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CN106854718A - Structural material containing energy and its preparation method and application - Google Patents

Structural material containing energy and its preparation method and application Download PDF

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CN106854718A
CN106854718A CN201611095947.0A CN201611095947A CN106854718A CN 106854718 A CN106854718 A CN 106854718A CN 201611095947 A CN201611095947 A CN 201611095947A CN 106854718 A CN106854718 A CN 106854718A
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structural material
energetic
powder
energetic structural
aluminum
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CN106854718B (en
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阳世清
李顺
崔伟峰
白书欣
黄彩敏
林庆章
李俊杰
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National University of Defense Technology
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/05Mixtures of metal powder with non-metallic powder
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C16/00Alloys based on zirconium
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    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/003Alloys based on aluminium containing at least 2.6% of one or more of the elements: tin, lead, antimony, bismuth, cadmium, and titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/02Alloys based on vanadium, niobium, or tantalum
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/04Alloys based on tungsten or molybdenum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/001Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
    • C22C32/0015Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
    • C22C32/0026Matrix based on Ni, Co, Cr or alloys thereof
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/001Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
    • C22C32/0015Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
    • C22C32/0031Matrix based on refractory metals, W, Mo, Nb, Hf, Ta, Zr, Ti, V or alloys thereof
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/001Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
    • C22C32/0015Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
    • C22C32/0036Matrix based on Al, Mg, Be or alloys thereof

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Abstract

The invention discloses one kind containing can structural material, including following mass fraction component:10%~60% aluminum or aluminum alloy, 35% ~ 89.5% high desnity metal and 0.5%~5.0% metal oxide;Wherein, aluminum or aluminum alloy is successive substrates phase, and high desnity metal particle and metal oxide particle are evenly distributed in the successive substrates phase.The structural material containing energy has the advantages that high intensity, reaction latent heat and good impact-response characteristic high.

Description

含能结构材料及其制备方法和应用Energetic structural materials and their preparation methods and applications

技术领域technical field

本发明属于新材料技术领域,尤其涉及一种含能结构材料及其制备方法和应用。The invention belongs to the technical field of new materials, and in particular relates to an energetic structural material and its preparation method and application.

背景技术Background technique

高效毁伤是远程精确打击的根本目的,目前武器的毁伤主要依靠以传统弹药为核心的战斗部,因此发展高毁伤弹药是提升远程精确打击武器的核心任务之一。传统战斗部主要由金属壳体、炸药以及相应的结构部件等组成,炸药是战斗部毁伤目标的能源,为提高战斗部的毁伤威力,一般采用提高炸药装填量和单位质量炸药能量的方式来实现,由于受到使用条件以及材料水平的限制,炸药的装填量存在极限,而炸药能量密度的提高也十分困难。此外,炸药能量释放与转换过程中毁伤元所获得的能量是炸药全部能量的一小部分,炸药装填量或能量密度的稍许提高并不一定能带来对目标毁伤效果的大幅度提升。因此,战斗部毁伤效能的提高需要拓展新的技术途径。High-efficiency damage is the fundamental purpose of long-range precision strikes. At present, the damage of weapons mainly depends on the warhead with traditional ammunition as the core. Therefore, the development of high-damage ammunition is one of the core tasks for upgrading long-range precision strike weapons. Traditional warheads are mainly composed of metal shells, explosives, and corresponding structural components. Explosives are the energy for warheads to damage targets. In order to improve the damage power of warheads, it is generally achieved by increasing the explosive loading and the explosive energy per unit mass. , due to the limitations of the conditions of use and the level of materials, there is a limit to the amount of explosives loaded, and it is very difficult to increase the energy density of explosives. In addition, the energy obtained by the damage element during the energy release and conversion process of the explosive is a small part of the total energy of the explosive, and a slight increase in the charge or energy density of the explosive does not necessarily bring about a large increase in the damage effect on the target. Therefore, the improvement of warhead damage efficiency needs to expand new technical approaches.

常见条件下稳定性高,但高速撞击可引发组分间放热反应的含能材料常称为反应材料(Reactive Materials,RMs),有高力学性能的反应材料称为反应结构材料或含能结构材料。采用含能结构材料制成战斗部的破片、药型罩以及壳体结构等部件,在炸药爆炸驱动下形成毁伤元,通过爆炸加载、高速冲击等方式给毁伤元施加反应所需的临界能量,促使其自身组元之间或者组元与环境之间发生反应二次释能,可实现对目标的引燃、引爆毁伤。含能结构材料在弹药中的应用是提高现有弹药性能的一种新途径(徐松林,阳世清,张炜等,PTFE/Al反应材料的力学性能研究。高压物理学报,2009,23(5): 384~388. 杨益,郑颖,王坤, 高密度活性材料及其毁伤效应进展研究,兵器材料科学与工程. 2013, 36(4): 81-85。宋磊,李宝锋,陈皓,美海军演示用“高密度活性材料”提高战斗部爆炸威力,装备参考.2011,49:32-33.)。Energetic materials with high stability under common conditions, but high-speed impacts can trigger exothermic reactions between components are often called reactive materials (Reactive Materials, RMs), and reactive materials with high mechanical properties are called reactive structural materials or energetic structures. Material. The warhead fragments, drug-type cover, shell structure and other components are made of energetic structural materials, and the damage element is formed under the driving of the explosive explosion, and the critical energy required for the reaction is applied to the damage element through explosive loading, high-speed impact, etc. Prompting the reaction between its own components or between the components and the environment to release energy twice, can achieve ignition and detonation damage to the target. The application of energetic structural materials in ammunition is a new way to improve the performance of existing ammunition (Xu Songlin, Yang Shiqing, Zhang Wei, etc., Research on the mechanical properties of PTFE/Al reactive materials. Journal of High Pressure Physics, 2009, 23(5 ): 384~388. Yang Yi, Zheng Ying, Wang Kun, Research progress on high-density active materials and their damage effects, Weapon Materials Science and Engineering. 2013, 36(4): 81-85. Song Lei, Li Baofeng, Chen Hao , The U.S. Navy demonstrated the use of "high-density active materials" to increase the explosive power of warheads, Equipment Reference. 2011, 49: 32-33.).

含能结构材料在使用时承受的外力主要有炸药驱动时的压应力、飞行卸载时的拉应力、冲击减速时的压应力和穿透目标卸载时的拉应力,因此含能结构材料一般需要具有以下特征:(1)具有足够高的强度,一方面确保材料可以作为结构件如战斗部壳体使用,另一方面确保在爆炸驱动和侵彻目标过程中的完整性;(2)具有合适的反应潜热和潜热释放能力,保证高速撞击时的能量释放特性;(3)适中的密度,确保材料必备的侵彻性能。The external forces that energetic structural materials bear during use mainly include compressive stress when explosives are driven, tensile stress when unloading in flight, compressive stress when impact decelerates, and tensile stress when penetrating the target and unloading. Therefore, energetic structural materials generally need to have The following characteristics: (1) have high enough strength, on the one hand, to ensure that the material can be used as a structural part such as a warhead shell, and on the other hand, ensure the integrity during the explosive drive and penetration of the target; (2) have a suitable Reaction latent heat and latent heat release ability ensure the energy release characteristics during high-speed impact; (3) Moderate density ensures the necessary penetration performance of the material.

为了获取满足上述要求的含能结构材料,申请号为201510733993.8的中国专利提出了一种含能材料的制备方法,该方法利用模压、烧结成型的方法制备含能结构材料,采用该方法得到的Al/W/PTFE含能材料相较于传统的Al/PTFE(Al:26.4wt%;PTFE:73.6wt%)含能材料在抗压强度和密度方面均有大幅提高,而含能材料的反应阈值也有所提高。但该类材料拉伸强度较低,一般不超过30MPa。In order to obtain energetic structural materials that meet the above requirements, the Chinese patent application number 201510733993.8 proposes a method for preparing energetic materials. This method uses molding and sintering methods to prepare energetic structural materials. The Al obtained by this method Compared with traditional Al/PTFE (Al: 26.4wt%; PTFE: 73.6wt%) energetic materials, /W/PTFE energetic materials have greatly improved compressive strength and density, and the reaction threshold of energetic materials also improved. However, the tensile strength of this type of material is low, generally not exceeding 30MPa.

专利号为201410176443.6的中国专利提出了一种含能结构材料,该材料由Al粉、KClO3粉和W粉三种粉末混合压制而成,材料在爆炸加速过程中足够钝感不发生反应,具有较大的侵彻威力,并能发生化学反应释放能量,增加毁伤目标能力。但该材料采用混粉后冷压成型,材料强度主要靠粉末之间的机械啮合力,强度较低。The Chinese patent No. 201410176443.6 proposes an energetic structural material, which is made by mixing and pressing Al powder, KClO 3 powder and W powder. The material is sufficiently insensitive and does not react during the acceleration of the explosion, and has Greater penetrating power, and can produce chemical reactions to release energy, increasing the ability to damage targets. However, the material is formed by cold pressing after powder mixing, and the strength of the material mainly depends on the mechanical meshing force between the powders, and the strength is relatively low.

申请号为201610044485.3的中国专利提出了一种含能结构材料破片,该材料由纳米铝粉、过渡金属氧化物、氧化剂、二茂铁、猛炸药和混合粘结剂混合后冷压成型得到,利用该材料制备的含能破片能量密度高、安全性能好、容易引发且纵火能力强,在炸药驱动时不会立即反应,但侵彻过程中可以发生强烈的化学反应并放出极高的热量,且能生成高温炽热的、具有流动性的反应产物。该材料的强度主要由粘结剂来决定,强度仍然较低。The Chinese patent application number 201610044485.3 proposes a fragment of energetic structural material, which is obtained by cold pressing after mixing nano-aluminum powder, transition metal oxide, oxidizer, ferrocene, high explosive and mixed binder. The energetic fragments prepared by this material have high energy density, good safety performance, easy initiation and strong arson ability, and will not react immediately when the explosive is driven, but a strong chemical reaction can occur during the penetration process and release extremely high heat, and It can generate hot, fluid reaction products at high temperature. The strength of the material is mainly determined by the binder, and the strength is still low.

专利号为201110440556.9的中国专利和申请号为201510606975.3的中国专利提出了二种制备钨锆合金含能结构材料的方法,利用该方法制备出的材料具有相对较好的力学性能,但该材料主要靠锆元素与环境中的氧气作用释放出能量,潜热释放能力较差,因此对燃油的引燃和炸药的引爆效果一般,需要在特定的条件下才有可能。The Chinese patent with the patent number 201110440556.9 and the Chinese patent with the application number 201510606975.3 proposed two methods for preparing tungsten-zirconium alloy energetic structural materials. The materials prepared by this method have relatively good mechanical properties, but the materials mainly rely on Zirconium reacts with oxygen in the environment to release energy, and its ability to release latent heat is poor. Therefore, the ignition of fuel oil and the detonation of explosives are generally effective, and it is possible only under specific conditions.

由此可见,目前公开报道含能结构材料的综合性能距离实际需求还具有一定的距离。It can be seen that the current public reports on the comprehensive performance of energetic structural materials still have a certain distance from the actual demand.

发明内容Contents of the invention

本发明要解决的技术问题是克服现有技术的不足,提供一种高强度、高反应潜热和良好的冲击反应特性的含能结构材料,还相应提供一种材料组分间无不良化学反应的上述含能结构材料的制备方法,另外,还提供该含能结构材料在战斗部中的应用。The technical problem to be solved by the present invention is to overcome the deficiencies of the prior art, to provide an energetic structural material with high strength, high latent heat of reaction and good impact response characteristics, and to provide a material without adverse chemical reactions between components. The preparation method of the above-mentioned energetic structural material also provides the application of the energetic structural material in warheads.

为解决上述技术问题,本发明采用以下技术方案:In order to solve the problems of the technologies described above, the present invention adopts the following technical solutions:

种含能结构材料,包括以下质量分数的组分:An energetic structural material, comprising the following components in mass fraction:

铝或铝合金 10%~60%Aluminum or aluminum alloy 10%~60%

高密度金属   35%~89.5%,和High Density Metal 35%~89.5%, and

金属氧化物 0.5%~5.0%;Metal oxide 0.5%~5.0%;

其中,铝或铝合金为连续基体相,高密度金属和金属氧化物均匀分布在所述连续基体相中。Wherein, aluminum or aluminum alloy is a continuous matrix phase, and high-density metals and metal oxides are evenly distributed in the continuous matrix phase.

上述的含能结构材料,优选的,所述高密度金属为Ni、W、Ta、Hf、Ti和Zr中的一种或几种。In the aforementioned energetic structural material, preferably, the high-density metal is one or more of Ni, W, Ta, Hf, Ti and Zr.

上述的含能结构材料,优选的,所述金属氧化物为Fe2O3、Fe3O4、PbO、CuO、MnO2、WO3、Bi2O3和MoO3中的一种或几种。For the aforementioned energetic structural material, preferably, the metal oxide is one or more of Fe 2 O 3 , Fe 3 O 4 , PbO, CuO, MnO 2 , WO 3 , Bi 2 O 3 and MoO 3 .

上述的含能结构材料,优选的,所述高密度金属为Ni、W或Ta中的一种或几种。In the aforementioned energetic structural material, preferably, the high-density metal is one or more of Ni, W or Ta.

上述的含能结构材料,优选的,所述金属氧化物为WO3或MoO3For the aforementioned energetic structural material, preferably, the metal oxide is WO 3 or MoO 3 .

作为一个总的发明构思,本发明还提供一种上述的含能结构材料的制备方法,包括以下步骤:As a general inventive concept, the present invention also provides a method for preparing the aforementioned energetic structural material, comprising the following steps:

(1)混料:根据含能结构材料的配方,将铝粉、高密度金属粉末、和金属氧化物粉末进行混合,得到混合粉末;(1) Mixing: According to the formula of energetic structural materials, aluminum powder, high-density metal powder, and metal oxide powder are mixed to obtain mixed powder;

(2)预成型:对混合粉末进行冷压,得到预成型体;(2) Preforming: Cold pressing the mixed powder to obtain a preform;

(3)烧结:对预成型体进行烧结,得到块状含能结构材料。(3) Sintering: The preform is sintered to obtain bulk energetic structural materials.

上述的含能结构材料的制备方法,优选的,所述步骤(1)中,所述混合粉末的粒度为0.1μm~50μm;所述步骤(2)中,所述冷压压力为100MPa~600MPa,时间为1min~10min。In the preparation method of the above energetic structural material, preferably, in the step (1), the particle size of the mixed powder is 0.1 μm to 50 μm; in the step (2), the cold pressing pressure is 100 MPa to 600 MPa , the time is 1min to 10min.

上述的含能结构材料的制备方法,优选的,所述步骤(3)中,所述烧结包括常压烧结和热压烧结。In the above method for preparing energetic structural materials, preferably, in the step (3), the sintering includes atmospheric pressure sintering and hot-press sintering.

上述的含能结构材料的制备方法,优选的,所述步骤(3)中,所述烧结的温度为300℃~600℃,保温时间为0.5h~3h;所述热压烧结的压力为100MPa~600MPa。In the preparation method of the above-mentioned energetic structural material, preferably, in the step (3), the sintering temperature is 300°C-600°C, and the holding time is 0.5h-3h; the pressure of the hot-press sintering is 100MPa ~600MPa.

作为一个总的发明构思,本发明还提供一种上述的含能结构材料或上述的含能结构材料的制备方法所制备的含能结构材料在战斗部中的应用。As a general inventive concept, the present invention also provides an application of the above-mentioned energetic structural material or the energetic structural material prepared by the above-mentioned method for preparing the energetic structural material in warheads.

与现有技术相比,本发明的优点在于:Compared with the prior art, the present invention has the advantages of:

1、本发明的含能结构材料,与现有的含能结构材料相比,是一种金属型的含能结构材料,材料中金属组分含量在95%以上;材料中铝或铝合金为连续基体相,其它高密度金属颗粒及金属氧化物颗粒均匀分布在铝基体相中,具有一定的强化作用,保证材料具有高的强度。为了使铝在成形过程中形成连续基体相从而使该含能结构材料具有高的强度,材料中低密度Al的质量含量在10%~60%之间;另外,添加了0.5~5.0wt%的金属氧化物,该范围内的金属氧化物含量对材料强度影响较小,可以在不明显改变材料强度的情况下,改变材料的冲击反应特性,使得该含能结构材料具有良好的冲击反应特性。优选地,通过调整材料的组分特别是重金属元素W、Ta和Hf的含量,可以在一定范围内改变材料的密度,满足不同应用场合的需要。1. Compared with the existing energetic structural materials, the energetic structural material of the present invention is a metal-type energetic structural material, and the metal component content in the material is more than 95%; the aluminum or aluminum alloy in the material is The continuous matrix phase, other high-density metal particles and metal oxide particles are evenly distributed in the aluminum matrix phase, which has a certain strengthening effect and ensures the high strength of the material. In order to make aluminum form a continuous matrix phase during the forming process so that the energetic structural material has high strength, the mass content of low-density Al in the material is between 10% and 60%; in addition, 0.5-5.0wt% Al Metal oxides, the metal oxide content within this range has little effect on the strength of the material, and can change the impact response characteristics of the material without significantly changing the strength of the material, so that the energetic structural material has good impact response characteristics. Preferably, by adjusting the composition of the material, especially the content of heavy metal elements W, Ta and Hf, the density of the material can be changed within a certain range to meet the needs of different applications.

2、本发明的含能结构材料,由于主要组分均为具有高燃烧热值的元素,因而具有很高的反应潜热。在冲击载荷的作用下,除了发生材料组分之间的化学反应,如Al和Ni反应生成AlNi、Al3Ni2和Al3Ni,Al和CuO反应生成Cu和Al2O3等之外,如果环境中有氧气,还会发生材料组分与氧气之间的化学反应,如Al和O2反应生成Al2O3、Zr和O2反应生成ZrO2等,在这些过程中释放出大量的热量。2. The energetic structural material of the present invention has high latent heat of reaction because the main components are all elements with high combustion calorific value. Under the action of impact load, in addition to the chemical reaction between material components, such as the reaction of Al and Ni to form AlNi, Al 3 Ni 2 and Al 3 Ni, the reaction of Al and CuO to form Cu and Al 2 O 3 , etc., If there is oxygen in the environment, chemical reactions between material components and oxygen will also occur, such as the reaction of Al and O 2 to generate Al 2 O 3 , the reaction of Zr and O 2 to generate ZrO 2 , etc., during which a large amount of heat.

3、试验表明,铝或铝合金的含量、成形压力、成形度和保温时间都对含能结构材料的强度有较大的影响。本发明的含能结构材料的制备方法,通过严格控制成形工艺,确保了成形后材料具有尽可能高的强度,且材料中各组分之间没有不良化学反应产生,无其它相生成。3. The test shows that the content of aluminum or aluminum alloy, forming pressure, forming degree and holding time all have a great influence on the strength of energetic structural materials. The preparation method of the energy-containing structural material of the present invention ensures that the formed material has as high strength as possible through strict control of the forming process, and there is no adverse chemical reaction between components in the material, and no other phases are formed.

附图说明Description of drawings

图1为本发明实施例1的Ni-Al含能结构材料的XRD图谱。Fig. 1 is the XRD spectrum of the Ni-Al energetic structural material of Example 1 of the present invention.

图2为本发明实施例1的Ni-Al含能结构材料的断口SEM图。Fig. 2 is a fracture SEM image of the Ni-Al energetic structural material of Example 1 of the present invention.

图3为本发明实施例1的Ni-Al含能结构材料的拉伸曲线。Fig. 3 is a tensile curve of the Ni-Al energetic structural material of Example 1 of the present invention.

图4为本发明实施例1的Ni-Al含能结构材料在约900m/s撞击速度下的冲击反应照片。Fig. 4 is a photograph of the impact reaction of the Ni-Al energetic structural material of Example 1 of the present invention at an impact velocity of about 900 m/s.

图5为对比例1的未添加金属氧化物Ni-Al含能结构材料在约900m/s撞击速度下的冲击反应照片。Fig. 5 is a photograph of the impact reaction of the Ni-Al energetic structural material without adding metal oxides in Comparative Example 1 at an impact velocity of about 900 m/s.

具体实施方式detailed description

以下结合说明书附图和具体优选的实施例对本发明作进一步描述,但并不因此而限制本发明的保护范围。The present invention will be further described below in conjunction with the accompanying drawings and specific preferred embodiments, but the protection scope of the present invention is not limited thereby.

实施例1:Example 1:

一种本发明的Ni-Al含能结构材料,包括Al、Ni和金属氧化物MoO3,Al、Ni和MoO3的质量比为48∶50∶2,其中,铝为连续基体相,Ni和MoO3均匀分布在铝基体相中。A Ni-Al energy-containing structural material of the present invention, comprising Al, Ni and metal oxide MoO 3 , the mass ratio of Al, Ni and MoO 3 is 48:50:2, wherein aluminum is the continuous matrix phase, Ni and MoO3 is uniformly distributed in the Al matrix phase.

一种上述本实施例的Ni-Al含能结构材料的制备方法,包括以下步骤:A preparation method of the Ni-Al energetic structural material of the above-mentioned present embodiment, comprising the following steps:

(1)混料:按照Al粉、Ni粉和MO3粉质量比为48∶50∶2的比例分别称取Al粉240g、Ni粉250g和MoO3粉10g,将称好的各种粉末在球磨机中混合均匀,所得混合粉末的粒径为0.5μm~20μm;(1) Mixing: Weigh 240g of Al powder, 250g of Ni powder and 10g of MoO 3 powder according to the mass ratio of Al powder, Ni powder and MO 3 powder in the ratio of 48:50:2. Mix evenly in a ball mill, and the particle size of the obtained mixed powder is 0.5μm~20μm;

(2)预成形:称取混合粉末200g,均匀铺设在凹模的底层,然后通过凸膜对铺设的粉末施加300MPa的压力并保压3min,卸压;(2) Preforming: Weigh 200g of the mixed powder, spread it evenly on the bottom of the die, and then apply a pressure of 300MPa to the laid powder through the convex film and keep the pressure for 3min, then release the pressure;

(3)烧结:将上述模具及模内的预成形体按5℃/min升温速率升至380℃,恒温90min后再施加400MPa的压力并恒压5min,脱模,得到Ni-Al含能结构材料。(3) Sintering: raise the temperature of the above mold and the preform in the mold to 380°C at a rate of 5°C/min, keep the temperature constant for 90 minutes, then apply a pressure of 400MPa and keep the pressure constant for 5 minutes, and demould to obtain a Ni-Al energetic structure Material.

图1为本实施例的Ni-Al含能结构材料的XRD图谱,由图可知,该Ni-Al含能结构材料的主要由金属Ni和Al组成,没有Ni-Al间金属间化合物相的存在。另外由于材料中MoO3的含量较少,因此也没有观察到MoO3衍射峰的存在。Figure 1 is the XRD spectrum of the Ni-Al energetic structural material of this example, as can be seen from the figure, the Ni-Al energetic structural material is mainly composed of metal Ni and Al, and there is no Ni-Al intermetallic compound phase . In addition, due to the low content of MoO 3 in the material, no diffraction peak of MoO 3 was observed.

图2为本实施例的Ni-Al含能结构材料的断口SEM图,可以看出,块状的连续基体相为Al, Ni颗粒及金属氧化物MoO3颗粒均匀分布在铝基体相中。Figure 2 is a fracture SEM image of the Ni-Al energetic structural material of this embodiment, it can be seen that the massive continuous matrix phase is Al, Ni particles and metal oxide MoO3 particles are evenly distributed in the aluminum matrix phase.

图3为本实施例的Ni-Al含能结构材料的拉伸曲线,由图可知,该Ni-Al含能结构材料的拉伸强度约为230MPa,远大于PTFE/Al类含能结构材料(不超过30MPa)。Fig. 3 is the tensile curve of the Ni-Al energetic structural material of this embodiment, as can be seen from the figure, the tensile strength of the Ni-Al energetic structural material is about 230MPa, which is much greater than that of the PTFE/Al energetic structural material ( not exceeding 30MPa).

另外,经测算,该Ni-Al含能结构材料的密度约为4.10g/cm3,高燃烧热值元素Al和Ni的质量含量约为96%。In addition, it is calculated that the density of the Ni-Al energetic structural material is about 4.10g/cm 3 , and the mass content of high combustion calorific value elements Al and Ni is about 96%.

对比例1:Comparative example 1:

本对比例的Ni-Al含能结构材料制备方法与实施例1相同,其不同点仅在于:材料中不包括金属氧化物MoO3The preparation method of the Ni—Al energetic structural material in this comparative example is the same as that in Example 1, the only difference being that the material does not include metal oxide MoO 3 .

图4为本发明实施例1的Ni-Al含能结构材料在约900m/s撞击速度下的冲击反应照片;图5为对比例1的未添加金属氧化物Ni-Al含能结构材料在约900m/s撞击速度下的冲击反应照片。对照图4和图5可知,实施例1中添加金属氧化物MoO3的Ni-Al含能结构材料在900m/s撞击速度下具有很大的反应火光面积,而对比例1中未添加金属氧化物MoO3的Ni-Al含能结构材料在相同撞击速度下反应火光面积非常小,显示出本发明实施例1的Ni-Al含能结构材料具有良好的冲击反应特性。Fig. 4 is the photo of the impact reaction of the Ni-Al energetic structural material of Example 1 of the present invention at an impact velocity of about 900m/s; Fig. 5 is the Ni-Al energetic structural material of Comparative Example 1 at about 900m/s Shock reaction photos at 900m/s impact velocity. Comparing Figures 4 and 5, it can be seen that the Ni-Al energetic structural material with metal oxide MoO3 added in Example 1 has a large reaction flare area at an impact velocity of 900m/s, while no metal oxide is added in Comparative Example 1. The Ni-Al energetic structural material of MoO 3 has a very small reaction flare area at the same impact velocity, which shows that the Ni-Al energetic structural material of Example 1 of the present invention has good impact response characteristics.

实施例2:Example 2:

一种本发明的Ni-Al-W含能结构材料,包括Al、高密度金属Ni和W,以及金属氧化物MoO3、WO3,Al、Ni、W、MoO3和WO3的质量比为17∶19∶60∶2∶2,其中,铝为连续基体相,Ni、W、MoO3和WO3均匀分布在铝基体相中。A Ni-Al-W energetic structural material of the present invention, including Al, high-density metal Ni and W, and metal oxides MoO 3 , WO 3 , the mass ratio of Al, Ni, W, MoO 3 and WO 3 is 17:19:60:2:2, wherein aluminum is a continuous matrix phase, and Ni, W, MoO 3 and WO 3 are evenly distributed in the aluminum matrix phase.

(1)混料:按照Al粉、Ni粉、W粉、MoO3和WO3粉质量比为17∶19∶60∶2∶2的比例分别称取Al粉85g、Ni粉95g、W粉300g、MO3粉10g和WO3粉10g,将称好的各种粉末在球磨机中混合均匀,所得混合粉末的粒径为0.5μm ~20μm;;(1) Mixing: Weigh 85g of Al powder, 95g of Ni powder and 300g of W powder according to the mass ratio of Al powder, Ni powder, W powder, MoO 3 and WO 3 powder in the ratio of 17:19:60:2:2 10g of MO 3 powder and 10g of WO 3 powder, mix the weighed powders uniformly in a ball mill, and the particle size of the obtained mixed powder is 0.5 μm ~ 20 μm;

(2)预成型:称取混合粉末200g,均匀铺设在凹模的底层,然后通过凸膜对铺设的粉末施加300MPa的压力并保压3min,卸压;(2) Preforming: Weigh 200g of the mixed powder and spread it evenly on the bottom of the die, then apply a pressure of 300MPa to the laid powder through the convex film and keep the pressure for 3min, then release the pressure;

(3)烧结:将上述模具及模内的预成型体按5℃/min升温速率升至400℃,恒温90min后再施加400MPa的压力并恒压5min,脱模,得到Ni-Al-W含能结构材料。(3) Sintering: raise the above-mentioned mold and the preform in the mold to 400°C at a rate of 5°C/min, keep the temperature constant for 90min, then apply a pressure of 400MPa and keep the pressure constant for 5min, and demould to obtain Ni-Al-W containing capable structural materials.

所述含能结构材料中高燃烧热值元素Al和Ni的质量含量约为37%,密度约为8.0g/cm3,拉伸强度约为210MPa。The mass content of high combustion heat value elements Al and Ni in the energetic structural material is about 37%, the density is about 8.0g/cm 3 , and the tensile strength is about 210MPa.

实施例3:Example 3:

一种本发明的Al-W-Ta含能结构材料,包括Al、高密度金属W和Ta,以及金属氧化物WO3,Al、W、Ta和WO3的质量比为20∶34∶43∶3,其中,铝为连续基体相, W、Ta和WO3均匀分布在铝基体相中。An Al-W-Ta energetic structural material of the present invention, comprising Al, high-density metal W and Ta, and metal oxide WO 3 , the mass ratio of Al, W, Ta and WO 3 is 20:34:43: 3. Among them, aluminum is the continuous matrix phase, and W, Ta and WO 3 are evenly distributed in the aluminum matrix phase.

(1)混料:按照Al粉、W粉、Ta粉和WO3粉质量比为20∶34∶43∶3的比例分别称取Al粉100g、W粉170g、Ta粉215g和WO3粉15g,将称好的各种粉末在球磨机中混合均匀,所得混合粉末的粒径为0.5μm ~50μm;(1) Mixing: Weigh 100g of Al powder, 170g of W powder, 215g of Ta powder and 15g of WO 3 powder according to the mass ratio of Al powder, W powder, Ta powder and WO 3 powder in the ratio of 20:34:43:3 , mix the weighed various powders uniformly in a ball mill, and the particle size of the obtained mixed powder is 0.5 μm ~ 50 μm;

(2)预成型:称取混合粉末200g,均匀铺设在凹模的底层,然后通过凸膜对铺设的粉末施加400MPa的压力并保压3min,卸压;(2) Preforming: Weigh 200g of the mixed powder and spread it evenly on the bottom of the die, then apply a pressure of 400MPa to the laid powder through the convex film and keep the pressure for 3min, then release the pressure;

(3)烧结:将上述模具及模内的预成型体按5℃/min升温速率升至480℃,恒温90min后再施加500MPa的压力并恒压5min,脱模,得到Al-W-Ta含能结构材料。(3) Sintering: raise the temperature of the above mold and the preform in the mold to 480°C at a rate of 5°C/min, keep the temperature constant for 90 minutes, then apply a pressure of 500 MPa and keep the pressure constant for 5 minutes, and demold to obtain Al-W-Ta containing capable structural materials.

所述含能结构材料中高燃烧热值元素Al和Ta的质量含量约为63%,材料的密度约为8.05g/cm3,拉伸强度约为280MPa。The mass content of high combustion heat value elements Al and Ta in the energetic structural material is about 63%, the density of the material is about 8.05g/cm 3 , and the tensile strength is about 280MPa.

实施例4:Example 4:

一种本发明的Al-Ni-Ta-Zr含能结构材料,包括Al、高密度金属Ni、Ta和Zr,以及金属氧化物WO3,Al、Ni、Ta、Zr和WO3的质量比为32∶14∶43∶10∶1,其中,铝为连续基体相,Ni、Ta、Zr和WO3均匀分布在铝基体相中。A kind of Al-Ni-Ta-Zr energetic structural material of the present invention, comprises Al, high-density metal Ni, Ta and Zr, and metal oxide WO 3 , the mass ratio of Al, Ni, Ta, Zr and WO 3 is 32:14:43:10:1, wherein aluminum is a continuous matrix phase, and Ni, Ta, Zr and WO 3 are uniformly distributed in the aluminum matrix phase.

(1)混料:按照Al粉、Ni粉、Ta粉、Zr粉和WO3粉质量比为32∶14∶43∶10∶1的比例分别称取Al粉160g、Ni粉70g、Ta粉215g、Zr粉50g和WO3粉5g,将称好的各种粉末在球磨机中混合均匀,所得混合粉末的粒径为0.5μm ~50μm;(1) Mixing: Weigh 160g of Al powder, 70g of Ni powder and 215g of Ta powder according to the mass ratio of Al powder, Ni powder, Ta powder, Zr powder and WO 3 powder in the ratio of 32:14:43:10:1 , Zr powder 50g and WO 3 powder 5g, mix the various powders that have been weighed evenly in a ball mill, and the particle size of the resulting mixed powder is 0.5 μm ~ 50 μm;

(2)预成型:称取混合粉末200g,均匀铺设在凹模的底层,然后通过凸膜对铺设的粉末施加400MPa的压力并保压3min,卸压;(2) Preforming: Weigh 200g of the mixed powder and spread it evenly on the bottom of the die, then apply a pressure of 400MPa to the laid powder through the convex film and keep the pressure for 3min, then release the pressure;

(3)烧结:将上述模具及模内的预成型体按5℃/min升温速率升至400℃,恒温90min后再施加500MPa的压力并恒压5min,脱模,得到Al-Ni-Ta-Zr含能结构材料。(3) Sintering: raise the temperature of the above mold and the preform in the mold to 400°C at a rate of 5°C/min, keep the temperature constant for 90min, then apply a pressure of 500MPa and keep the pressure constant for 5min, demould, and obtain Al-Ni-Ta- Zr energetic structural material.

所述含能结构材料中高燃烧热值元素Al、Ni、Ta和Zr的质量含量约为99%,材料的密度约为5.35g/cm3,拉伸强度约为200MPa。The mass content of high combustion heat value elements Al, Ni, Ta and Zr in the energetic structural material is about 99%, the density of the material is about 5.35g/cm 3 , and the tensile strength is about 200MPa.

以上所述仅是本发明的优选实施方式,本发明的保护范围并不仅局限于上述实施例。凡属于本发明思路下的技术方案均属于本发明的保护范围。应该指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下的改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above descriptions are only preferred implementations of the present invention, and the scope of protection of the present invention is not limited to the above examples. All technical solutions under the idea of the present invention belong to the protection scope of the present invention. It should be pointed out that for those skilled in the art, improvements and modifications without departing from the principle of the present invention should also be regarded as the protection scope of the present invention.

Claims (10)

1.一种含能结构材料,其特征在于,包括以下质量分数的组分:1. An energetic structural material, characterized in that it comprises the following components in mass fraction: 铝或铝合金 10%~60%Aluminum or aluminum alloy 10%~60% 高密度金属   35%~89.5%,和High Density Metal 35%~89.5%, and 金属氧化物 0.5%~5.0%;Metal oxide 0.5%~5.0%; 其中,铝或铝合金为连续基体相,高密度金属和金属氧化物均匀分布在所述连续基体相中。Wherein, aluminum or aluminum alloy is a continuous matrix phase, and high-density metals and metal oxides are evenly distributed in the continuous matrix phase. 2.根据权利要求1所述的含能结构材料,其特征在于,所述高密度金属为Ni、W、Ta、Hf、Ti和Zr中的一种或几种。2. The energetic structural material according to claim 1, wherein the high-density metal is one or more of Ni, W, Ta, Hf, Ti and Zr. 3.根据权利要求2所述的含能结构材料,其特征在于,所述金属氧化物为Fe2O3、Fe3O4、PbO、CuO、MnO2、WO3、Bi2O3和MoO3中的一种或几种。3. The energetic structural material according to claim 2, wherein the metal oxides are Fe 2 O 3 , Fe 3 O 4 , PbO, CuO, MnO 2 , WO 3 , Bi 2 O 3 and MoO One or more of 3 . 4.根据权利要求3所述的含能结构材料,其特征在于,所述高密度金属为Ni、W或Ta中的一种或几种。4. The energetic structural material according to claim 3, wherein the high-density metal is one or more of Ni, W or Ta. 5.根据权利要求4所述的含能结构材料,其特征在于,所述金属氧化物为WO3或MoO35 . The energetic structural material according to claim 4 , wherein the metal oxide is WO 3 or MoO 3 . 6.一种如权利要求1~5任一项所述的含能结构材料的制备方法,包括以下步骤:6. A method for preparing the energetic structural material according to any one of claims 1 to 5, comprising the following steps: (1)混料:根据含能结构材料的配方,将铝粉、高密度金属粉末、和金属氧化物粉末进行混合,得到混合粉末;(1) Mixing: According to the formula of energetic structural materials, aluminum powder, high-density metal powder, and metal oxide powder are mixed to obtain mixed powder; (2)预成型:对混合粉末进行冷压,得到预成型体;(2) Preforming: Cold pressing the mixed powder to obtain a preform; (3)烧结:对预成型体进行烧结,得到块状含能结构材料。(3) Sintering: The preform is sintered to obtain bulk energetic structural materials. 7.根据权利要求6所述的含能结构材料的制备方法,其特征在于,所述步骤(1)中,所述混合粉末的粒度为0.1μm~50μm;所述步骤(2)中,所述冷压压力为100MPa~600MPa,时间为1min~10min。7. The method for preparing energetic structural materials according to claim 6, characterized in that, in the step (1), the particle size of the mixed powder is 0.1 μm to 50 μm; in the step (2), the The cold pressing pressure is 100MPa-600MPa, and the time is 1min-10min. 8.根据权利要求7所述的含能结构材料的制备方法,其特征在于,所述步骤(3)中,所述烧结包括常压烧结和热压烧结。8 . The method for preparing energetic structural materials according to claim 7 , wherein in the step (3), the sintering includes atmospheric pressure sintering and hot-press sintering. 9.根据权利要求8所述的含能结构材料的制备方法,其特征在于,所述步骤(3)中,所述烧结的温度为300℃~600℃,保温时间为0.5h~3h;所述热压烧结的压力为100MPa~600MPa。9. The preparation method of energetic structural materials according to claim 8, characterized in that, in the step (3), the sintering temperature is 300°C-600°C, and the holding time is 0.5h-3h; The pressure of the hot pressing sintering is 100MPa-600MPa. 10.一种如权利要求1~5任一项所述的含能结构材料或如权利要求6~9任一项所述的含能结构材料的制备方法所制备的含能结构材料在战斗部中的应用。10. An energetic structural material as described in any one of claims 1 to 5 or an energetic structural material prepared by the method for preparing an energetic structural material as described in any one of claims 6 to 9 in the warhead in the application.
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CN110360902A (en) * 2019-08-01 2019-10-22 北京理工大学 A kind of preparation method for the micro- bullet of active metal being mounted with high explosive
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CN113649579A (en) * 2021-08-18 2021-11-16 北京理工大学 Composite energetic fragment containing tough outer layer and brittle inner layer and preparation method thereof
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