TW200940945A - Apparatus for defeating high energy projectiles - Google Patents
Apparatus for defeating high energy projectiles Download PDFInfo
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- TW200940945A TW200940945A TW098102667A TW98102667A TW200940945A TW 200940945 A TW200940945 A TW 200940945A TW 098102667 A TW098102667 A TW 098102667A TW 98102667 A TW98102667 A TW 98102667A TW 200940945 A TW200940945 A TW 200940945A
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- metal
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- emitter
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
- F41H5/023—Armour plate, or auxiliary armour plate mounted at a distance of the main armour plate, having cavities at its outer impact surface, or holes, for deflecting the projectile
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0442—Layered armour containing metal
- F41H5/045—Layered armour containing metal all the layers being metal layers
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
200940945 六、發明說明： 【發明所屬之技術領域】 本發明係關於一種裝甲構造，其可抵抗經設計以挫敗車 輛裝甲之南能量固體發射體之穿透。 • 本申請案主張2008年1月23曰申請之美國專利申請案 12/010,268的優先權，申請案12/010,268為2〇〇7年3月2日申 請之申請案11/713,012的部分接續案，申請案u/713,〇12為 2006年9月15日申請之申請案11/5213〇7的部分接續案。 ❹ 【先前技術】 習知之裝甲會遭到各種發射體的攻擊，該等發射體經設 計以藉由以固體或射流狀物體穿透裝甲或藉由在裝甲中引 發衝擊波（該等衝擊波以導致裝甲散裂之方式而反射，使 得形成一開口且穿透體（通常插至裝甲之一部分）穿過，或 在裝甲未被實體穿透之情況下裝甲之内層散裂且裝甲碎片 以高速度發射）而挫敗裝甲。 ❹一些反裝甲武器被推進至裝甲之外表面，在該處成形裝 藥***而形成將穿透固體裝甲之大體線性的金屬"射流"； 此等通常稱作空心裝藥（H〇n〇w Charge)(HC)武器。第二類 .型反裝甲武器使用線性、大質量之金屬穿透體，其以高速 度發射以穿透裝甲。此類型之武器被稱為EFP(***形成發 射體）或SFF(自形成碎片）或"餅狀裝藥"或有時稱為"盤狀裝 藥"。 在一些此等武器中’彈頭特性相當於HC與EFP之混合 體’且產生—系列排成一列向目標發射之金屬穿透體。本 137805.doc 200940945 文中將此武器稱為混合彈頭。混合彈頭根據其具有多少，，射 流”或HC效應及其產生至多少單一大穿透體（類似於EFP)而 作用。 各種保護系統可有效抵禦HC射流。不同系統中最著名 的係反應性裝甲’該等裝甲在保護層中使用***物，其在 被擊中時引爆以在HC射流穿透目標前使大多HC射流斷 開。問題為此等***系統在抵禦EFP或混合系統方面表現 不佳。 已提出另一種系統以抵禦此等武器，其中裝甲包含兩 層’ 一電導體安置於該兩層之間。在電導體與裝甲之相鄰 表面之間建立一顯著電位。當射流或狹長固體穿透體穿透 裝曱時，其在裝甲層與電導體之間建立一導電路徑，該電 位經由該路徑而放電。當有足夠電能量經由穿透體放電 時，穿透體被熔融或汽化，且其穿透下一層裝甲的能力顯 著降低。 另類型之反裝曱武器以高速度推進相對較大、大質量 之大體球形固體發射體（或一系列之多個發射體）。當球形 金屬發射體擊中裝曱時，撞擊引發衝擊波，衝擊波之反射 方式使得自周圍材料切下栓塞狀之裝甲部分且其沿金屬發 射體之路徑發射，同時金屬發射體附著至該栓塞狀部分。 此，象可明顯地對裝甲以此方式被挫敗的車輛内之系統及 人員具有很顯著的毀害效應。 雖然HC類型武器的設計特徵及材料要求其由具有技術 專長之實體製造’但是後—類型之武器（咖及混合型）可 137805.doc 200940945 由容易在戰鬥區域中獲得之材料建構。出於彼原因及此等 武器十分有效之事實，已證明其對使用習知裝甲之車輛而 言係很難對付的。 三個所提及類型之彈頭<穿透效能冑常被#料穿透一 , 定量之實心RHA(軋製均質裝曱）鋼裝甲的能力《該等武器 • 類型之典型效能為：HC彈頭可穿透1至3 ft厚度之RHA， EFP彈頭可穿透丨至6英吋之RHA ’且混合彈頭可穿透2至12 英吋厚之RHA。此等估計係基於重量小於15磅並以其最佳 ® 各別之最優間距距離發射之彈頭。在第一英吋的RHA中穿 出之孔之直徑為.HC為高至一英吋直徑的孔，EFp為高至 9英吋直徑的孔，且混合型的孔直徑在上述兩者之間。不 同裝藥之最佳各別最優間距距離為：11(：裝藥的間距距離 在3英尺以下為良好的但在1〇行或1〇 以上很差；對於EFp 裝藥，高至30英尺的間距距離產生幾乎相同（良好）之穿透 且穿透性將僅在諸如50碼之很大距離處顯著降低；且對於 φ 屍合型裝藥，穿透在高至1〇 ft的間距距離處係良好的但在 增加至20英尺之後穿透性開始顯著降低。使用此等裝藥之 方式由此等間距距離及其有效性得以最優化之方式而判定 • (例如，穿透體彈道與裝甲之角度）。此等因素引起本發明 .保護裝甲之設計。 本發明可有效對抗混合型裝藥，因為必須將混合型裝藥 靠近道路邊緣置放以提供深穿透且因此其必須向上傾斜以 擊中所要目標部分。因此，其並不與裝曱表面成直角地擊 中裝甲β射流因此至少部分自其彈道偏離，且其穿透性降 137805.doc 200940945 低。有效的EFP可自相對較長之間距距離發射且很有機會 命中並具有良好穿透性，但本發明對於對抗EFp很有效。 混合型及EFP係本發明主要意欲應付之威脅。 雖然任何反裝曱發射體可由足夠強度及厚度之裝曱抵 ’ 禦，但是額外之裝甲厚度係沉重且昂貴的，使用其將增加 • 任何裝甲車輛的重量，此又會對車輛引擎及傳動系造成更 大壓力。 當與阻擋特定武器穿透所需之RHA相比較時，可依據提 供重量優勢的對抗此等類型武器之裝曱解決方案節省之 RHA重量而量測該等裝曱解決方案。可將此優勢計算作為 一保護比率，該比率等於阻擋武器穿透所需之RHA重量除 乂所&議裝曱系統的將停止相同武器之重量。按照存在於 武器之預期彈道方向上的每單位前方面積而計算此等重 量。 因此，存在對一種裝甲之需要，該裝甲可在無需過多厚 φ 度之裝曱的情況下抵禦來自反裝甲設備之發射體。較佳 地此裝甲由可以合理成本容易地製造且併入車輛設計 中，且更佳地可被添加至現有車輛的材料製成。 ' 隨著對裝甲車輛之威脅增加且變得更多樣化，需要裝曱 . 或裝甲系統之組合來抵禦各種威脅。本發明是保護車輛抵 抗軍用冑擊步搶子彈、炸彈破片及地雷***所需之普通設 。十特徵之外的。本文描述了一種裝曱系統，該系統提昇了 裝甲車輛之防護等級，使其可抵禦EFp及混合型裝藥。 【發明内容】 、 137805.doc 200940945 本發明之額外目標及優勢將部分陳述於隨後之描述中， 且部分將自描述顯而易見，或可藉由實踐本發明而獲知。 將藉由在所附申請專利範圍中特定地指出之要素及組合實 現並獲得本發明之目標及優勢中的一或多者。 為達成目標中之一或多者及根據本發明之目的，如本文 所體現及廣泛描述’本發明包含用於抵禦固體發射體之裝 甲系統。該系統之一實施例包括至少一裴曱板，該裝曱板 經定位以首先遭遇發射體且在一上游表面（相對於發射體 彈道）上具有經安置以與組成金屬發射體之金屬摩擦熔接 或結合的組合物之金屬塗層。 本發明之另一實施例為一用於抵禦固體發射體之裝甲系 統’該系統具有複數個沿發射體彈道定位且沿彈道彼此間 隔開的金屬裝甲板’經定位以首先遭遇發射體之金屬裝甲 板在其上游表面（相對於彈道）上具有經安置以與組成金屬 發射體之金屬摩擦熔接或結合的組合物之金屬塗層，且其 他金屬裝曱板中之至少一者在其上游表面上具有經安置以 與組成相鄰之上游金屬裝甲板之金屬摩擦熔接或結合的組 合物之金屬塗層。 系統之另一實施例包括：一外金屬裝甲板，其位於發射 體彈道中；一内部金屬裝曱板，其大致平行於第一金屬裝 甲板而定位且沿彈道自第一金屬裝曱板向下游位移一距離 以形成第一分散空間；及第一金屬層，其位於外金屬裝甲 板與内部金屬裝曱板之間，該第一金屬層為相對於外金屬 裝甲板及内部金屬裝甲板之厚度較薄的，且第一金屬為經 137805.doc 200940945 安置以與外裝甲板金屬及内部裝甲板金屬中之至少一者摩 擦熔接或結合的組合物。該系統可進一步包括：一内金屬 裝曱板，其大致平行於内部金屬裝曱板而定位且沿彈道自 内部金屬裝曱板向下游位移以形成第二分散空間；及第二 , 金屬層，其位於内部金屬裝甲板與内金屬裝甲板之間，該 • 第一金屬層為相對於内部金屬裝甲板及内金屬裝曱板之厚 度較薄的，且第二金屬為經安置以與内部裝甲板金屬及内 裝曱板金屬中之至少一者摩擦熔接或結合的組合物。 ® 本發明之特定實施例係用於抵禦固體銅發射體之裝甲系 統，該裝甲系統具有-外裝甲板，該外裝甲板經定位以首 先遭遇銅發射體且包含具有大於20,000磅/平方英忖之極限 拉伸強度及8至40毫米之範圍内之厚度的鋁合金。亦存在 内4裝曱板’其包含具有大於2G，GGG^t/平方英忖之極限 拉伸強度及8至40毫米之範圍内之厚度的鋁合金。該内部 裝甲板大致平行於外裝曱板而安置，並（相對於發射體彈 φ 道）自外裝甲板向下游位移25至150毫米之距離以在外裝甲 板與内部裝甲板之間形成第-分散空間。該系統進一步包 括内裝甲板，其包含具有大於20，_磅/平方英吋之拉伸強 . 度、大於10%之斷裂伸長率及8至40毫米之範圍内之厚度 ㈣合金。該内㈣f板大致平行於内部裝甲板而安置^ 且自内部裝甲板向下游位移25至15〇毫米之距離以在内部 裝甲板與内铭裝甲板之間形成第二分散空間。外金屬裝甲 板在其上游表面（相對於彈道）上具有—金屬塗層，其經安 置以與鋼摩擦熔接或結合，部金屬裝甲板及内金屬裝甲 137805.doc 200940945 板在其各別上游表面上具有經安置以與銘摩擦溶接或結合 之金屬層或塗層。 該系統亦可包括鋼裝甲板，其具有大於35〇之勃氏 (BHneU)硬度及4至20毫米之範圍内之厚度。鋼裝甲板自内 . 鋁内部裝曱板向下游位移（相對於彈道）以形成5至3〇毫求之 第二分散空間。此實施例可較佳地用以改良 •，中車輛之車身包括固定至其内部表面之一層片 裝甲，例如硬質聚合物/纖維複合物及/或一層抗穿透織 β 物。 應瞭解以上概述及以下[實施方式]僅為例示性及說明性 的’且並非限制如所主張之本發明。 被併入且構成此說明書之一部分的隨附圖式說明本發明 之若干實施例，且連同描述用於解釋本發明之原理。 【實施方式】 現將對本發明之現有較佳實施例進行詳細參考，其實例 ⑩ 說明於隨附圖式中。在任何可能之處，將在諸圖式中使用 相同參考數字來指代相同或相似部分。 根據本發明，提供用於抵禦固體發射體之裝甲系統。雖 . 然本發明及其實施例可阻礙由成形裝藥產生之狹長金屬 射流”之穿透，但其主要效用係抵禦由製造成之***設備 或臨時拼凑之***設備形成並推進之相對之非狹長大質量 之固體金屬發射體。本發明之實施例可包括用於應付除了 非狹長固體金屬發射體外的金屬射流及/或狹長大質量之 金屬穿透體的系統。若已知特定發射體之重量、密度、速 137805.doc 200940945 度及大小’則可選擇系統參數以抵禦該特定發射體。系統 參數為包含本發明之層之材料層的機械特性（極限拉伸強 度、硬度、彈性模數、破裂韌性及受迫衝擊速度）、該等 層之間隔（層之間的距離，亦即，分散空間之厚度）以及置 . 放在該等層之間的空間中之任何材料之性質。 根據本發明之一態樣’提供一經定位以沿發射體彈道首 先遭遇發射體之外板。該板可具有平行、相對之平坦表 面。在其上游表面（相對於發射體彈道）上，外板可包括經 ® 安置以與組成金屬發射體之金屬摩擦熔接或結合之組合物 的金屬塗層。如本文中所體現，及如圖1中所示，裝甲系 、·先1〇ι括外裝甲板12，其在板12之相對於發射體彈道34 之上游表面上具有一金屬塗層22。如進一步將揭示，本發 明之目標為選擇用於金屬塗層22之材料以引發發射體摩擦 熔接或結合至若干裝曱層中之第一層，且使該層之一部分 斷裂。以此方式，發射體被擴大，並由於附著之裝甲部分 〇 而變侍更重，且被減慢，以至於發射體與自該等層破裂並 溶接或結合至發射體的裝甲之組合更易於由裝甲或板狀材 料之-或多個連續層停止，如本文關於本發明之另一 • 所論述。 •㈣語"金屬"而言，中請者意謂包括基本金屬、基本金 屬之合金及其非合金混合物。 就術5吾"摩擦溶接或結合"而言，申請者意謂一金屬結構 由於發射體（或發射體加上—或多個金屬裝甲板之部分 下游結構所賦予之能量而黏附或附著至另一金屬結構，而 137805.doc -11 - 200940945 不依靠特定黏附或附著機構。因此，若術語”熔接"或"結 合•'具有一較窄技術定義，則如由申請中之申請專利範圍 所界定的本發明不意欲受到此等術語之限制。 撞擊固體之發射體引發固體中之衝擊波。穿過該系統之 衝擊波提供了在該板之内表面處喷發之能量，但該喷發之 方向係藉由其中具有衝擊波能量之材料之内表面的形狀及 衝擊能量將被傳輸至内表面附近之材料決定。當自該固體BACKGROUND OF THE INVENTION 1. Field of the Invention This invention relates to an armor construction that resists penetration of a south energy solid emitter designed to defeat vehicle armor. • This application claims the priority of U.S. Patent Application Serial No. 12/010,268, filed on Jan. 23, 2008, and the application Serial No. 12/010,268 is part of the continuation of the application 11/713,012 filed on March 2, 2007. , application u/713, 〇12 is part of the continuation of the application for application 11/5213〇7 on September 15, 2006. ❹ [Prior Art] Conventional armor is attacked by various emitters designed to penetrate armor with solid or jet objects or to induce shock waves in armor (the shock waves cause armor) Reflected in a manner of spalling, such that an opening is formed and the penetrating body (usually inserted into one part of the armor) passes through, or the inner layer of the armor is spalled without armor penetration and the armor debris is fired at high speed) And defeated armor. ❹ Some anti-armor weapons are pushed to the outer surface of the armor where the shaped charge explodes to form a generally linear metal that will penetrate the solid armor "jet"; these are commonly referred to as hollow charges (H〇n 〇w Charge)(HC) weapon. The second type of anti-armor weapon uses a linear, massive metal penetrating body that is fired at high speed to penetrate the armor. This type of weapon is known as EFP (Explosive-Formed Emitter) or SFF (Self-Formed Debris) or "Cup-like Charge" or sometimes "Disc-type Charge". In some of these weapons, the 'warhead characteristics correspond to a mixture of HC and EFP' and produce - a series of metal penetrating bodies that are emitted toward the target. This 137805.doc 200940945 article refers to this weapon as a hybrid warhead. The hybrid warhead acts according to how much it has, the jet "or HC effect and how many single large penetrating bodies (similar to EFP) are produced. Various protection systems are effective against HC jets. The most famous reactive armor in different systems 'The armor uses explosives in the protective layer that detonate when hit to break most of the HC jets before the HC jet penetrates the target. The problem is that such explosive systems do not perform well against EFP or hybrid systems. Another system has been proposed to protect against such weapons, in which the armor consists of two layers of 'an electrical conductor placed between the two layers. A significant potential is established between the electrical conductor and the adjacent surface of the armor. When the jet or narrow solid When the penetrating body penetrates the device, it establishes a conductive path between the armor layer and the electrical conductor, and the potential is discharged through the path. When sufficient electrical energy is discharged through the penetrating body, the penetrating body is melted or vaporized. And its ability to penetrate the next layer of armor is significantly reduced. Another type of anti-arming weapon advances relatively large, large mass spherical solid emitters at a high speed (or a series The plurality of emitters. When the spherical metal emitter hits the mounting, the impact induces a shock wave, and the shock wave is reflected in such a manner that the embolic portion of the armor is cut from the surrounding material and is emitted along the path of the metal emitter while the metal is emitted. The body is attached to the plug-like portion. This, as can obviously have a significant destructive effect on the systems and personnel in the vehicle in which the armor is defeated in this way. Although the design features and materials of the HC-type weapon require technical The entity of expertise produces 'but the type of weapon (cafe and hybrid) can be 137805.doc 200940945 constructed from materials that are easily obtained in the battle zone. For reasons of which and the fact that such weapons are very effective, it has been proved It is difficult to deal with the use of conventional armored vehicles. The three types of warheads mentioned above are often penetrated by a material, quantitative solid RHA (rolled homogeneously mounted) steel armor. Capabilities "The typical performance of these weapons types is: HC warheads can penetrate RHAs of 1 to 3 ft thickness, EFP warheads can penetrate to 6 feet of RHA' and hybrid warheads can Through 2 to 12 inches of RHA. These estimates are based on warheads that weigh less than 15 pounds and are fired at their optimum optimal distances. The diameter of the hole through the first inch of RHA. The .HC is a hole of up to one inch in diameter, the EFp is a hole of up to 9 inches in diameter, and the diameter of the hybrid type is between the above two. The optimal optimal spacing distance for different charges is :11(: The distance between the charges of the charge is below 3 feet, but it is poor at 1 line or more; for EFp charges, the distance of up to 30 feet produces almost the same (good) penetration and Penetration will only be significantly reduced at large distances such as 50 yards; and for φ corpse-type charges, penetration is good at pitch distances up to 1 ft but penetrates after increasing to 20 feet Sex begins to decrease significantly. The way in which these charges are used is determined by the way the equidistant distances and their effectiveness are optimized • (eg, penetrating the ballistic trajectory and armor angle). These factors cause the invention to protect the design of the armor. The present invention is effective against mixed charge because the mixed charge must be placed close to the edge of the road to provide deep penetration and therefore must be tilted upward to hit the desired target portion. Therefore, it does not hit the armored beta jet at right angles to the mounting surface and thus at least partially deviates from its ballistics, and its penetration is reduced by 137805.doc 200940945. Effective EFPs can be launched from relatively long distances and have a good chance of hitting and having good penetration, but the present invention is very effective against EFp. Hybrid and EFP are the threats to which the present invention is primarily intended to cope. Although any counter-mounting emitter can be supported by a sufficient strength and thickness, the additional armor thickness is heavy and expensive, and its use will increase • the weight of any armored vehicle, which in turn will affect the vehicle's engine and drive train. Cause more pressure. When compared to the RHA required to block the penetration of a particular weapon, the mounting solutions can be measured in terms of the weight of the RHA saved against the mounting of these types of weapons. This advantage can be calculated as a protection ratio equal to the weight of the RHA required to block the penetration of the weapon, and the weight of the same weapon will be stopped. These weights are calculated as the area per unit front that exists in the expected ballistic direction of the weapon. Therefore, there is a need for an armor that can withstand an emitter from a counter armor device without requiring too much thickness. Preferably, the armor is made of a material that can be easily manufactured at a reasonable cost and incorporated into the design of the vehicle, and more preferably can be added to existing vehicles. As the threat to armored vehicles increases and becomes more diverse, a combination of armored systems or armored systems is needed to withstand various threats. SUMMARY OF THE INVENTION The present invention is a conventional design for protecting a vehicle against military sniping rifles, bomb fragments, and mine explosions. Beyond the ten features. This article describes a mounting system that increases the degree of protection of armored vehicles against EFp and hybrid charges. BRIEF DESCRIPTION OF THE DRAWINGS [0009] The additional objects and advantages of the present invention will be set forth in part in the description which follows. One or more of the objects and advantages of the present invention will be realized and obtained by the elements and combinations particularly pointed out in the appended claims. In order to achieve one or more of the objectives and in accordance with the purpose of the present invention, as embodied and broadly described herein, the present invention includes an armor system for resisting solid emitters. An embodiment of the system includes at least one raft plate positioned to first encounter an emitter and having an upstream surface (relative to the emitter trajectory) disposed to frictionally weld with a metal constituting the metal emitter Or a metal coating of the combined composition. Another embodiment of the present invention is an armor system for resisting solid emitters. The system has a plurality of metal armor plates positioned along the trajectory of the emitter and spaced apart from each other along the ballistics. The metal armor is positioned to first encounter the emitter. The plate has a metal coating on its upstream surface (relative to the ballistic) that is disposed to frictionally fuse or bond with the metal constituting the metal emitter, and at least one of the other metal slabs is on its upstream surface A metal coating having a composition disposed to frictionally weld or bond with a metal constituting an adjacent upstream metal armor. Another embodiment of the system includes: an outer metal armor plate positioned in the projectile trajectory; an inner metal mounting plate positioned substantially parallel to the first metal armor panel and extending along the ballistic path from the first metal mounting plate Downwardly displaced a distance to form a first dispersion space; and a first metal layer between the outer metal armor plate and the inner metal mounting plate, the first metal layer being opposite to the outer metal armor plate and the inner metal armor plate The thinner, and first metal is a composition disposed by 137805.doc 200940945 to frictionally weld or bond with at least one of the outer deck metal and the inner armor metal. The system may further include: an inner metal mounting plate positioned substantially parallel to the inner metal mounting plate and displaced downstream from the inner metal mounting plate along the ballistics to form a second dispersion space; and a second, metal layer, It is located between the inner metal armor plate and the inner metal armor plate, the first metal layer is relatively thin relative to the inner metal armor plate and the inner metal mounting plate, and the second metal is placed to be placed with the inner armor A composition that frictionally welds or bonds at least one of the sheet metal and the interior raft metal. ® A particular embodiment of the present invention is an armor system for resisting a solid copper emitter having an outer jacket that is positioned to first encounter a copper emitter and that includes greater than 20,000 pounds per square inch. Aluminum alloy having an ultimate tensile strength and a thickness in the range of 8 to 40 mm. There is also an inner 4 mounting plate which comprises an aluminum alloy having an ultimate tensile strength greater than 2 G, GGG^t/square inch and a thickness in the range of 8 to 40 mm. The inner armor plate is placed substantially parallel to the outer fascia and is displaced (relative to the projectile φ tract) from the outer deck to a downstream distance of 25 to 150 mm to form the first between the outer armor and the inner armor plate - Disperse space. The system further includes a interior deck comprising a tensile strength greater than 20, lbs. per square inch, an elongation at break greater than 10%, and a thickness in the range of 8 to 40 millimeters. The inner (four)f-plate is disposed substantially parallel to the inner armor panel and is displaced downstream from the inner armor deck by a distance of 25 to 15 mm to form a second dispersing space between the inner armor panel and the inner deck. The outer metal armor plate has a metal coating on its upstream surface (relative to the ballistics) that is placed to frictionally weld or bond with the steel, and the metal armor plate and inner metal armor 137805.doc 200940945 plates are on their respective upstream surfaces. There is a metal layer or coating disposed to fuse or bond with the rubbing. The system may also include a steel armor panel having a BHneU hardness of greater than 35 inches and a thickness in the range of 4 to 20 millimeters. Steel armored from the inside. The aluminum inner mounting plate is displaced downstream (relative to the ballistics) to form a second dispersion space of 5 to 3 inches. This embodiment is preferably used to improve the body of a vehicle including a layer of armor secured to its interior surface, such as a rigid polymer/fiber composite and/or a layer of anti-penetration. The above summary, as well as the following <RTIgt; </ RTI> <RTIgt; </ RTI> <RTIgt; </ RTI> <RTIgt; The accompanying drawings, which are incorporated in FIG [Embodiment] A preferred embodiment of the present invention will now be referred to in detail, and an example 10 thereof will be described with reference to the accompanying drawings. Wherever possible, the same reference numerals are used in the FIGS According to the present invention, an armor system for resisting solid emitters is provided. Although the invention and its embodiments can impede the penetration of elongated metal jets produced by shaped charges, the primary utility is to counteract the relative non-formation created and propelled by explosive devices or temporarily assembled explosive devices. Narrow and massive solid metal emitters. Embodiments of the invention may include systems for coping with metal jets other than non-slit solid metal emitters and/or elongated masses of metal penetrating bodies. Weight, Density, Speed 137805.doc 200940945 degrees and size 'The system parameters can be selected to withstand this particular emitter. The system parameters are the mechanical properties of the material layer containing the layer of the invention (extension tensile strength, hardness, modulus of elasticity). , fracture toughness and forced impact velocity), the spacing of the layers (the distance between the layers, that is, the thickness of the dispersion space), and the nature of any material placed in the space between the layers. One aspect of the present invention provides a plate that is positioned to first encounter an outer body of the emitter along the trajectory of the emitter. The plate may have parallel, opposite flat surfaces. On its upstream surface (relative to the emitter trajectory), the outer panel may comprise a metal coating disposed by the ® to frictionally fuse or bond the metal constituting the metal emitter. As embodied herein, and as shown in FIG. As shown, the armor system first includes an outer deck 12 having a metal coating 22 on the upstream surface of the panel 12 relative to the emitter ballistic 34. As will be further disclosed, the object of the present invention is The material for the metal coating 22 is selected to cause the emitter to be frictionally welded or bonded to the first layer of the plurality of layers and to partially break the layer. In this manner, the emitter is enlarged and due to the attached armor Part of the enthalpy becomes heavier and slower, so that the combination of the emitter and the armor that ruptures from the layers and fuses or bonds to the emitter is more likely to stop by the armor or plate material - or multiple successive layers As discussed herein with respect to another aspect of the present invention. • (4) The term “metal” refers to the inclusion of basic metals, alloys of base metals and their non-alloy mixtures. Molten or knot In the case of ", the applicant means that a metal structure adheres or adheres to another metal structure due to the energy imparted by the emitter (or the emitter plus or part of the downstream structure of the metal armor plate), and 137805. Doc -11 - 200940945 does not rely on a specific adhesion or attachment mechanism. Therefore, if the term "welding" or "combination" has a narrower technical definition, the invention as defined by the scope of the patent application in the application is not intended. Subject to these terms. The impactor that strikes the solid initiates a shock wave in the solid. The shock wave passing through the system provides the energy ejected at the inner surface of the plate, but the direction of the eruption is due to the shock wave therein. The shape of the inner surface of the energy material and the impact energy will be determined by the material being transported to the vicinity of the inner surface. When from the solid
接收衝擊能量之材料具有顯著較低之受迫衝擊波傳輸速度 時，該能量將在表面處被反射且不被傳輸。舉例而言，在 其中具有衝擊波之材料為固體（例如以5〇〇〇米/秒傳導衝擊 波之鋁或鋼）且接收衝擊波之材料為空氣（僅具有33〇米/秒 之爻追衝擊波傳輸速度）之情況下，該不匹配將導致能量 在相關之板表面處聚積並接著導致一喷發。此喷發之一種 形式已知為散裂。 形成板之固體材料之材料特性會影響能量耗散及動量偏 離穿透線之傳輸’且藉此影響散裂發生在金屬板之後部的 方式。若材料為脆性的（類似於大多數陶变），則前面處之 硬度優勢在發生散裂之後面處失去，因為該材料具有很低 t斷裂伸長率且該材料碎成小片，將較少之能量帶離穿透 當材料展現1()%或更A之斷裂伸長率值時，可在諸如 鋼：：它金屬之材料中產生較大之單—裂片。具有耗合至 =伸長率值之高拉伸強度（諸如對於銘高於 英吋）之材料要求較大量之能詈以外τ 嘮十方 動量#栢—法 旎里以扯下一塊大裂片。藉由 、疋，相對於撞擊發射體質量的大質量裂片將導 137805.doc •12- 200940945 致退出板之後部且穿過分散空間而被帶至下一保護板上的 組份速度的較大降低。 根據本發明之另一或第二態樣，系統包括沿發射體彈道 定位之一或多個連續裝曱板’該等連續裝曱板大致平行於 外裝甲板而定向且彼此相對位移以在相鄰之裝曱板之間形 成分散空間。 如此處體現’及在圖1中示意性描繪，系統丨〇包括一系 列大體平行之板’包含外金屬裝甲板12、内部金屬裝曱板 14及内金屬裝甲板15。如本文中所使用，"裝曱板I，為板狀 部件’其經安置以使發射體破碎、偏轉或分散或吸收來自 發射體之能量以促進由系統之其他部分來抵禦該發射體。 其可為一已知之金屬裝甲板材料（亦即，高強度之金屬板） 或比習知裝甲板強度較低之習知金屬板，其可在本發明中 用以影響發射體使得裝曱系統中之其它元件抵禦發射體。 内裝曱板15可包含裝甲車輛之車身的裝曱板16(參見圖9)， 或可為一第二較低密度裝曱板’其後為車輛車身之裝曱板 16(參見圖4)。下文將進一步詳細論述該後一實施例。 如此處所體現及圖1中所描繪，系統1〇亦包括一將板12 及14分開一距離19之第一分散空間18，及一將板14及15分 開的第二分散空間20。板14及15在其各別上游表面上具有 金屬塗層22及24以提供與來自直接相鄰之上游板（圖1實施 例中分別為12及14)之碎片的摩擦熔接或結合。分散空間 為在相鄰之板之間或在大體上垂直於該等板之方向上量測 的空間，且分散空間的功能為允許穿過其的材料側向分 137805.doc •13- 200940945 散。術語”側向"意謂在與發射體初始飛行路線（亦即發射體 之彈道）成一角度的方向上。移動材料被分散地越多入 射到下一連續層上之能量就越不集中。此外，層間的距離 越大（分散空間之厚度越大），在每表面面積的下游金屬裝 甲板上由移動材料賦予的動能將越少。明顯地，若分散距 . 離很大，則大量動能將自原始穿透線散開並失去，但所得 刀層、、.σ構將不實際地厚。另一方面，若分散空間之厚度太 小，則移動材料不被分散，其動能及動量不耗散，且其可 具有足夠之忐量及集中度以挫敗系統之隨後裝甲層。熟習 本發明所屬技藝之技術者，藉由本文提供之一般指導，結 &下文之實例，可設計系統以抵禦以特定速度沿特定彈道 行進之特定發射體或發射體之混合。 如下文將更詳細揭示’該系統包含複數個分層板，其中 相鄰之板由所謂的分散空間所分離 '组成該系統之板中之 至 > 一者（在其與下游相鄰之板（相對於發射體彈道）之間） 藝 /、有金屬層，該金屬層經安置以摩擦熔接或結合至當發 射體撞擊該板時脫離的上游板之碎片之金屬。雖然當前將 摩擦溶接/結σ金屬層組態為下游板之上游表面上的一塗 層係較佳@ <旦疋熟習此項技術者將瞭解該塗層可施加至 上游板之下游表面或作為分散空間中之獨立薄片或膜。 又可在給疋分散空間中提供兩個或兩個以上塗層或獨立 薄片。 藉由本揭不案’熟習此項技術者能夠對圖1之塗層Μ、 24及26選擇適自金屬及尺寸以提供與特定應用中之金屬板 137805.doc •14, 200940945 Γ之=炼接或結合1此而論，來自***結合技 :之和導可為有用的，諸如，sz 4’842，182及其中所引用的參考文獻。 專利 ❹When the material receiving the impact energy has a significantly lower forced shock wave transmission velocity, the energy will be reflected at the surface and not transmitted. For example, a material having a shock wave therein is a solid (for example, aluminum or steel that conducts a shock wave at 5 〇〇〇 m / sec) and the material receiving the shock wave is air (only having a 〇 shock wave transmission speed of 33 〇 / sec) In the event of this mismatch, energy will accumulate at the surface of the associated plate and then cause an eruption. One form of this eruption is known as spalling. The material properties of the solid material forming the panel affect the energy dissipation and the transmission of momentum away from the transmission line' and thereby affect the manner in which spalling occurs at the rear of the metal sheet. If the material is brittle (similar to most pottery), the hardness advantage in the front is lost after the spalling, because the material has a very low elongation at break and the material breaks into small pieces, which will be less. Energy Band Penetration When the material exhibits an elongation at break value of 1 (%) or A, a larger single-lobed can be produced in a material such as steel::metal. A material with a high tensile strength (such as for a higher than 吋) requires a larger amount of energy than τ 唠 十方 Momentum #柏—法 旎里 to tear off a large lob. By means of, 疋, a large mass split relative to the mass of the impinging emitter will lead to a greater velocity of the component that is brought to the rear of the panel and passed through the dispersion space to the next protective panel. reduce. In accordance with another or second aspect of the present invention, the system includes one or more continuous mounting panels along the trajectory of the emitter. The continuous mounting panels are oriented generally parallel to the outer deck and are displaced relative to each other to A dispersing space is formed between the adjacent mounting plates. As embodied herein and schematically depicted in FIG. 1, the system includes a series of generally parallel plates comprising an outer metal armor plate 12, an inner metal mounting plate 14 and an inner metal armor plate 15. As used herein, "flap plate" is a plate member' that is positioned to cause the emitter to break, deflect or disperse or absorb energy from the emitter to facilitate protection of the emitter by other portions of the system. It can be a known metal armor plate material (ie, a high-strength metal plate) or a conventional metal plate having a lower strength than the conventional armor plate, which can be used in the present invention to influence the emitter to make the mounting system The other components in the body resist the emitter. The inner fascia 15 may comprise a sill 16 of the body of the armored vehicle (see Figure 9), or may be a second lower density sill board followed by a sill 16 of the vehicle body (see Figure 4). . This latter embodiment will be discussed in further detail below. As embodied herein and depicted in FIG. 1, system 1A also includes a first dispersion space 18 that separates panels 12 and 14 by a distance 19, and a second dispersion space 20 that separates panels 14 and 15. Plates 14 and 15 have metal coatings 22 and 24 on their respective upstream surfaces to provide friction welding or bonding with fragments from directly adjacent upstream plates (12 and 14 in the Figure 1 embodiment, respectively). The dispersing space is a space measured between adjacent plates or in a direction substantially perpendicular to the plates, and the function of the dispersing space is to allow the material to pass through the lateral 137805.doc •13- 200940945 . The term "lateral" means that in the direction of the initial flight path of the emitter (i.e., the trajectory of the emitter), the more the dispersed material is dispersed, the less concentrated the energy is incident on the next successive layer. In addition, the greater the distance between the layers (the greater the thickness of the dispersion space), the less kinetic energy imparted by the moving material on the metal armor plate on the downstream of each surface area. Obviously, if the dispersion distance is large, a large amount of kinetic energy The original penetrating line is scattered and lost, but the obtained scalpel layer, .σ structure will not be practically thick. On the other hand, if the thickness of the dispersing space is too small, the moving material is not dispersed, and its kinetic energy and momentum are not consumed. Dispersing, and it may have sufficient volume and concentration to defeat the subsequent armor layer of the system. Those skilled in the art to which the present invention pertains can design the system to defend against the general guidance provided herein, and the examples below. A particular emitter or combination of emitters that travel along a particular trajectory at a particular speed. As will be disclosed in more detail below, 'the system includes a plurality of layered panels, where adjacent panels are made of so-called The space is separated 'in the plate that makes up the system> (one between its adjacent plate (relative to the projectile ballistics)) has a metal layer that is placed for friction welding Or a metal that is bonded to the debris of the upstream plate that is detached when the emitter strikes the plate. Although it is currently preferred to configure the frictional fusion/junction metal layer as a coating on the upstream surface of the downstream plate@@lt; Those skilled in the art will appreciate that the coating can be applied to the downstream surface of the upstream panel or as a separate sheet or film in the dispersion space. It is also possible to provide two or more coatings or individual sheets in the given dispersion space. By this disclosure, those skilled in the art will be able to select the appropriate metal and size for the coatings, 24 and 26 of Figure 1 to provide metal plates for specific applications. 137805.doc •14, 200940945 === Or in conjunction with this, it may be useful to derive from the combination of explosions, such as sz 4'842, 182 and the references cited therein.
=然此等參考文獻主要針對藉由使用***在金屬板之間 一t可靠結合所必需之關係，但其的確提供關於在金屬以 何金屬傾向於結合至其他金屬的指導。若撞 、’、’其為發射體或為相鄰之裝曱層碎片)之表面預 期為銅，則裝甲系統之上游表面較佳為自由以下各物組成 之群中所選出之金屬：銅、鐵、銘、欽。若撞擊物件（益 ，其為發射體或為相鄰之裝甲層碎片)之表面預期為鋼， 則裝甲系統之上游表面較佳為自由以下各物組成之群中選 出之金屬：鐵、鎂、钥、銅、錯、欽、錄及銘。若撞擊物 件（無論其為發射體或為相鄰之裝甲層）之表面預期為銘， J裝甲系統之上游表面較佳為自由以下各物組成之群中選 出之金屬…鋁、鐵、鈦及銅。若撞擊物件(無論其為發射 體或為相鄰之裝曱層碎片）預期為欽，則裝曱系統之上游 表面較佳為自由以下各物組成之群中選出之金屬：鈦、 鐵、鎳及鋁。 已觀察到，由於摩擦熔接/結合現象，上游板之一或多 個碎片變得附著至發射體金屬且與發射體一起大體沿發射 體彈道行進，但因為以下原因，以相對於發射體速度而言 減少之速度行進。 根據動量守恆，速度乘以發射體之質量將小於或等於速 度乘β發射體與自該板破裂且繼續與發射體一起移動之任 137805.doc -15- 200940945 何板°卩分的質量之和。以公式陳述：MP.V0Mp+f· Vp+f，其 中MP為發射體之質量，％為發射體之速度，Μ"為發射體 加上已摩擦炫接或結合至發射體且自板之剩餘部分破裂的 板。卩分之質量，且Vp+f為發射體加上已熔接至發射體且自 板之剩餘部分破裂的板部分之組合質量的速度，其中 >符 號才曰示由減少之退出速度Vp+f所表明的在板之破裂變形中 的能量耗散》 在本發明之較佳實施例中，外金屬裝曱層為相對堅韌之 可延展材料。其可具有相對薄的金屬塗層以促進與發射體 及/或在其上游表面上之硬質非金屬材料層（例如，陶瓷材 料層）之熔接/結合以引發發射體之破裂及/或變形，但在每 一狀況下，外裝曱層之功能為吸收發射體之一些能量，以 使其平坦（使其質量之至少一些側向位移），及/或顯著降低 其速度。 如圖2 A中所描缯· ’遇到高強度但低韌性之板（例如，具 有小於5%之拉伸斷裂變形之金屬）的相對大質量之發射體 3〇在其表面上變形，且發射體之撞擊的衝擊自板12切下一 板部分12, ’且變形之發射體30與板部分i2,的組合穿過板 12。因為在圖2A實例中，板12為硬且堅固的，所以不存在 板之顯著變形’或能量之吸收或發射體速度之降低。或 者，若發射體具有足夠大之速度使得該板中衝擊波之速度 不能先於穿透的發射體’則裝曱板之金屬橫向位移至該裝 甲板自身中。在此狀況下，穿透的發射體未在其前方裝甲 板上扯下足夠的裝曱板以實現該發射體之動量損失，藉此 137805.doc 200940945 降低了對彼穿透的最大減速量。徑向位移機制為HC射流 用以穿透裝甲之方法。此允許HC裝藥比EFp挫敗更大厚度 之裝甲。 然而，如圖2B中所描繪，遇到較低強度但較高韌性之板 (例如，具有大於7%，且較佳大於1〇%之拉伸斷裂變形之 金屬）之相對大質量的發射體30在其表面上變形，且板12 相應變形，從而吸收能量。在使板變形後，發射體自板12 切下一板部分12"，且變形之發射體3〇與板部分12”的組合 穿過板12並與板12分開。然而，存在板之顯著變形、由切 下大面積的板22引起的能量吸收，且因為板部分12"與變 形的發射體30之組合質量，所以存在該組合之速度的顯著 降低。 裝甲板中之衝擊波之速度應顯著快於穿透體之速度。裝 曱板之韌性接著可被充分利用且撕裂線可（藉由反射及諧 振現象）給出圖2B中描繪為角&之有利的撕裂線。角a愈 大，在被穿透之板變形時吸收的能量愈多，且變形之發射 體與黏附至其的裝甲部分的組合重量愈大。 鋼及銘合金中之受迫衝擊波之速度為約5，〇〇〇米/秒，所 以若撞擊之發射體具有接近或高於彼者之速度，則穿透表 現得較類似於HC。HC之穿透視其穿透之材料之密度而 定，且較低密度材料表現較好。當對付高速度發射體時， 鋁裝甲比鋼裝曱較佳，但當速度已由先前穿透降低時，則 堅韌的鋼板亦變得有效。EFP通常具有2,5〇〇米/秒或更慢 之速度’且混合型具有更小及更輕之以3〇〇〇至35〇〇米/秒 137805.doc 17 200940945 移動之前導穿透體，所以其較難以阻止。對於EFP，板12 所吸收之能量與板之變形及圖2B中所描繪之角度a成正比 例。= However, these references are primarily concerned with the relationship necessary to reliably bond a metal plate by using an explosion, but it does provide guidance as to what metal tends to bind to other metals in the metal. If the surface of the impact, ',' is the emitter or the adjacent layer of the layer is expected to be copper, then the upstream surface of the armor system is preferably free from the metal selected from the group consisting of: copper, Iron, Ming, Qin. If the surface of the impact object (which is an emitter or an adjacent layer of armor layer) is expected to be steel, the upstream surface of the armor system is preferably a metal selected from the group consisting of: iron, magnesium, Key, copper, wrong, Qin, recorded and Ming. If the surface of the impact object (whether it is an emitter or an adjacent armor layer) is expected to be the surface, the upstream surface of the J armor system is preferably free from the metals selected from the group consisting of aluminum, iron, titanium and copper. If the impacting object (whether it is an emitter or an adjacent layer of the enamel layer) is expected to be chin, the upstream surface of the mounting system is preferably a metal selected from the group consisting of titanium, iron, nickel. And aluminum. It has been observed that due to the friction welding/bonding phenomenon, one or more of the upstream plates become attached to the emitter metal and generally travel along the emitter ballistics with the emitter, but for the following reasons, relative to the emitter speed Words reduce the speed of travel. According to the conservation of momentum, the speed multiplied by the mass of the emitter will be less than or equal to the mass of the beta emitter and the mass of the rupture from the plate and continue to move with the emitter. 137805.doc -15- 200940945 . Stated by the formula: MP.V0Mp+f·Vp+f, where MP is the mass of the emitter, % is the velocity of the emitter, and Μ" is added to the emitter plus friction or bonded to the emitter and remaining from the board Partially broken plate. The mass of the component, and Vp+f is the velocity of the combined mass of the emitter plus the plate portion that has been fused to the emitter and ruptured from the remainder of the panel, where the > symbol indicates the exit velocity Vp+f The indicated energy dissipation in the rupture deformation of the panel. In a preferred embodiment of the invention, the outer metal mounting layer is a relatively tough ductile material. It may have a relatively thin metal coating to promote fusion/bonding of the emitter and/or a layer of hard non-metallic material (eg, a layer of ceramic material) on its upstream surface to initiate cracking and/or deformation of the emitter, In each case, however, the function of the outer layer of the outer layer is to absorb some of the energy of the emitter to flatten it (at least some of its lateral displacement) and/or to significantly reduce its velocity. As depicted in Figure 2A, 'a relatively large mass of emitter 3 that encounters a high strength but low toughness plate (e.g., a metal having less than 5% tensile fracture deformation) is deformed on its surface, and The impact of the impact of the emitter strikes the plate portion 12 from the plate 12, and the combination of the deformed emitter 30 and the plate portion i2 passes through the plate 12. Because the panel 12 is hard and strong in the example of Figure 2A, there is no significant deformation of the panel or absorption of energy or reduction in emitter velocity. Alternatively, if the emitter is sufficiently large that the velocity of the shock wave in the panel does not precede the penetrating emitter, then the metal of the panel is laterally displaced into the deck itself. Under this condition, the penetrating emitter does not tear enough of the mounting plate on its front armor plate to achieve momentum loss of the emitter, thereby reducing the maximum amount of deceleration to the penetration. The radial displacement mechanism is the method used by the HC jet to penetrate the armor. This allows the HC charge to frustrate a greater thickness of armor than EFp. However, as depicted in Figure 2B, a relatively large mass of emitter that encounters a lower strength but higher toughness plate (e.g., a metal having a tensile fracture deformation greater than 7%, and preferably greater than 1%) is encountered. 30 is deformed on its surface, and the plate 12 is deformed accordingly to absorb energy. After deforming the plate, the emitter cuts the plate portion 12" from the plate 12, and the combination of the deformed emitter 3〇 and the plate portion 12" passes through the plate 12 and is separated from the plate 12. However, there is significant deformation of the plate. The energy absorption caused by the cutting of the large-area plate 22, and because of the combined mass of the plate portion 12" and the deformed emitter 30, there is a significant reduction in the speed of the combination. The velocity of the shock wave in the armor plate should be significantly faster. At the speed of the penetrating body, the toughness of the mounting plate can then be fully utilized and the tear line can be used (by reflection and resonance phenomena) to give an advantageous tear line depicted in Figure 2B as an angle & Larger, the more energy is absorbed when the plate is penetrated, and the combined weight of the deformed emitter and the armor that adheres to it is greater. The velocity of the forced shock wave in steel and alloy is about 5, 〇 〇〇米/sec, so if the impacting emitter has a velocity close to or higher than the other, the penetration will behave more similarly to HC. The penetration of HC depends on the density of the material it penetrates, and is lower. Density materials perform better when dealing with high speed In the case of body, aluminum armor is better than steel, but when the speed has been reduced by previous penetration, the tough steel plate also becomes effective. EFP usually has a speed of 2,5 mm / sec or slower' and The hybrid type has a smaller and lighter weight of 3〇〇〇 to 35〇〇米/sec. 137805.doc 17 200940945 Moves the lead through the body, so it is more difficult to stop. For EFP, the energy and board absorbed by the board 12 The deformation is proportional to the angle a depicted in Figure 2B.
根據本發明，第一分散空間在大體垂直於板的方向上具 有足夠長度以允許穿過第一分散空間的材料之顯著側向分 散。如此處在包含圖丨中所示之一系列金屬裝曱板之系統 中所體現，分散空間18具有足夠之厚度（如箭頭19所指示） 以允許材料在分散空間18内之顯著側向分散（圖3A-C中示 意性展示之發射體及板12之部分12") ^ 在本發明之此第二態樣中，外板12在其前表面上可具有 5不/、有金屬塗層22以促進在第一發射體30,與外板12 之間的熔接/結合。特定言 <，可在一或多個相鄰之金屬 裝甲板之間提供一或多個金屬層或塗層，諸如分別在内部 褒甲板u及内裝甲板15之上游表面上的金屬塗層24及/或 % ’如圖1中所描繪。然而，在外板12上額外地具有金屬 塗層22以錢裝甲板12摩擦熔接/結合至發㈣ 能係較佳的。 _尹不意性展示，多個發射體30,、30··、30,,，，产 ^箭頭34所指示之初始彈道朝外板⑵亍進。雖然該等發I 體、!描繪為大體球形，但是其可為任何特定形狀。 如圖3时示意性展示，第—發射體3〇，已遇到外 體3°，已側向變形成-較平坦形狀且使板變形。： :擊引發之裂口的準確組態回應於形成板12的材料之動性 改變’但當發射體遇到金屬層時’其傾向於彈出幾乎整 137805.doc -18· 200940945 體之栓塞12”，該栓塞12"包含裝f板12之材料，其上嵌有 變形之發射體30,（如圖3C中示意性描繪）。圖3D描繪經組 合且側向變大之發射體3〇,及第一層裝甲之部分12"以及在 第二層14上之第二發射體3〇”的效應。特定言之，組合之 發射體3G及裝甲栓塞12,·之橫向變形已切下並彈出兩個發 射體30,及30”與第一及第二裝甲板之部分12"及14•的更大 之組合。 發射體30’及3〇”與已自頭兩個裝甲板切下的裝甲 板。P刀（12及14 )之組合遇到圖3E中之最後裝甲層。該組 合使圖3F中之另—或”内"裝f板"變形，但發射體與自第 一層切下的裝甲之摩擦熔接/結合部分的組合之大小以一 不足以挫敗最後裝甲層15之速度移動，該最後裝甲層^可 為如將在下文論述之金屬裝甲板。 "在，佳實施例中，外金屬裝曱層對於鋼板具有M，〇〇〇碎/ "英对之極限拉伸強度及對於銘板具有3〇，_碎/平方英 时之極限拉伸強度，佬怨古 、 使得同逮發射體在擊中裝曱表面時可 大體上被壓平。然而裝甲不應太脆以致允許變形衝擊使初 層開裂並在初始裝甲層十穿孔（而不沿彈道自發射 移除能1與動量）β圖2八中騎此非較佳之現象 t外裝甲金屬層將具有相對較高之拉伸斷裂伸長率。, 外裝甲層具有高破裂韌,秘吐 田 眭時，穿透外層之材料之質量可增 加’但其速度降低且更多之材料側向分散。 若裝甲板為銘合金，較佳地其 更佳10%之斷裂伸县宠从， 田丹，芏乂 7/〇且 伸長率的銘合金組成。較佳鋁合金之實例 137805.doc 200940945 包括：7017、7178-T6、7039 Τ-64、7079-T6、7075-T6及 Τ651、5083-0、5083-Η113、5050 HI 16及 6061-Τ6。當裝 甲層基本上由紹合金組成時’較佳地其具有在8至4〇毫米 之範圍内之厚度。若外裝甲板為鋼，較佳地此板基本上由 具有至少7%且更佳10%之斷裂伸長率的材料組成。較佳鋼 之實例包括：SSAB Weldox 700、SSAB Armox 500T(瑞 典，Oxelesund之SSAB 〇xel6sund之產品）、R〇Q_TUF、According to the invention, the first dispersion space has a sufficient length in a direction substantially perpendicular to the plate to allow significant lateral dispersion of the material passing through the first dispersion space. As embodied herein in a system comprising a series of metal mounting panels as shown in the drawings, the dispersion space 18 has sufficient thickness (as indicated by arrow 19) to allow for significant lateral dispersion of material within the dispersion space 18 ( The emitter and plate 12 portion 12" schematically shown in Figures 3A-C. ^ In this second aspect of the invention, the outer panel 12 may have a 5/not metal coating 22 on its front surface. To promote fusion/bonding between the first emitter 30 and the outer panel 12. In particular, one or more metal layers or coatings may be provided between one or more adjacent metal armor plates, such as metal coatings on the inner surface of the inner raft deck u and the inner deck 15, respectively. 24 and / or % ' as depicted in Figure 1. However, it is preferred to additionally have a metal coating 22 on the outer panel 12 to frictionally weld/bond to the hair (4). _ Yin unintentional display, multiple emitters 30,, 30 · ·, 30,,,, produced by the arrow 34, the initial ballistics are pushed toward the outer panel (2). Although these hairs, ! are depicted as generally spherical, they can be of any particular shape. As schematically shown in Fig. 3, the first emitter 3〇, which has encountered an outer body 3°, has been laterally deformed - a relatively flat shape and deformed the plate. : : The exact configuration of the crack caused by the shot responds to the dynamic change of the material forming the plate 12 'but when the emitter encounters the metal layer ' it tends to pop up almost 137805.doc -18 · 200940945 body plug 12" The plug 12" comprises a material enclosing the plate 12 with a deformed emitter 30 embedded therein (as schematically depicted in Figure 3C). Figure 3D depicts the combined and laterally enlarged emitter 3〇, and The effect of the first layer of armored portion 12" and the second emitter 3' on the second layer 14". In particular, the combination of the emitter 3G and the armor plug 12, the lateral deformation has been cut and popped up with two emitters 30, and the 30" is larger with the first and second armor plates 12" and 14• The combination of the launcher 30' and 3" and the armor plate that has been cut from the first two armor panels. The combination of P-knife (12 and 14) encounters the final armor layer in Figure 3E. This combination deforms the other or "inner" of Figure 3F, but the combination of the emitter and the friction-welding/bonding portion of the armor cut from the first layer is not sufficient to defeat the final armor. The speed of layer 15 is moved, and the final armor layer can be a metal armor plate as will be discussed below. " In a preferred embodiment, the outer metal mounting layer has M for the steel plate, mashing &"英The ultimate tensile strength and the ultimate tensile strength of the 铭 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ It should not be too brittle to allow the deformation shock to crack the initial layer and remove the energy in the initial armor layer (without removing the energy 1 and momentum from the ballistic self-emission). Figure 2 is a non-preferred phenomenon. It has a relatively high tensile elongation at break. The outer armor layer has a high fracture toughness. When the secret layer is used, the quality of the material penetrating the outer layer can be increased, but the speed is reduced and more materials are laterally dispersed. The board is a good alloy, preferably 10% better. It is composed of Ming alloys from Shenxian, Tiandan, 芏乂7/〇 and elongation. Examples of preferred aluminum alloys 137805.doc 200940945 Includes: 7017, 7178-T6, 7039 Τ-64, 7079-T6, 7075 -T6 and Τ651, 5083-0, 5083-Η113, 5050 HI 16 and 6061-Τ6. When the armor layer consists essentially of a smelting alloy, it preferably has a thickness in the range of 8 to 4 mm. The outer armor is steel, preferably the board consists essentially of a material having an elongation at break of at least 7% and more preferably 10%. Examples of preferred steels include: SSAB Weldox 700, SSAB Armox 500T (Sweden, Oxelesund) SSAB 〇xel6sund products), R〇Q_TUF,
ROQ-TUF AM700(美國，Indiana，East Chicag〇，奶制ROQ-TUF AM700 (USA, Indiana, East Chicag〇, milk system
Steel之產品）、ASTM A517及滿足美國軍用規格mil 46i〇〇 之鋼。當裝甲層基本上由鋼組成時，較佳地其具有在5至 2〇毫米之範圍内的厚度。 尤刖所挪述，高強度材料可替代用以促進與發射體金 屬摩擦熔接或結合之金屬塗層22(或除金屬塗層22外還可） 用於外裝甲板12之外表面上。此材料之實例為陶究装甲。 此外層可引發發㈣之***並對付㈣於本發明所對付之 相對大質量、軟的發射體的其它類型發射體。 散ΪΓΓ另—實施例亦藉由將分散元件(未圖示)置於分 t間中而弓」發穿過分層設備中之分散空間之材料的側向 發受輸分散元件中之所引 ㈣波载有由穿透體施加在分散元件上 =比。接著此能量將分散元件作為裂片發射，二 二量之物件必須將該能量傳遞至另-接收器 本發明之—態樣，可提供—内金屬 千仃於内部金屬裝甲板而安置极其大致 直且自該内 137805.doc 20· 200940945 下游位移以形成一第二分散空間，該第二分散空間足夠厚 以允許穿過其之材料的顯著側向分散。 如此處所體現及圖丨中所描繪，系統可包括内金屬裝曱 板15，其與上游（相對於彈道）内部金屬裝曱板14形成分散 二間20。如上文所揭示’内裝甲板之主要目的為防止已分 散並由穿過系統之上游部分（亦即，外金屬裝甲板12、内 部金属裝曱板14、分散空間18及金屬塗層24(及塗層22， 若板12經定位以首先遭遇發射體））而減慢的材料之任何進 一步穿透。所描繪之實施例包括三個板但本發明並非限制 於板之該數目，因此在揭示案中引用的"内"裝甲板臨近 "内部”裝甲板》因此，本發明可包括多於或少於三個裝曱 板。又，更佳地最内部之裝甲板包含具有高破裂韌性之材 料以抵抗撞擊於其上之材料的任何進一步穿透。 較佳内板包含具有大於350之勃氏硬度的材料。更佳地 内板基本上由自由以下各物組成之群中選出的材料組成： 鋁合金、鋼合金及鈦合金、金屬基質複合物及聚合物基質 複合物。如已反覆揭示，系統之目標中之一者係引發穿過 裝曱系統之材料之分散以提高此材料不穿透系統之機率。 本發明之另一態樣係將裝曱系統併入到現有車輛（裝甲 或非裝甲）上。對於非裝甲車麵，内裝甲板應抵抗穿過裝 曱系統之任何材料之穿透，以使該材料不進入車輛。以此 方式，非裝曱車輛在穿甲彈藥或設備攻擊下之生存能力顯 著改良。藉由將本發明系統併入到裝曱車輛之外部表面 上，裝甲車輛對穿曱彈藥或設備攻擊之抵抗能力可得以進 137805.doc 21 · 200940945 一步改良。 中描繪抗穿透性得以改良之 為具有包含镇Μ # w 裝甲車輛之實施例，圖4 輛二= 殼式車身38的防爆裝甲陸地車 ,之底 在此實施例中，車身38具有界定至少 中心分4°，其中V形之頂點大體平行於車翻之 車輛之外部。 本發月之裝甲系統被固定至裝甲 ❹Steel's products), ASTM A517 and steel that meets US military specifications mil 46i〇〇. When the armor layer consists essentially of steel, it preferably has a thickness in the range of 5 to 2 mm. In particular, the high strength material may be substituted for the metal coating 22 (or in addition to the metal coating 22) for facilitating frictional fusion or bonding with the emitter metal for use on the outer surface of the outer deck 12. An example of this material is ceramic armor. The additional layer may initiate the splitting of the (four) and other types of emitters of the relatively large mass, soft emitters to which the invention is directed. The divergence-embodiment is also cited in the laterally-transferring and dispersing element of the material that passes through the dispersing space in the layering device by placing the dispersing element (not shown) in the interval t (4) The wave load is applied by the penetrating body on the dispersing element = ratio. This energy then causes the dispersing element to be emitted as a split, and the two-component object must transfer this energy to the other embodiment of the present invention, which provides that the inner metal is placed substantially flat on the inner metal armor plate and From the inner 137805.doc 20·200940945 downstream displacement to form a second dispersion space that is thick enough to allow significant lateral dispersion of the material passing therethrough. As embodied herein and depicted in the drawings, the system can include an inner metal mounting panel 15 that forms a discrete two compartment 20 with the upstream (relative to the ballistic) inner metal mounting panel 14. As disclosed above, the primary purpose of the interior deck is to prevent it from being dispersed and passing through the upstream portion of the system (ie, the outer metal armor plate 12, the inner metal mounting plate 14, the dispersion space 18, and the metal coating 24 (and The coating 22, if the plate 12 is positioned to first encounter the emitter)), slows any further penetration of the material. The depicted embodiment includes three plates but the invention is not limited to this number of plates, and therefore the "inside" armored adjacent "internal" armor plate cited in the disclosure therefore, the invention may include more than Or less than three mounting plates. Also, preferably the innermost armor panel comprises a material having high fracture toughness to resist any further penetration of the material impinging thereon. Preferably, the inner panel contains a bolus greater than 350. Harder material. More preferably, the inner panel consists essentially of materials selected from the group consisting of: aluminum alloys, steel alloys and titanium alloys, metal matrix composites and polymer matrix composites. One of the goals of the system is to initiate dispersion of material through the mounting system to increase the probability that the material will not penetrate the system. Another aspect of the invention incorporates the mounting system into an existing vehicle (armor or non-armor) Armor). For non-armored surfaces, the interior deck shall resist penetration of any material passing through the mounting system so that the material does not enter the vehicle. In this manner, the non-mounted vehicle is in armor-piercing projectiles. The survivability of drugs or equipment attacks is significantly improved. By incorporating the system of the invention into the exterior surface of the mounted vehicle, the resistance of the armored vehicle to the attack of the ammunition or equipment can be advanced. 137805.doc 21 · 200940945 Improved. The improved penetration resistance is improved with an embodiment comprising a ballast #w armored vehicle, Figure 4 is an explosion-proof armored land vehicle with a shell body 38, in this embodiment, the body 38 has Define at least 4° in the center, where the apex of the V is roughly parallel to the outside of the vehicle. The armor system of this month is fixed to the armor.
一替代實施例為添加至現有車鈿 负皁輛或車輛之部分的根據所 揭不系統的分層裝甲板之一岑客伽扼 次多個獨立總成，以增強其對 上文所描述之武器之抵抗力。 在較佳實施例中，用以形成車身38之薄片材料16可為至 少兩種不同之薄片材料。在圖4中所描繪之實施例中，包 含v形部分42(此處為"雙頦"V型）之車身38之部分可由堅勒 薄片材料形成。如本文所使用，詞語"堅勤"為抵抗裂縫經 由八擴張之材料’大體稱為具有高破裂韌性之材料。如此 處所體S，底部部分40(包含V形部分42)較佳地為已知為 ”R〇Q-tuf AM700(Indiana ’ East Chicago，Mittal Steel之產 品）之薄片鋼。已知為SSAB Weld〇x 7〇〇(瑞典，〇xel6sund 之SSAB 〇xeli5Sund之產品）的另一材料亦較佳作為用於底 部部分40之材料。亦可使用類似A5 17、A514之通常用於 建造鍋爐的鋼及具有可與Weld〇x 7〇0相當的類 似屈服強度及斷裂伸長率之其他鋼。車身38之上部部分44 較佳地由裝甲板形成。尤其較佳之材料已知為SSAb Armox 400(瑞典 ’ 〇xel3sund之SSAB Oxeldsund之產品）， 137805.doc -22· 200940945 ，管滿足美請L_A_4議之^將係可行I大體而 »薄片材料較佳地基本上由自由以下各物組成之群中選 出之金屬組成：鋼、鋼裝甲、鈦合金及鋁合金。An alternative embodiment is a plurality of independent assemblies of one of the tiered armor plates added to the existing ruthenium or vehicle portion to enhance the above described The resistance of weapons. In the preferred embodiment, the sheet material 16 used to form the body 38 can be at least two different sheet materials. In the embodiment depicted in Figure 4, a portion of the body 38 that includes a v-shaped portion 42 (here "double 颏" V-type) may be formed from a sheet of sheet material. As used herein, the term "hard work" is a material that has high fracture toughness for materials that resist cracking through eight expansions. As described herein, the bottom portion 40 (including the V-shaped portion 42) is preferably a sheet steel known as "R〇Q-tuf AM700 (Indiana 'East Chicago, product of Mittal Steel). Known as SSAB Weld〇 Another material of x 7〇〇 (Swedish, product of SSAB 〇xeli5Sund of 〇xel6sund) is also preferred as the material for the bottom portion 40. It is also possible to use steels similar to those used in A5 17 and A514 for the construction of boilers and Other steels of similar yield strength and elongation at break comparable to Weld® x 7 〇 0. The upper portion 44 of the body 38 is preferably formed by armor plates. Particularly preferred materials are known as SSAb Armox 400 (Swedish '〇xel3sund The product of SSAB Oxeldsund), 137805.doc -22· 200940945, the tube meets the US, please L_A_4, which will be feasible, and the thin-sheet material is preferably composed of a metal selected from the group consisting of the following free radicals. : Steel, steel armor, titanium alloy and aluminum alloy.
在另一較佳實施财’車輛車身包括經組態並經設計以 鄰近車輛36之車身38的薄片裝甲16之内部表面的内部薄片 裝曱46之系統。如此處體現，及圖5中所描繪，車㈣包 括先前描述之裝甲系統1G，冑甲系統1〇具有外金屬裝甲板 12、内部金屬裝甲板14及鄰近車身此金屬薄片裝甲此 外部表面的内金屬裝甲板15。車輛36亦具有一層鄰近車身 之内部表面的薄片裝f46H較佳實施例中，此薄片 裝甲46可包含一硬質聚合物/纖維複合物。 車輕36之内部薄片裝甲46亦可包含一種包含纖維之編織 物。又一較佳實施例包括編織物46,之内部裝甲層（該編織 物46’包含纖維及複數個陶瓷板48)，如圖6中示意性描繪。 在車輛36之又一實施例中（圖7中所描繪），鄰近車輛内 部表面38之纖維薄片裝甲46，（或硬質聚合物/纖維複合物 46,或另一層金屬裝甲板（未圖示）)與内部表面間隔以形成 間隙50〇 雖然本發明提供對固體發射體之抵抗力，但其亦提供添 加對狹長固體及液體發射體之防護的機會。如上文在背景 刀中所揭示’存在具有兩層裝甲之系統，其中一電導體 安置於兩層裝甲之間。在電導體與裝甲之相鄰表面之間建 立一顯著電位。當液體或固體穿透體穿透裝甲時，其在裝 甲層與電導體之間建立一導電路徑，該電位經由該路徑放 137805.doc -23- 200940945 電。當存在經由穿透體放電之足夠電能量時，穿透體被熔 融或汽化’且其穿透下一層裝曱之能力顯著降低。因為此 系統可容易地併入於本發明之裝甲系統中而無顯著之劣 勢，所以本發明之較佳實施例包括一安置於兩個相鄰裝甲 板之間的分散空間中之導電部件。 如此處所體現及圖8中所描繪，提供電力源52以施加電 力至兩個相鄰金屬裝曱板（亦即，板12或14)中之任一者及 安置於分散空間18中之導電部件54。冑力供應源經組態以 提供足夠電力以使在兩個相鄰金屬裝甲板中之至少一者與 導電部件54之間形成電連接的狹長發射體之至少一部分分 散。 圖9為包括本發明之又一實施例之車輛之示意部分截面 圖如圖9中所示，車輛車身包括—包含—金屬裝甲材料 之車身邛件1 6，在該車身部件上安置兩個間隔開之金屬裝 甲板（高硬度板裝曱或堅韌、更具延展性之板材料），其經 描繪為外層12及内部層14。在圖9實施例中，車身金屬裝 甲薄片16提供如先前所論述的圖1實施例中之内金屬裝曱 板丨5之功能。雖然此實施例被描繪為車輛之整體部分，但 八亦可包含用於增強車輛之任何所要部分之防護的附加總 成。 熟％此項技術者將顯而易見，可對本發明做出各種修改 及變化。本發日月&括屬於以下申請專利範圍及其等效物之 範疇内之本發明的修改及變化。 【圖式簡單說明】 137805.doc -24· 200940945 圖1為本發明之一實施例的透視示意圖； 圖2A-B為兩個正由單個相對大質量之非狹長固體發射體 穿透的不同裝甲板之示意截面圖； 圖3 A-F描繪正遭到一系列相對大質量之非狹長固體發射 體寺驗的裝甲板之—序列示意截面側視圖； 圖4為包括本發明之-實施例之裝甲車輛的示意截面 圓，In another preferred embodiment, the vehicle body includes a system of internal sheet assemblies 46 that are configured and designed to be adjacent to the interior surface of the sheet armor 16 of the body 38 of the vehicle 36. As embodied herein, and depicted in FIG. 5, the vehicle (4) includes the armor system 1G previously described, the armor system 1 has an outer metal armor deck 12, an inner metal armor deck 14 and an adjacent outer surface of the outer surface of the foil armor. Metal armor plate 15. The vehicle 36 also has a sheet of f46H adjacent the interior surface of the body. In the preferred embodiment, the sheet armor 46 can comprise a rigid polymer/fiber composite. The inner sheet armor 46 of the vehicle light 36 may also comprise a braid comprising fibers. A further preferred embodiment includes a braid 46 having an inner armor layer (the braid 46' comprising fibers and a plurality of ceramic sheets 48), as schematically depicted in FIG. In yet another embodiment of the vehicle 36 (depicted in Figure 7), the fiber sheet armor 46 adjacent to the interior surface 38 of the vehicle, (or hard polymer/fiber composite 46, or another layer of metal armor plate (not shown) Intervaling from the interior surface to form a gap 50. Although the present invention provides resistance to solid emitters, it also provides the opportunity to add protection to elongated solids and liquid emitters. As disclosed above in the background knife, there is a system with two layers of armor in which an electrical conductor is placed between the two layers of armor. A significant potential is established between the electrical conductor and the adjacent surface of the armor. When a liquid or solid penetrating body penetrates the armor, it establishes a conductive path between the armor layer and the electrical conductor, through which the potential is discharged by 137805.doc -23-200940945. When there is sufficient electrical energy to discharge through the penetrating body, the penetrating body is melted or vaporized' and its ability to penetrate the next layer of mounting is significantly reduced. Since this system can be easily incorporated into the armor system of the present invention without significant disadvantages, the preferred embodiment of the present invention includes a conductive member disposed in a dispersing space between two adjacent armor plates. As embodied herein and depicted in FIG. 8, a power source 52 is provided to apply power to either of two adjacent metal mounting plates (ie, plates 12 or 14) and conductive components disposed in the discrete space 18. 54. The power supply is configured to provide sufficient power to dissipate at least a portion of the elongated emitter that forms an electrical connection between at least one of the two adjacent metal armor plates and the conductive member 54. Figure 9 is a schematic partial cross-sectional view of a vehicle including a further embodiment of the present invention. As shown in Figure 9, the vehicle body includes a body member 16 containing a metal armor material, and two compartments are placed on the body member. Open metal armor panels (high hardness panel or tough, more ductile sheet material), depicted as outer layer 12 and inner layer 14. In the embodiment of Fig. 9, the body armor sheet 16 provides the function of the inner metal platen 5 of the embodiment of Fig. 1 as previously discussed. While this embodiment is depicted as an integral part of the vehicle, eight may also include additional assemblies for enhancing the protection of any desired portion of the vehicle. It will be apparent to those skilled in the art that various modifications and changes can be made in the present invention. Modifications and variations of the present invention within the scope of the following claims and their equivalents are included. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic perspective view of an embodiment of the present invention; FIG. 2A-B are two different armor being penetrated by a single relatively large mass of non-narrow solid emitters. Figure 3 is a schematic cross-sectional side view of an armor plate undergoing a series of relatively large mass non-narrow solid emitters; Figure 4 is an armored vehicle including the embodiment of the present invention. Schematic cross section circle,
圖5為本發明之實施例之示意截面圖，其中組成車輛車 身之裝甲與本發明之内裝甲板相鄰並與其間隔開，且該車 輛在車身内包括内部發射體吸收層； 圖6為本發明之實施例之示意截面圖，其中組成車辆車 身之裝甲與本發明之内裝f板相鄰並與其間隔開，且該車 輛在車身内包括織物及陶瓷板之内部發射體吸收層丨 園/為本發明之實施例 〜叫叫六τ殂成旱輛車 裝甲與本發明之内裝甲板相鄰並與其間隔開，且該車 輛在車身内包括與車身間隔開以形成—間隙的織物及陶 板之内部發射體吸收層； 瓦 圖8為本發明之-實施例之透視圖，其中在相鄰的 間隔開之裝甲板之間存在一導電薄片： f 圖9為併人有本發明之實施例的^車_之透 面圖，其中車輛車身裝甲層包含内裝甲板。 刀戴 【主要元件符號說明】 10 裝曱系統 外裝甲板/外金屬裝甲板 137805.doc -25- 200940945 12' 板部分 12" 板部分/栓塞 14 内部金屬裝甲板 14' 板部分 15 内金屬裝曱板 16 薄片裝甲/薄片材料/車身部件/裝曱板 ' 18 第一分散空間 19 距離/箭頭 ❹ 20 第二分散空間 22 金屬塗層 24 金屬塗層 26 金屬塗層 30 發射體 30' 發射體 30" 發射體 30"' 發射體 φ 34 彈道/箭頭 36 防爆裝曱陸地車輛/車輛 • 38 車身/車輛内部表面 40 底部部分 42 V形部分 44 車身之上部部分 46 硬質聚合物/纖維複合物/内部薄片裝曱 46' 纖維薄片裝甲/編織物 137805.doc -26- 200940945 48 50 52 54 陶瓷板 間隙 電力源 導電部件 ❹ 137805.doc -27Figure 5 is a schematic cross-sectional view of an embodiment of the present invention in which the armor constituting the vehicle body is adjacent to and spaced apart from the interior deck of the present invention, and the vehicle includes an inner emitter absorbing layer in the vehicle body; A schematic cross-sectional view of an embodiment of the invention in which the armor constituting the vehicle body is adjacent to and spaced apart from the inner panel of the present invention, and the vehicle includes an inner emitter absorbing layer of fabric and ceramic sheets in the vehicle body. / is an embodiment of the present invention - the vehicle is called a six-turt-dry truck armor adjacent to and spaced apart from the interior deck of the present invention, and the vehicle includes a fabric spaced apart from the vehicle body to form a gap in the vehicle body and An internal emitter absorptive layer of a ceramic panel; FIG. 8 is a perspective view of an embodiment of the present invention in which a conductive sheet is present between adjacent spaced apart armor plates: f FIG. 9 is an implementation of the present invention. For example, the vehicle's armor layer contains a built-in deck. Knife wearing [main component symbol description] 10 mounting system exterior deck / outer metal armor plate 137805.doc -25- 200940945 12' plate part 12" plate part / plug 14 internal metal armor plate 14' plate part 15 inner metal曱16 16 sheet armor/sheet material/body parts/frames' 18 first dispersion space 19 distance/arrow ❹ 20 second dispersion space 22 metal coating 24 metal coating 26 metal coating 30 emitter 30' emitter 30" Emitter 30"' Emitter φ 34 Ballistic/Arrow 36 Explosion-Proof Land Vehicle/Vehicle • 38 Body/Vehicle Interior Surface 40 Bottom Section 42 V-Shaped Section 44 Upper Body Section 46 Hard Polymer/Fiber Composite/ Internal sheet mounting 46' Fiber sheet armor/braid 137805.doc -26- 200940945 48 50 52 54 Ceramic plate gap power source conductive parts 137 137805.doc -27
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| US9170071B2 (en) * | 2006-05-01 | 2015-10-27 | Warwick Mills Inc. | Mosaic extremity protection system with transportable solid elements |
| US8966669B2 (en) | 2010-02-12 | 2015-03-03 | James Michael Hines | Shock wave generation, reflection and dissipation device |
| PL2796827T3 (en) * | 2013-04-22 | 2018-08-31 | Constellium Valais Sa (Ag, Ltd) | Composite panel for vehicle armour |
| DE102019116153A1 (en) * | 2019-06-13 | 2020-12-17 | Kennametal Inc. | Armor plate, armor plate composite and armor |
| DE102019116363A1 (en) | 2019-06-17 | 2020-12-17 | Benteler Automobiltechnik Gmbh | Method for the production of an armor component for motor vehicles |
| TR202003526A1 (en) * | 2020-03-06 | 2021-09-21 | Secant Teknoloji Gelistirme Sanayi Ve Ticaret Anonim Sirketi | ADDITIONAL ARMOR SYSTEM FOR ARMORED VEHICLES |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1236033A (en) * | 1917-04-18 | 1917-08-07 | Salvador Montes Almengual | Protective armor. |
| US3164465A (en) * | 1962-11-08 | 1965-01-05 | Martin Metals Company | Nickel-base alloys |
| US4090011A (en) * | 1964-07-02 | 1978-05-16 | Reynolds Metals Company | Armor |
| US5429031A (en) * | 1973-05-02 | 1995-07-04 | The United States Of America As Represented By The Secretary Of The Army | Light weight armor |
| US5007326A (en) * | 1990-01-16 | 1991-04-16 | The United States Of America As Represented By The Secretary Of The Army | Cast single plate P900 armor |
| DE4116088A1 (en) * | 1991-05-16 | 1992-11-19 | Forschungszentrum Juelich Gmbh | METHOD FOR JOINING STEEL WITH ALUMINUM OR TITANIUM ALLOY PARTS AND TURBOCHARGERS RECEIVED AFTER |
| US6216579B1 (en) * | 1998-10-15 | 2001-04-17 | Her Majesty The Queen In Right Of Canada, As Represented By The Solicitor General Acting Through The Commissioner Of The Royal Mounted Canadian Police | Composite armor material |
| US7082868B2 (en) * | 2001-03-15 | 2006-08-01 | Ati Properties, Inc. | Lightweight armor with repeat hit and high energy absorption capabilities |
| US6758125B1 (en) * | 2002-12-18 | 2004-07-06 | Bae Systems Information And Electronic Systems Integration Inc. | Active armor including medial layer for producing an electrical or magnetic field |
| US7513186B2 (en) * | 2004-03-11 | 2009-04-07 | Plasan-Kibbutz Sasa | Ballistic armor |
| US20060013977A1 (en) * | 2004-07-13 | 2006-01-19 | Duke Leslie P | Polymeric ballistic material and method of making |
| US7357062B2 (en) * | 2006-04-11 | 2008-04-15 | Force Protection Industries, Inc. | Mine resistant armored vehicle |
-
2008
- 2008-01-23 US US12/010,268 patent/US20120090451A1/en not_active Abandoned
-
2009
- 2009-01-14 WO PCT/US2009/030941 patent/WO2009094271A1/en active Application Filing
- 2009-01-22 TW TW098102667A patent/TW200940945A/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| WO2009094271A1 (en) | 2009-07-30 |
| WO2009094271A8 (en) | 2009-10-01 |
| US20120090451A1 (en) | 2012-04-19 |
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