper, zinc. etc. It is further contemplated that the metal foil sublayer 118’ may comprise the same thickness as or a different thickness than the metal foil sublayer 118”.

[0063] In an exemplary embodiment shown in FIG. 3E, the primary layer 102 may comprise a metal sputtering sublayer 120 (e.g., via sputter deposition methods). The metal sputtering sublayer 120 may be a metal such as, but not limited to, alloy steels, aluminum (and alloys), brass, bronze, carbon steel, cobalt (and alloys), Constantan® foil (Cu55Ni), copper (and alloys),

Evanohm® foil (Ni75Cr20A12.5Cu2.5), gold (and alloys), iron (and allows), magnesium (and alloys), nickel (and alloys), nickel-base super alloys (e.g., Inconel®), niobium (and alloys), stainless steel (e.g., stainless steel type 309, stainless steel type 321), tantalum (and alloys), tin (and alloys), titanium (and alloys), tungsten (and alloys), yttrium (and alloys), zinc (and alloys), or any other suitable foil and mixtures thereof. The metal sputtering sublayer 120 may be any metal or refractory metal with a melting temperature greater than or equal to 2200°F. It is contemplated that the metal sputtering sublayer 120 may comprise the outside surface 110 of the strike face 100 and be configured to be exposed (e g., to a flame). It is further contemplated that the sputtering sublayer 120 may be positioned on a metal foil sublayer 118.

[0064] In exemplary embodiments shown in FIG. 3F, the primary layer 102 may comprise an insulating sublayer 122. It is contemplated that an adhesive 106 may attach the metal foil sublayer 118 or the plurality of metal foil sublayers 118 to the insulating sublayer 122, such that the insulating sublayer 122 may be positioned on top of the metal foil sublayer 118 or the plurality of metal foil sublayers 118. It is further contemplated that an adhesive 106 may attach the sputtering sublayer 120 to the insulating sublayer 122, such that the insulating sublayer 122 may be positioned on top of the sputtering sublayer 120. It is contemplated that the insulating sublayer 122 may comprise the outside surface 110 of the strike face 100 and be configured to be exposed (e.g., to a flame).

[0065] In an exemplary embodiment shown in FIG. 3G, the primary layer 102 may comprise an armor sublayer 124. The armor sublayer 124 may be configured to absorb energy and damage. It is contemplated that an adhesive 106 may attach the metal foil sublayer 118 or the plurality of metal foil sublayers 118 to the armor sublayer 124, such that the armor sublayer 124 may be positioned on top of the metal foil sublayer 118 or the plurality of metal foil sublayers 118. It is further contemplated that an adhesive 106 may attach the sputtering sublayer 120 to the armor sublayer 124, such that the armor sublayer 124 may be positioned on top of the sputtering sublayer 120. It is contemplated that the armor sublayer 124 may comprise the outside surface 110 of the strike face 100 and be configured to be exposed (e.g., to a flame).

[0066] In an exemplary embodiment shown in FIG. 4, there may be an air gap 126 between the primary layer 102 and the secondary layer 104. An air gap is understood to mean a break (e.g., empty space) between two objects (e.g., the primary layer 102 and the secondary layer 104). For example, adhesive 106 may attach the primary layer 102 and the secondary layer 104 at discrete points, and an air gap 126 may form between said points. It is contemplated that there may be an air gap 126 between sublayers (e.g., metal foil sublayer 118, insulating sublayer 122, armor sublayer 124, etc.) within the primary layer 102. It is further contemplated that there may be an air gap 126 between sublayers (e.g., insulating sublayer 114, laminate sublayer 116, etc.) within the secondary layer 104.

[0067] In exemplary embodiments wherein more than one layer/sublayer is used (e.g., a primary layer 102 and a secondary layer 104, more than one foil sublayers 118, etc.), the layered materials may form a pillowing effect (not shown) wherein the layers separate under flame impingement. This pillowing effect advantageously introduces an air gap that interrupts conductive heat transfer to the strike face 100.

[0068] In exemplary embodiments shown in FIG. 5A, the primary layer 102 may comprise a thin paper facing 128. It is contemplated that an adhesive 106 may attach the metal foil sublayer 118 or the plurality of metal foil sublayers 118 to the thin paper facing 128, such that thin paper facing 128 may be positioned on top of the metal foil sublayer 118 or the plurality of metal foil sublayers 118. It is further contemplated that an adhesive may attach the sputtering sublayer 120 to the thin paper facing 128, such that the thin paper facing 128 may be positioned on top of the sputtering sublayer 120. It is contemplated that the thin paper facing 128 may comprise the outside surface 110 of the strike face 100 and be configured to be exposed (e g., to a flame). The thin paper facing 128 may have a thickness of 0.002 inches or less (i.e., not greater than 0.002 inches).

[0069] In exemplary embodiments shown in FIG. 5B, the secondary layer 104 may comprise a thin paper facing 128. It is contemplated that the thin paper facing 128 may comprise the inside surface 108 of the strike face 100 and be configured to attach to a substrate 112. The thin paper facing 128 may have a thickness of 0.002 inches or less (i.e., not greater than 0.002 inches). [0070] It is contemplated that the thin paper facing 128 may add electrical insulation and durability to the strike face 100. It is further contemplated the thin paper facing may be lightweight and comprise adhesive compatibility. The thin paper facing 128 may be doped with a polyurethane resin or a polyimide resin filled with titanium and/or tantalum powder.

[0071] The adhesive 106 is configured to attach the primary layer 102 to the secondary layer 104. As described above, the adhesive 106 is further configured to attach one or more sublayers to other sublayers. The adhesive 106 may be a continuous layer, a discrete point, or a series of discrete points.

[0072] It is contemplated that the adhesive 106 is a fire suppressive adhesive. In exemplary embodiments, the adhesive 106 comprises at least one inorganic fusible salt dissolved in an aqueous binder solution. The inorganic fusible salt may be a salt such as, but not limited to, hydrated boron-containing compounds, hydrated sulfate compounds, various hydrated phosphate salts, and hydrated silicates and mixtures thereof. In a preferred embodiment, the salt is sodium silicate (Na2 Si Os, also known as water glass).

[0073] Without wishing to be bound by theory, it is contemplated that the at least one fusible salt contains at least one water molecule bound to an inorganic salt and releases water through dehydration or decomposition when heated. The adhesive 106 creates a barrier to heat transfer and undergoes a chemical reaction upon heating that forms water, cools, and suppresses a fire. During this chemical reaction, heat is absorbed and water vapor is released, thereby providing a cooling effect. Accordingly, the adhesive 106 may act as an inflammable adhesive rather than a flame-retardant adhesive.

[0074] When more than one salt is used, the additional salt (or salts) may have a higher water release threshold temperature. Continuous release of water molecules from the adhesive over a range of temperatures is desirable.

[0075] While not necessary for the success of the strike face 100, it is contemplated that the adhesive 106 may penetrate or partially penetrate the layer or sublayer to which it is applied, thereby impregnating the layer or sublayer.

[0076] While sodium silicate may be employed as the salt to act as a combination adhesive and fire and/or heat barrier, compatible inorganic materials may be added to the sodium silicate to further enhance handling characteristics of the sodium silicate, and/or mechanical properties and/or fire and heat resistance of the resulting strike face. The additives should be soluble in, miscible with, or suspended in the sodium silicate solution, and should be non-reactive with sodium silicate, or, if reactive with the sodium silicate, the resulting reaction product(s) should be intumescent. For example, the additive may be fumed silica, as the addition of fumed silica to the sodium silicate increases the crystallization temperature of the sodium silicate and the fire resistance (combustion temperature) of a strike face produced therefrom.

[0077] Other inorganic salts and oxides, such as ferric oxide, titanium oxide, aluminum trihydrate, sodium aluminum sulfosilicate, antimony trioxide and antimony pentoxide, mica, a carbon material such as carbon black or graphite and mixtures of one or more of the foregoing which are given as exemplary, satisfy some or all of the aforesaid criteria and are useful in accordance with the present invention.

[0078] The adhesive 106 may further comprise other components such as, but not limited to, intumescing materials, expandable graphite, metallic powders (e.g., titanium, tantalum, and/or iron), polyurethane, polyimide, acrylic, acrylate, silicone, thermoplastic films, thermoplastic scrim/webs, or any other suitable component and mixtures thereof. For example, metallic powders may be dispersed within the adhesive.

[0079] It is contemplated that the adhesive 106 may provide resistant to hydrofluoric acid. It is not uncommon for certain lithium-ion batteries to emit hydrofluoric acid (e.g., in liquid, vapor, or gaseous form) when the battery undergoes a catastrophic thermal event. It is contemplated that sodium silicate as the salt in the adhesive 106 may provide such benefits, as sodium silicate is strongly basic and may react with and neutralize emitted hydrofluoric acid.

[0080] As described above, the strike face 100 may be used as a single layer structure, such that the primary layer 102 is adhered to a substrate 112, or the strike face 100 may be used as a multilayer structure, such that the primary layer 102 is adhered to the secondary layer 104 and the layers are adhered to a substrate 112. In alternative embodiments, the strike face 100 may be used as a single layer structure such that the primary layer 102 is mechanically fastened to the substrate 112, or the strike face 100 may be used as a multi-layer structure such that the primary layer is adhered to the second layer 104, and the layers are mechanically fastened to the substrate

112. Mechanical fasteners include, but are not limited to, bolts, screws, rivets, or any other suitable mechanical fastener. It is contemplated that the mechanical fastener may comprise a material such as, but not limited to, steel, titanium, etc.

[0081] In all embodiments, it is contemplated that the strike face 100 may be used with minimal change or redesign of a substrate 112. This advantageously eliminates the need for costly R&D and/or product recertification costs.

[0082] It is contemplated that through modification and optimization of the above-defined elements (e.g., the first layer 102, the second layer 104, the adhesives 106, etc.), the strike face 100 may be used in a wide variety of applications and in conjunction with a wide variety of substrates 112. It is contemplated that the strike face 100 may be formable and may be adhered or mechanically fastened through multiple methods. It is contemplated that the strike face 100 may be used in conjunction with sensitive containment materials. It is contemplated that the substrate 112 may be an existing flame barrier to provide increased fire resistance and increased protective ability.

[0083] The following uses of the above-described strike face are contemplated, though the strike face is in no way limited to the enumerated uses.

[0084] Shipping Container

[0085] In an exemplary use shown in FIG. 6, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with a shipping container, such that the shipping container is the substrate 112. A shipping container may be defined as a container used for shipment, storage, and/or handling of various products, materials, etc. The shipping container may be any shape and be made of any material (e.g., steel, aluminum, fiber-reinforced polymer, etc.).

[0086] For example, the substrate 112 may be a shipping container wherein the inside surface 108 of the strike face 100 may be configured to attach to the composite skin of the shipping container.

[0087] Additionally, the substrate 112 may be a shipping container flexible fabric roll-up door wherein the inside surface 108 of the strike face 100 may be configured to attach to the flexible fabric door of the shipping container.

[0088] Attachment of the strike face 100 to the shipping container may be via adhesive (e.g., adhesive 106) or a mechanical fastening means.

[0089] Aircraft

[0090] In another exemplary use shown in FIG. 7, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with an aircraft, such that the skin of the aircraft is the substrate 112. Exemplary aircraft include commercial aircraft (e.g., airplanes, helicopters, etc.), cargo aircraft, light-sport aircraft, military/fighter aircraft, etc.

[0091] The strike face may be attached to various surfaces (i.e., “skins”) related to the aircraft. For example, the substrate 112 may be an aircraft wherein the inside surface 108 of the strike face 100 may be configured to attach to the interior surface of the aircraft cargo-hold, replacing the traditional “cargo-liner’ while increasing the temperature resistant capabilities above the regulatory minimum temperature capability of 14 CFR 25.853 Part III, Boeing BSS 7323, Airbus AITM 2.0010, FAA Fire Test Handbook Chapter 8. Attachment of the strike face 100 to the cargo-hold may be via adhesive (e.g., adhesive 106) or a mechanical fastening means. [0092] In another exemplary use, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used to lower the temperature that a composite armor panel would see to below that of the degradation temperature of the armor itself. Specifically, the strike face 100 may be used with the commercial aircraft fan-blade containment system, where temperatures are high enough that metallic containment and/or a combination of temperature insulation and traditional composite armor is employed.

[0093] Battery Enclosures (Electric Vehicles)

[0094] In another exemplary use shown in FIG. 8, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with battery enclosures, such as battery enclosures included in electric or hybrid cars, such that the battery enclosure is the substrate 112. For example, the substrate may form the inner surface of a composite or metallic battery enclosure, wherein the inside surface 108 of the strike face 100 may be oriented towards the externally facing outer surfaces of the battery. Similarly, the invention may make up containment cells within a battery enclosure, or may even be a stand-alone structure to provide the safe transport, storage, and handling of bulk lithium ion batteries assembled for electric or hybrid vehicle use. Similarly, the invention may be attached to a composite skid-plate or spall liner that protects the interior of the vehicle (e.g. - battery) from abuse impacts and punctures which could cause thermal runaway of the batteries.

[0095] Attachment of the strike face 100 may be via adhesive (e.g., adhesive 106) or a mechanical fastening means.

[0096] Battery Enclosures (Ballistic Gatling gun)

[0097] Similarly, in another exemplary use, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with battery enclosures for an electrically driven ballistic Gatling gun, such that the battery enclosure is the substrate 112 (see, e.g., FIG. 8). For example, the substrate may form the inner surface of a composite or metallic battery enclosure, wherein the inside surface 108 of the strike face 100 may be oriented towards the externally facing outer surfaces of the battery. Similarly, the invention may make up containment cells within a battery enclosure or may even be a stand-alone structure to provide the safe transport, storage, handling, and use of lithium-ion batteries assembled for electrically driven ballistic Gatling gun use. Attachment of the strike face 100 to the Gatling Gun battery enclosure be via adhesive (e.g., adhesive 106) or a mechanical fastening means.

[0098J Attachment of the strike face 100 may be via adhesive (e.g., adhesive 106) or a mechanical fastening means.

[0099] Battery Enclosures (Electrical Vehicle Take-Off and Landing (eVTOL) Vehicles)

[00100] Similarly, in another exemplary use, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with battery enclosures in eVTOL vehicles, such that the battery enclosure is the substrate 112 (see, e.g., FIG. 8). For example, the substrate may form the inner surface of a composite or metallic battery enclosure, wherein the inside surface 108 of the strike face 100 may be oriented towards the externally facing surfaces of the battery. Similarly, the invention may make up containment cells within a battery enclosure or may even be a stand-alone structure to provide the safe transport, storage, handling, and usage of lithium-ion batteries assembled for eVTOL use.

[00101] Attachment of the strike face 100 may be via adhesive (e.g., adhesive 106) or a mechanical fastening means.

[00102] Battery Enclosures (Electrically Controlled and/or Propelled Ballistic Missiles and Ordnance) [00103] Similarly, in another exemplary use, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with battery enclosures for electrically controlled and/or propelled ballistic missiles and ordnance, such that the battery enclosure is the substrate 112 (see, e.g., FIG. 8). For example, the substrate may form the inner surface of a composite or metallic battery enclosure, wherein the inside surface 108 of the strike face 100 may be oriented towards the externally facing outer surfaces of the battery. Similarly, the invention may make up containment cells within a battery enclosure or may even be a stand-alone structure to provide the safe transport, storage, handling, and use of lithium-ion batteries assembled for electrically controlled and/or propelled ballistic missiles and ordnance. [00104] Attachment of the strike face 100 may be via adhesive (e g., adhesive 106) or a mechanical fastening means.

[00105] Computer Server/Data Rooms

[00106] In another exemplary use, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with computer server/data rooms including batteries used in backup systems. For example, the substrate may form the inner surface of a composite or metallic battery enclosure, wherein the inside surface 108 of the strike face 100 may be oriented towards the externally facing outer surfaces of the battery. Similarly, the invention may make up containment cells within a battery enclosure or may even be a standalone structure to provide the safe transport, storage, usage, and handling of lithium-ion batteries assembled for computer server/data rooms including batteries used in backup systems. Similarly, the invention could be applied to common construction materials to provide a substrate that provides additional fire-rated barriers for garages or other storage rooms where battery charging and storage may occur. [00107] Electrically Driven Watercraft and Propulsion Systems

[00108] In another exemplary use, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with electrically driven watercraft and propulsion systems. For example, the substrate may form the inner surface of a composite or metallic battery enclosure, wherein the inside surface 108 of the strike face 100 may be oriented towards the externally facing outer surfaces of the battery. Similarly, the invention may make up containment cells within a battery enclosure or may even be a stand-alone structure to provide the safe transport, storage, usage, and handling of lithium-ion batteries assembled for electrically driven watercraft and propulsion systems.

[00109] Auxiliary Power Unit (APU) Surround or APU Battery Enclosure

[00110] In another exemplary use, in accordance with an exemplary embodiment of the invention, the strike face 100 may be used in conjunction with an aircraft. For example, the substrate 100 may be an aircraft auxiliary power unit (APU) surround or APU battery enclosure that may be lined with the interior surface 108. The strike face 108 may be oriented inward, firehardening the interior surface of the APU surround or APU battery enclosure while increasing the temperature resistant capabilities above the regulatory minimum and protecting the surrounding traditional containment structure from temperature hot enough to cause structural degradation.

EXAMPLES

[00111] Example 1

[00112] In this example, four flame barrier samples were prepared and tested.

[00113] Sample 1 consisted of a 5-mil (0.005 inches) metal foil layer. Sample 2 consisted of a 2-mil (0.002 inches) metal foil layer. Sample 3 consisted of a 1-mil (0.001 inches) metal foil layer. Sample 4 consisted of a '/z-mil (0.0005 inches) metal foil layer. The metal foil layers correspond to metal foil layer 118 as described above. Samples 1-4 were put through a standard 2750°F torch test for 15-minutes. All of Samples 1-4 provided identical back-face temperature reduction regardless of thickness.

[00114] Samples 1-4 were then “abused” by rolling them into a ball, then flattening and repeating standard testing, with no change in performance.

[00115] Samples 2-4 were then put through a 6-hour 2000°F soak in a kiln, then put through the standard test, left to return to ambient temperature, and put back through a second standard test. No change in performance was observed.

[00116] This level of performance (repeat bums, soak at temperature before bums, abuse before burns), is not common and indicates lower thickness and higher performance are feasible.

[00117] Example 2

[00118] In this example, seven flame barrier samples were prepared and tested.

[00119] Sample 5 (comparative example) consisted of a stainless-steel foil layer and an aramid reinforced thermoset laminate layer. Sample 6 (comparative example) consisted of vermiculite coated fiberglass layer (0.080 inches thick). Sample 7 (comparative example) consisted of a silica fabric layer. Sample 8 (comparative example) consisted of a non-woven silica layer. Sample 9 (comparative example) consisted of an aramid reinforced thermoset laminate layer, a stainless-steel foil layer, and a non-woven silica layer, adhered with Super 77 Bond adhesive.

[00120] Samples 5-9 were tested with a 2,500°F-point load flame exposure for a duration of 270 seconds. These test results are displayed in Table 1.

Table 1: Testing Results

[00121] Each of Samples 5-9 displayed failing results. Sample 5 failed due to the introduction of a particular woven aramid as a fuel source throughout the test, causing flames to erupt from the boundaries of the sample. Samples 6-8 allowed flame penetration and therefore failed. Sample 9 failed due to the adhesive, which generated fuel and added energy to the flame reaction causing burn-through and/or other failing criteria. These samples fail to withstand the high temperatures indicative of lithium-ion battery failure.

[00122] Samples 10 and 11 encompassed exemplary embodiments of the strike face described above. Sample 10 consisted of an aramid reinforced thermoset laminate layer, a stainless-steel foil layer, a carbon layer, and a non-woven silica layer as consecutive layers. Sample 11 consisted of an aramid reinforced thermoset laminate layer, a carbon layer, a stainless-steel foil layer, and a non-woven silica layer as consecutive layers.

[00123] Samples 10 and 11 were tested with a 2,500°F-point load flame exposure for a duration of 240 seconds. These test results are displayed in FIG. 9.

[00124] Each of Samples 10 and 11 displayed passing results. Samples 10 and 11 are capable of a 15-minute exposure to a 2,500°F flame. While individual materials displayed failing results (see Table 1), when combined correctly (e g., Samples 10 and 11), materials may display their most advantageous traits alongside one another to create a high-temperature resistant flame barrier while retaining desired mechanical properties.

[00125] It should be understood that modifications to the embodiments disclosed herein can be made to meet a particular set of design criteria. For instance, the number of or configuration of components or parameters may be used to meet a particular objective.

[00126] It will be apparent to those skilled in the art that numerous modifications and variations of the described examples and embodiments are possible in light of the above teachings of the disclosure. The disclosed examples and embodiments are presented for purposes of illustration only. Other alternative embodiments may include some or all of the features of the various embodiments disclosed herein. For instance, it is contemplated that a particular feature described, either individually or as part of an embodiment, can be combined with other individually described features, or parts of other embodiments. The elements and acts of the various embodiments described herein can therefore be combined to provide further embodiments.

[00127] It is the intent to cover all such modifications and alternative embodiments as may come within the true scope of this invention, which is to be given the full breadth thereof. Additionally, the disclosure of a range of values is a disclosure of every numerical value within that range, including the end points. Thus, while certain exemplary embodiments of the device and methods of making and using the same have been discussed and illustrated herein, it is to be distinctly understood that the invention is not limited thereto but may be otherwise variously embodied and practiced within the scope of the following claims.