CN111892466A - High-density high-energy metal fuel - Google Patents
High-density high-energy metal fuel Download PDFInfo
- Publication number
- CN111892466A CN111892466A CN202010725818.5A CN202010725818A CN111892466A CN 111892466 A CN111892466 A CN 111892466A CN 202010725818 A CN202010725818 A CN 202010725818A CN 111892466 A CN111892466 A CN 111892466A
- Authority
- CN
- China
- Prior art keywords
- density
- energy
- metal fuel
- metal
- percent
- 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.)
- Pending
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B27/00—Compositions containing a metal, boron, silicon, selenium or tellurium or mixtures, intercompounds or hydrides thereof, and hydrocarbons or halogenated hydrocarbons
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Abstract
The invention relates to a high-density high-energy metal fuel, belonging to the technical field of energetic materials. The metal fuel comprises the following components in percentage by mass based on 100% of the total mass of the metal fuel formula: 1.0 to 10.0 percent of magnesium, 57.0 to 73.0 percent of boron and 26.0 to 39.0 percent of high-density metal; the high-density metal is titanium, tungsten or zirconium. The metal fuel is prepared by a ball milling method or a mechanical mixing method at 500-800 ℃ in an inert atmosphere. The metal fuel can effectively improve the energy level of the energy-containing system and realize the great leap of the total energy release value of the energy-containing system; the metal source is wide, the cost is low, the large-scale production is facilitated, and the method has wide application prospect in the fields of propellants and explosives.
Description
Technical Field
The invention relates to a high-density high-energy metal fuel, in particular to a high-density high-energy metal fuel for manufacturing explosives and powders, belonging to the technical field of energetic materials.
Background
The chemical nature of high explosive is a mixed system of oxidizer and combustible agent close to zero oxygen balance. Currently, the output power of the mixed explosive improved by means of synthesizing new single-substance explosives does not have much space for rising. In recent years, some synthesized oxidants with explosive energy higher than that of CL-20 explosives cannot be applied due to the limitations of safety, stability and the like. Therefore, another approach is needed to increase the energy of the mixed explosive. The intervention of the novel high-energy fuel is an important means for greatly improving the total energy release value of the mixed explosive.
Since the 21 st century, the high-energy explosive technology with high-energy metal fuel as the core is regarded as a strategic means for guaranteeing the national safety, and the world first-class military and the strong country invest a great deal of capital in the research and development of the high-energy metal fuel. Under the drive of America and Russia, relevant development plans and research projects are started in Germany, Sweden, India, Japan and other countries, and research and application of high-energy metal fuel are promoted. The novel high-energy metal fuel explosive has become an important leading-edge technology for constructing conventional deterrence force and actual combat capability in a few military strong countries, and the development level of the novel high-energy metal fuel explosive represents national defense actual force and combat capability of the country. China also actively explores the preparation of high-energy metal fuel so as to obtain the high-energy metal fuel with higher combustion heat value than the traditional metal aluminum. The traditional binary alloy can only meet the requirement of high combustion heat value, but cannot simultaneously ensure the density level, which is far from enough for an energy-containing system.
Disclosure of Invention
In order to overcome the defects in the prior art, the invention aims to provide a high-density high-energy metal fuel which is suitable for manufacturing explosives and powders.
In order to achieve the purpose of the invention, the following technical scheme is provided.
The high-density high-energy metal fuel comprises the following components in percentage by mass, based on 100% of the total mass of a metal fuel formula:
1.0 to 10.0 percent of magnesium,
57.0-73.0% of boron and 26.0-39.0% of high-density metal.
Wherein the high density metal is titanium, tungsten or zirconium.
The invention relates to a preparation method of a high-density high-energy metal fuel, which adopts a ball milling method or a mechanical mixing method at the temperature of 500-800 ℃ under an inert atmosphere.
The ball milling method under the inert atmosphere comprises the following specific steps:
placing agate balls, magnesium, boron and high-density metal powder into a ball mill, ball-milling for 8-30 h at 500-800 ℃ in an inert atmosphere, and stopping ball-milling to obtain the high-density high-energy metal fuel, wherein the high-density high-energy metal fuel contains a small amount of amorphous magnesium/boron/high-density intermetallic compounds.
Advantageous effects
1. The invention provides a high-density high-energy metal fuel, which can effectively improve the energy level of an energy-containing system, improve the operational efficiency of a weapon system, realize the great leap of the total energy release value of the energy-containing system and have wide application prospects in the fields of propellants and explosives.
2. The invention provides a high-density high-energy metal fuel, which has wide metal sources, low cost, large-scale production and huge application potential.
Drawings
FIG. 1 is a scanning electron microscope photograph of the final product obtained in example 2.
Detailed Description
The invention is further illustrated by the following examples, which are not intended to limit the scope of the invention.
The following tests were carried out on the products prepared in the following examples:
(1) density of
The test was performed using a BelPycno full-automatic true density analyzer from macxbair, usa.
(2) Heat value
The test was carried out using a C2000 standard oxygen bomb calorimeter from IKA, Germany.
(3) Morphology and elemental distribution
The test was carried out using a Scanning Electron Microscope (SEM) model S-4700 of Hitachi, Japan and its accompanying X-ray energy spectrometer EDS.
Example 1
The high-density high-energy metal fuel comprises the following components in percentage by mass, based on 100% of the total mass of a metal fuel formula: 10.0 percent of magnesium, 57.0 percent of boron and 33.0 percent of titanium.
The preparation method adopts a high-temperature ball milling method and comprises the following specific steps:
placing agate balls, magnesium, boron and high-density metal powder titanium into a ball mill, ball-milling for 10 hours at the temperature of 650 ℃ in an argon atmosphere, and stopping ball-milling to obtain a final product, namely the high-density high-energy metal fuel, wherein the final product contains a small amount of amorphous magnesium/boron/titanium intercrystallization compounds.
The final products obtained were tested and the results were as follows:
(1) density of
The density was 2.73g/cm3。
(2) Heat value
The mass heat of combustion was 9925 kJ/kg.
(3) Morphology and elemental distribution
The test was carried out using a Scanning Electron Microscope (SEM) model S-4700 from Hitachi, Japan and its own X-ray energy spectrometer EDS.
The final product was observed by scanning electron microscopy and showed: the product particles are fine, and the components are mixed uniformly.
The energy spectrometer test shows that the element mass fraction distribution is as follows: 10.0 percent of magnesium, 57.0 percent of boron and 33.0 percent of titanium.
Example 2
The high-density high-energy metal fuel comprises the following components in percentage by mass, based on 100% of the total mass of a metal fuel formula: 1.0% of magnesium, 73.0% of boron and 26.0% of tungsten.
The preparation method adopts a high-temperature ball milling method and comprises the following specific steps:
placing agate balls, magnesium, boron and high-density metal powder tungsten into a ball mill, ball-milling for 30h at 800 ℃ in an argon atmosphere, and stopping ball-milling to obtain a final product, namely the high-density high-energy metal fuel, wherein the final product contains a small amount of amorphous magnesium/boron/tungsten intercompound.
The final products obtained were tested and the results were as follows:
(1) density of
The density was 3.065g/cm3。
(2) Heat value
The mass heat of combustion was 8726 kJ/kg.
(3) Morphology and elemental distribution
The test was carried out using a Scanning Electron Microscope (SEM) model S-4700 of Hitachi, Japan and its accompanying X-ray energy spectrometer EDS.
The final product was observed by scanning electron microscopy, as shown in FIG. 1, and the results indicated that: the product particles are fine, and the components are mixed uniformly.
The energy spectrometer test showed the following element distributions: 1.0% of magnesium, 73.0% of boron and 26.0% of tungsten.
Example 3
The high-density high-energy metal fuel comprises the following components in percentage by mass, based on 100% of the total mass of a metal fuel formula: 3.0 percent of magnesium, 58.0 percent of boron and 39.0 percent of zirconium.
The preparation method adopts a high-temperature ball milling method and comprises the following specific steps:
placing agate balls, magnesium, boron and high-density metal zirconium powder into a ball mill, carrying out ball milling for 8 hours in an argon environment at 500 ℃, and stopping ball milling to obtain a final product, namely the high-density high-energy metal fuel, wherein the final product contains a small amount of amorphous magnesium/boron/zirconium intercompound.
The final products obtained were tested and the results were as follows:
(1) density of
The density was 3.065g/cm3。
(2) Heat value
The mass heat of combustion was 8726 kJ/kg.
(3) Morphology and elemental distribution
The test was carried out using a Scanning Electron Microscope (SEM) model S-4700 of Hitachi, Japan and its accompanying X-ray energy spectrometer EDS.
The final product was observed by scanning electron microscopy and showed: the product particles are fine, and the components are mixed uniformly.
The energy spectrometer test showed the following element distributions: 3.0 percent of magnesium, 58.0 percent of boron and 39.0 percent of zirconium.
Claims (3)
1. A high-density high-energy metal fuel is characterized in that: the metal fuel comprises the following components in percentage by mass based on 100% of the total mass of the metal fuel formula:
1.0 to 10.0 percent of magnesium,
57.0 to 73.0 percent of boron,
26.0 to 39.0 percent of high-density metal;
the high-density metal is titanium, tungsten or zirconium.
2. A method for producing a high-density high-energy metal fuel as defined in claim 1, wherein: the method is a ball milling method or a mechanical mixing method under the inert atmosphere of 500-800 ℃.
3. The method for preparing a high-density high-energy metal fuel as claimed in claim 2, wherein: the ball milling method under the inert atmosphere comprises the following specific steps:
placing agate balls, magnesium, boron and high-density metal powder into a ball mill, ball-milling for 8-30 h at 500-800 ℃ in an inert atmosphere, and stopping ball-milling to obtain the high-density high-energy metal fuel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010725818.5A CN111892466A (en) | 2020-07-24 | 2020-07-24 | High-density high-energy metal fuel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010725818.5A CN111892466A (en) | 2020-07-24 | 2020-07-24 | High-density high-energy metal fuel |
Publications (1)
Publication Number | Publication Date |
---|---|
CN111892466A true CN111892466A (en) | 2020-11-06 |
Family
ID=73189921
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202010725818.5A Pending CN111892466A (en) | 2020-07-24 | 2020-07-24 | High-density high-energy metal fuel |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN111892466A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113956120A (en) * | 2021-10-22 | 2022-01-21 | 北京理工大学 | Propellant mixed fuel of molecular perovskite energetic material composite metal aluminum |
CN114085120A (en) * | 2021-10-22 | 2022-02-25 | 北京理工大学 | Boron-containing molecular perovskite energetic material mixed fuel |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6736912B1 (en) * | 1977-03-24 | 2004-05-18 | Jerry L. Fields | Combustible compositions for air-augmented rocket engines |
CN103030483A (en) * | 2012-12-26 | 2013-04-10 | 南京理工大学 | Bright green cold firework composition and production method thereof |
CN105838472A (en) * | 2016-03-22 | 2016-08-10 | 天津大学 | Gel fuel and preparation method |
CN106542942A (en) * | 2016-10-21 | 2017-03-29 | 重庆大学 | A kind of boracic fuel-rich electric ignition solid propellant and preparation method thereof |
CN106905091A (en) * | 2017-03-15 | 2017-06-30 | 重庆大学 | It is a kind of based on perchlorate can automatically controlled burning solid propellant and preparation method thereof |
CN107879867A (en) * | 2017-06-28 | 2018-04-06 | 湖北航天化学技术研究所 | A kind of high-energy insensitive is pressed plastic bonded explosive |
CN108892599A (en) * | 2018-08-15 | 2018-11-27 | 湖北航天化学技术研究所 | A kind of fuel-rich propellant formula |
CN109851457A (en) * | 2019-03-22 | 2019-06-07 | 湖北航天化学技术研究所 | A kind of automatically controlled solid propellant and preparation method thereof containing metal fuel |
CN110981665A (en) * | 2019-12-24 | 2020-04-10 | 湖北航天化学技术研究所 | Boron-containing fuel-rich propellant for platform combustion |
-
2020
- 2020-07-24 CN CN202010725818.5A patent/CN111892466A/en active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6736912B1 (en) * | 1977-03-24 | 2004-05-18 | Jerry L. Fields | Combustible compositions for air-augmented rocket engines |
CN103030483A (en) * | 2012-12-26 | 2013-04-10 | 南京理工大学 | Bright green cold firework composition and production method thereof |
CN105838472A (en) * | 2016-03-22 | 2016-08-10 | 天津大学 | Gel fuel and preparation method |
CN106542942A (en) * | 2016-10-21 | 2017-03-29 | 重庆大学 | A kind of boracic fuel-rich electric ignition solid propellant and preparation method thereof |
CN106905091A (en) * | 2017-03-15 | 2017-06-30 | 重庆大学 | It is a kind of based on perchlorate can automatically controlled burning solid propellant and preparation method thereof |
CN107879867A (en) * | 2017-06-28 | 2018-04-06 | 湖北航天化学技术研究所 | A kind of high-energy insensitive is pressed plastic bonded explosive |
CN108892599A (en) * | 2018-08-15 | 2018-11-27 | 湖北航天化学技术研究所 | A kind of fuel-rich propellant formula |
CN109851457A (en) * | 2019-03-22 | 2019-06-07 | 湖北航天化学技术研究所 | A kind of automatically controlled solid propellant and preparation method thereof containing metal fuel |
CN110981665A (en) * | 2019-12-24 | 2020-04-10 | 湖北航天化学技术研究所 | Boron-containing fuel-rich propellant for platform combustion |
Non-Patent Citations (3)
Title |
---|
赵凤起,等: "《神奇的含能材料》", 30 November 2017, 国防工业出版社 * |
路甬祥: "《现代科学技术大众百科 技术卷》", 30 June 2001, 浙江教育出版 * |
陈勇,等: "《面对等离子体钨基复合材料的制备及其性能研究》", 31 October 2009, 合肥工业大学出版社 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113956120A (en) * | 2021-10-22 | 2022-01-21 | 北京理工大学 | Propellant mixed fuel of molecular perovskite energetic material composite metal aluminum |
CN114085120A (en) * | 2021-10-22 | 2022-02-25 | 北京理工大学 | Boron-containing molecular perovskite energetic material mixed fuel |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN111892466A (en) | High-density high-energy metal fuel | |
CN111097919B (en) | Preparation method of multi-component refractory alloy spherical powder | |
CN109332695B (en) | Selective laser melting preparation method of molybdenum-based alloy with enhanced oxidation resistance | |
CN113354494B (en) | High-density specific impulse propellant and preparation method thereof | |
Yang et al. | Reinforced combustion of the ZrH2-HMX-CMDB propellant: The critical role of hydrogen | |
CN108103337B (en) | Preparation method of magnesium-based hydrogen storage material | |
CN111825936B (en) | Aluminum powder/polytetrafluoroethylene composite material and preparation method thereof | |
CN102286694A (en) | Oxidation-resistant iron-based high-temperature alloy and preparation method thereof | |
CN101525716B (en) | Iron aluminide intermetallic compound-titanium diboride composite material and preparation method thereof | |
Chen et al. | Effect of CuO on the thermal kinetics and combustion properties of Al/MoO3 thermite prepared by ball milling | |
Li et al. | Thermal decomposition reaction mechanism and combustion performance of AlH3/AP energetic composite | |
CN110629100A (en) | Preparation method of oxide dispersion strengthened nickel-based high-temperature alloy | |
CN113929547B (en) | High-calorific-value boron-based composite powder and preparation method thereof | |
CN101723670B (en) | Ti(CxN1-x)/Al2O3 composite material and preparation method thereof | |
CN111484384B (en) | Metal/carbon-coated boron-based composite fuel and preparation method thereof | |
CN111331130B (en) | Preparation method of flower-shaped nano manganese hydroxide coated aluminum composite material | |
CN109081766A (en) | A kind of Al-NaF hybrid fuel and its preparation method and application | |
CN111471884A (en) | Ternary alloy Mg0.5Al0.5B2Preparation method | |
CN113651659A (en) | Metal-based energetic fragment with impact reaction activity and preparation method thereof | |
CN114230428A (en) | Boron-containing high-energy solid propellant | |
Wang et al. | Dual-core–shell structure B@ LiF@ AP with multi-effect synergies to improve processibility and energy release characteristics of B | |
CN111892966B (en) | High-energy metal fuel for boron-containing propellant | |
CN106521275A (en) | Carbon magnesium base composite hydrogen storage material and preparation method thereof | |
CN115650812B (en) | Coordination ion type high-energy aluminum powder, preparation method and application thereof | |
LU503579B1 (en) | 1,2,4-triazole nitrate-coated boron-magnesium composite metal powder fuel and preparation method therefor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20201106 |
|
RJ01 | Rejection of invention patent application after publication |