JP2939532B2 - Parallel flying eccentric reactive defense structure - Google Patents

Parallel flying eccentric reactive defense structure

Info

Publication number
JP2939532B2
JP2939532B2 JP5463697A JP5463697A JP2939532B2 JP 2939532 B2 JP2939532 B2 JP 2939532B2 JP 5463697 A JP5463697 A JP 5463697A JP 5463697 A JP5463697 A JP 5463697A JP 2939532 B2 JP2939532 B2 JP 2939532B2
Authority
JP
Japan
Prior art keywords
explosive
jet
parallel
metal
flying
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP5463697A
Other languages
Japanese (ja)
Other versions
JPH10253296A (en
Inventor
慶康 油井
正 水野
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BOEICHO GIJUTSU KENKYU HONBUCHO
Original Assignee
BOEICHO GIJUTSU KENKYU HONBUCHO
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BOEICHO GIJUTSU KENKYU HONBUCHO filed Critical BOEICHO GIJUTSU KENKYU HONBUCHO
Priority to JP5463697A priority Critical patent/JP2939532B2/en
Publication of JPH10253296A publication Critical patent/JPH10253296A/en
Application granted granted Critical
Publication of JP2939532B2 publication Critical patent/JP2939532B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/007Reactive armour; Dynamic armour

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明が属する技術分野】本発明は、爆薬等爆発性のエ
ネルギ物質のエネルギを利用した反応性防御構造(以下
防御構造と略する)に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a reactive defense structure (hereinafter, abbreviated as a defense structure) utilizing the energy of an explosive energy material such as an explosive.

【0002】[0002]

【従来の技術】従来の防御構造の構造は、図4に示すよ
うに、2枚の金属製平板21、23の間に爆薬等爆発性
のエネルギ物質22を充填した構造である。
2. Description of the Related Art As shown in FIG. 4, a conventional defense structure has a structure in which an explosive or other explosive energy substance 22 is filled between two metal flat plates 21 and 23. As shown in FIG.

【0003】上記金属製平板とエネルギ物質とから構成
される従来の防御構造は、円錐状の金属製ライナを有す
る爆薬筒(以下爆薬筒と略する)から発生する金属の流
体又は粉体状の金属の高速の流れ(以下ジェットと略す
る)に対しては極めて良好な減殺効果(以下ジェット減
殺効果と略する)を発揮するが、このジェット減殺効果
は爆薬筒から発生したジェットが防御構造に入射する角
度、すなわち爆薬筒から発生したジェットと防御構造の
金属製平板面の法線とが成す角度である撃角に大きく依
存するため、爆薬筒から発生したジェットが防御構造に
小さな撃角で入射した場合、防御構造による爆薬筒から
発生したジェットの能力のジェット減殺効果は著しく低
下する。また、各種車両等に装着された防御構造が、爆
薬筒によってその機能を発揮した時、車両等の外板に近
い側の防御構造の金属製平板が高速で車両等の外板に衝
突するため、車両等の外板がスポール破壊等の被害を受
ける可能性がある。
[0003] A conventional defense structure composed of a metal flat plate and an energy material is a metal fluid or powder generated from an explosive cylinder having a conical metal liner (hereinafter abbreviated as an explosive cylinder). It exerts a very good abatement effect (hereinafter abbreviated as a jet abatement effect) against a high-speed flow of metal (hereinafter abbreviated as a jet). Since the angle of incidence, that is, the angle of attack, which is the angle between the jet generated from the explosive cylinder and the normal of the metal plate surface of the defense structure, greatly depends on the jet generated from the explosive cylinder, In the event of an incident, the jet-attenuating effect of the capability of the jet generated from the explosive cartridge by the defensive structure is significantly reduced. Also, when the defense structure mounted on various vehicles, etc. exerts its function by the explosive cylinder, the metal plate of the defense structure on the side close to the outer plate of the vehicle collides with the outer plate of the vehicle at high speed. There is a possibility that the outer panel of a vehicle or the like may be damaged by spalling.

【0004】[0004]

【発明が解決しようとする課題】図5〜図7は、従来の
防護構造の作用を説明するための図であり、これにより
従来の防護構造の課題を具体的に説明する。爆薬筒から
発生したジェット31が従来の防御構造に衝突するとエ
ネルギ物質22は速やかに反応し、2枚の金属製平板2
1、23は金属製平板面の法線方向に高速で飛しょうを
開始する。この高速で飛しょうする2枚の金属製平板
が、図5に示すように、爆薬筒から発生したジェットと
相互干渉を起こす結果、ジェットの能力は大幅に減殺さ
れる。32は金属製平板と干渉して能力を失った爆薬筒
から発生したジェットである。しかしながら、このジェ
ット減殺機構から明らかなように、従来の防御構造で
は、図6に示すように、爆薬筒から発生したジェットが
防御構造に小さな撃角で入射した場合、防御構造の金属
製平板21及び23によって、爆薬筒から発生したジェ
ット31の能力を減殺することは困難であり、良好なジ
ェット減殺効果を発揮することはほとんど期待できない
という欠点がある。また、各種車両等に装着された防御
構造が、爆薬筒によってその機能を発揮した時、高速で
飛しょうする防御構造の金属製平板のうち、車両等の外
板に近い側の金属製平板23が、高速で車両等の外板5
3に衝突するため、図7に示すように、車両等の外板が
スポール破壊等の被害を受け(破壊片54、55)を受
ける可能性がある。本発明の平行飛しょう型偏心防御構
造は、従来のエネルギ物質を2枚の金属製平板により挟
んだ防御構造の構造の諸欠点にかんがみて、各種の改良
を加えた結果、完成するに至ったものである。
FIGS. 5 to 7 are diagrams for explaining the operation of the conventional protective structure, and the problems of the conventional protective structure will be specifically described. When the jet 31 generated from the explosive cylinder collides with the conventional defense structure, the energy substance 22 reacts quickly and the two metal flat plates 2
Nos. 1 and 23 start flying at a high speed in the direction of the normal to the flat metal surface. As shown in FIG. 5, the two metal plates flying at high speed mutually interfere with the jet generated from the explosive cartridge, and as a result, the capability of the jet is greatly reduced. Numeral 32 denotes a jet generated from an explosive cartridge that has lost its ability due to interference with a metal flat plate. However, as is apparent from this jet abatement mechanism, in the conventional defense structure, as shown in FIG. 6, when the jet generated from the explosive cartridge enters the defense structure at a small angle of attack, the metal plate 21 of the defense structure is not used. And 23, it is difficult to reduce the capability of the jet 31 generated from the explosive cartridge, and there is a drawback that it is hardly expected to exhibit a good jet attenuating effect. Further, when the defense structure mounted on various vehicles and the like exerts its function by the explosive cylinder, the metal plate 23 on the side closer to the outer plate of the vehicle among the metal plates of the defense structure flying at high speed. But at high speed
7, there is a possibility that the outer plate of the vehicle or the like suffers damage such as spall destruction (destruction pieces 54 and 55) as shown in FIG. The parallel flying eccentric protection structure of the present invention has been completed as a result of various improvements in view of the various drawbacks of the conventional protection structure in which an energy substance is sandwiched between two metal flat plates. Things.

【0005】すなわち、本発明の平行飛しょう型偏心防
御構造は、爆薬筒から発生したジェットが平行飛しょう
型偏心防御構造に入射する角度に依存せず、従来の防御
構造以上の高いジェット減殺効果を発揮することが可能
な防御構造のみならず、各種車両等に装着された平行飛
しょう型偏心防御構造が、爆薬筒によってその機能を発
揮した時、高速で飛しょうする平行飛しょう型偏心防御
構造の車両等の外板に近い側の金属製板による車両等の
外板のスポール破壊等の被害を軽減する防御構造を提供
することを目的とするものである。
That is, the parallel flight type eccentric protection structure of the present invention has a higher jet attenuating effect than the conventional protection structure without depending on the angle at which the jet generated from the explosive cartridge enters the parallel flight type eccentric protection structure. Not only the defensive structure that can demonstrate the effect, but also the parallel flying type eccentric defense structure mounted on various vehicles, etc., when the function is demonstrated by the explosive cartridge, the parallel flying type eccentric protection that flies at high speed It is an object of the present invention to provide a defense structure for reducing damage such as spall breakage of an outer plate of a vehicle or the like by a metal plate on the side close to the outer plate of the vehicle or the like having a structure.

【0006】[0006]

【課題を解決するための手段】本発明の平行飛しょう型
偏心防御構造は、図1の実施の形態に示すように、2枚
の金属製板11、13の間に爆薬等爆発性のエネルギ物
質12を充填した構造を有する反応性防御構造におい
て、前記2枚の金属製板11、13は、その一端面の側
から他端面の側に向けて、その厚さが傾斜状に変化した
形状であり且つ一方の金属製板11と他方の金属製板1
3とで厚さの変化の方向が反対方向とされたことを特徴
としている。すなわち、厚さが非対称な2枚の金属製板
11、13の間にエネルギ物質12を充填した構造であ
る。
As shown in the embodiment of FIG. 1, the parallel flying type eccentric protection structure of the present invention has an explosive energy such as an explosive between two metal plates 11 and 13. In a reactive defense structure having a structure filled with a substance 12, the two metal plates 11, 13 have a shape in which the thickness is inclined from the one end surface to the other end surface. And one metal plate 11 and the other metal plate 1
3 is characterized in that the direction of the change in the thickness is made the opposite direction. That is, the energy material 12 is filled between two metal plates 11 and 13 having asymmetric thicknesses.

【0007】[0007]

【作用】平行飛しょう型偏心防御構造の構造を、厚さが
非対称な2枚の金属製板の間にエネルギ物質を充填した
構造にすることにより、爆薬筒から発生したジェットが
本発明の平行飛しょう型偏心防御構造に小さな撃角で入
射した場合でも、図2に示すように、金属製板11、1
3が金属製板面の法線方向には飛しょうせず平行型の偏
心飛しょうをするため、この平行型の偏心飛しょうをす
る金属製板と爆薬筒から発生したジェットが相互干渉を
起こし、その結果ジェットの能力が大幅に減殺されるの
で、防御構造としてのジェット減殺効果を発揮すること
が可能となる。すなわち、爆薬筒から発生したジェット
が防御構造に小さな撃角で入射した場合、従来の防御構
造ではジェットの能力を減殺することは期待できなかっ
たが、本発明の平行飛しょう型偏心防御構造では減殺す
ることができるため、全体として従来の防御構造以上の
ジェット減殺効果を発揮することができる。さらに、各
種車両等に装着された本発明の平行飛しょう型偏心防御
構造が、爆薬筒によってその機能を発揮した時、金属製
板11、13が金属製板面の法線方向には飛しょうせず
平行型の偏心飛しょうをするため、高速で飛しょうする
平行飛しょう型偏心防御構造の金属製板のうち、車両等
の外板に近い側の金属製板13が車両等の外板53に徐
々に接触しながら衝突するので、図3に示すように、外
板がスポール破壊等の被害を受ける可能性はなくなる。
[Function] The jet generated from the explosive cartridge is the parallel flight of the present invention by making the structure of the parallel flight type eccentric protection structure a structure in which energy material is filled between two asymmetric metal plates. As shown in FIG. 2, even when the metal plates 11 and
3 does not fly in the direction of the normal of the metal plate surface but makes a parallel type eccentric flight, so the parallel type eccentric metal plate and the jet generated from the explosive cylinder cause mutual interference. As a result, the ability of the jet is greatly reduced, so that it is possible to exhibit the jet reducing effect as a defense structure. In other words, when the jet generated from the explosive cartridge enters the defense structure at a small angle of attack, the conventional defense structure could not be expected to reduce the ability of the jet, but with the parallel flying eccentric protection structure of the present invention Since it can be attenuated, it is possible to exert a jet attenuating effect more than the conventional defense structure as a whole. Further, when the parallel flying type eccentric protection structure of the present invention mounted on various vehicles and the like exerts its function by the explosive cylinder, the metal plates 11 and 13 fly in the normal direction of the metal plate surface. Among the metal plates of the parallel flying type eccentric protection structure which flies at high speed in order to make a parallel type eccentric flying, the metal plate 13 on the side close to the outer plate of the vehicle etc. is the outer plate of the vehicle etc. Since the collision occurs while gradually contacting the outer surface 53, there is no possibility that the outer plate is damaged by spalling or the like as shown in FIG.

【0008】[0008]

【実施例】図1は、本発明に係る平行飛しょう型偏心防
御構造の実施例を示す。平行飛しょう型偏心防御構造を
構成する金属製板11及び13には、高張力鋼、超高張
力鋼、防弾鋼等の鉄型材料あるいはアルミニウム合金、
チタン合金等の軽金属材料を用いる。金属製板の板厚は
対象とする爆薬筒の口径、ライナ形状等により変わる
が、板厚の薄い側の板厚は2〜5mmの範囲が、また板
厚の厚い側の板厚は4〜10mmの範囲が適当である。
そして、一方の金属製板11の板厚の薄い側と他方の金
属製板13の板厚の厚い側を同じ側にする。エネルギ物
質12は、PBX型の高爆速低銃撃感度爆薬等を用い、
エネルギ物質の厚さは対象とする爆薬筒の口径、ライナ
形状等に応じて、3〜10mmの範囲が適当である。
1 shows an embodiment of a parallel flying type eccentricity prevention structure according to the present invention. The metal plates 11 and 13 constituting the parallel flying type eccentric protection structure include iron-type materials such as high-strength steel, ultra-high-strength steel, and bullet-proof steel or aluminum alloys.
A light metal material such as a titanium alloy is used. The thickness of the metal plate varies depending on the caliber, liner shape, etc. of the target explosive cylinder, but the thickness of the thinner side is in the range of 2 to 5 mm, and the thickness of the thicker side is 4 to 5 mm. A range of 10 mm is appropriate.
Then, the thinner side of one metal plate 11 and the thicker side of the other metal plate 13 are set to the same side. The energy substance 12 uses a PBX-type high explosive low-fire sensitivity explosive or the like,
The thickness of the energy material is suitably in the range of 3 to 10 mm depending on the diameter of the target explosive cylinder, the shape of the liner, and the like.

【0009】なお、本発明の構造の形状及び寸法等は、
装着する車両等の種類、装着する部位、特にその傾斜角
度及び対象とする爆薬筒の種類により適宜設計可能であ
る。
The shape and dimensions of the structure of the present invention are as follows.
The design can be made as appropriate according to the type of the vehicle to be mounted, the site to be mounted, particularly the inclination angle and the type of the target explosive cylinder.

【0010】[0010]

【発明の効果】本発明の平行飛しょう型偏心防御構造
は、厚さが非対称な2枚の金属製板の間にエネルギ物質
を充填した構造であり、従来の防御構造では、爆薬筒か
ら発生したジェットが小さな撃角で防御構造に入射した
場合、ジェットの能力を減殺することは期待できなかっ
たが、本発明の平行飛しょう型偏心防御構造では、爆薬
筒から発生したジェットが小さな撃角で平行飛しょう型
偏心防御構造に入射した場合でも、金属製板が金属製板
面の法線方向には飛しょうせず平行型の偏心飛しょうを
するため、この平行型の偏心飛しょうをする金属製板と
爆薬筒から発生したジェットが相互干渉を起こし、その
結果ジェットの能力が大幅に減殺されるので、防御構造
としてのジェット減殺効果を発揮することが可能とな
る。さらに、各種車両等に装着された本発明の平行飛し
ょう型偏心防御構造が、爆薬筒によってその機能を発揮
した時、金属製板が金属製板面の法線方向には飛しょう
せず平行型の偏心飛しょうをするため、高速で飛しょう
する平行飛しょう型偏心防御構造の金属製板のうち、車
両等の外板に近い側の金属製板が車両等の外板に徐々に
接触しながら衝突するので、車両等の外板がスポール破
壊等の被害を受ける可能性はなくなる。以上述べたよう
に、本発明の平行飛しょう型偏心防御構造は、各種車両
等の外板防護力向上及び平行飛しょう型偏心防御構造が
機能した時、高速で飛しょうする平行飛しょう型偏心防
御構造の金属製板のうち、車両等の外板に近い側の金属
製板が車両等の外板に与える被害を軽減するために利用
価値の高いものである。
The parallel flying type eccentric protection structure of the present invention is a structure in which an energy substance is filled between two asymmetric metal plates. In the conventional protection structure, a jet generated from an explosive cylinder is used. Could not be expected to reduce the jet's ability if it hit the defense structure at a small angle of attack, but with the parallel flying eccentric protection structure of the present invention, the jet generated from the explosive cylinder parallelized at a small angle of attack. Even if it is incident on the flying-type eccentric protection structure, the metal plate does not fly in the normal direction of the metal plate surface but makes a parallel-type eccentric flying. Jets generated from the plate making and the explosive cartridge cause mutual interference, and as a result, the ability of the jet is greatly reduced, so that the jet can be reduced as a defense structure. Furthermore, when the parallel flying type eccentric protection structure of the present invention mounted on various vehicles, etc. exerts its function by the explosive cylinder, the metal plate does not fly in the normal direction of the metal plate surface. Among the metal plates of the parallel flying type eccentric protection structure that fly at high speed to make the mold eccentric flying, the metal plate near the outer plate of the vehicle etc. gradually contacts the outer plate of the vehicle etc. Since the vehicle collides with the vehicle, there is no possibility that the outer panel of the vehicle or the like is damaged by spall. As described above, the parallel flight type eccentricity prevention structure of the present invention is a parallel flight type eccentricity which flies at a high speed when the protection function of the outer plate of various vehicles and the like and the parallel flight type eccentricity protection structure functions. Among the metal plates of the defense structure, the metal plate on the side closer to the outer plate of the vehicle or the like is highly useful in reducing damage to the outer plate of the vehicle or the like.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明に係る平行飛しょう型偏心防御構造を示
す図である。
FIG. 1 is a view showing a parallel flight type eccentricity prevention structure according to the present invention.

【図2】同作用を説明する図である。FIG. 2 is a diagram illustrating the same operation.

【図3】同作用を説明する図である。FIG. 3 is a diagram illustrating the same operation.

【図4】従来の防御構造を示す図である。FIG. 4 is a diagram showing a conventional defense structure.

【図5】同作用を説明する図である。FIG. 5 is a diagram illustrating the same operation.

【図6】同作用を説明する図である。FIG. 6 is a diagram illustrating the same operation.

【図7】同作用を説明する図である。FIG. 7 is a diagram illustrating the same operation.

【符号の説明】[Explanation of symbols]

11 金属製板 12 エネルギ物質 13 金属製板 21 金属製平板 22 エネルギ物質 23 金属製平板 31 ジェット 32 能力を失ったジェット 53 外板 54 破壊片 55 破壊片 REFERENCE SIGNS LIST 11 metal plate 12 energetic material 13 metal plate 21 metal flat plate 22 energetic material 23 metal flat plate 31 jet 32 jet which lost capability 53 outer plate 54 destruction piece 55 destruction piece

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 2枚の金属製板(11),(13)の間
に爆薬等爆発性のエネルギ物質(12)を充填した構造
を有する反応性防御構造において、前記2枚の金属製板
(11),(13)は、その一端面の側から他端面の側
に向けて、その厚さが傾斜状に変化した形状であり且つ
一方の金属製板(11)と他方の金属製板(13)とで
厚さの変化の方向が反対方向とされたことを特徴とする
平行飛しょう型偏心反応性防御構造。
1. A reactive defense structure having a structure in which an explosive or other explosive energy substance (12) is filled between two metal plates (11) and (13). (11) and (13) have a shape in which the thickness changes from one end surface side to the other end surface side in an inclined manner, and one metal plate (11) and the other metal plate (13) The parallel flying type eccentric reactive protection structure, characterized in that the thickness changes in opposite directions.
JP5463697A 1997-03-10 1997-03-10 Parallel flying eccentric reactive defense structure Expired - Lifetime JP2939532B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5463697A JP2939532B2 (en) 1997-03-10 1997-03-10 Parallel flying eccentric reactive defense structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5463697A JP2939532B2 (en) 1997-03-10 1997-03-10 Parallel flying eccentric reactive defense structure

Publications (2)

Publication Number Publication Date
JPH10253296A JPH10253296A (en) 1998-09-25
JP2939532B2 true JP2939532B2 (en) 1999-08-25

Family

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JP5631061B2 (en) * 2010-06-03 2014-11-26 オート・メラーラ ソシエタ ペル アテオニOto Melara S.P.A. Active bulletproof system
IL237991A0 (en) * 2015-02-26 2017-12-31 Cohen David Device
IL239523A0 (en) 2015-02-26 2015-11-30 Cohen David Armor
KR20180093896A (en) * 2015-10-22 2018-08-22 데이비드 코헨 Reaction gloves

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