Thermally coupled SHS processes in (Ni + Al)/(Co + Ti)/(Ni + Al) layered system: experimental and theoretical study

R. Gabbasov, V. Kitler, V. Prokof'ev, A. M. Shul’pekov
{"title":"Thermally coupled SHS processes in (Ni + Al)/(Co + Ti)/(Ni + Al) layered system: experimental and theoretical study","authors":"R. Gabbasov, V. Kitler, V. Prokof'ev, A. M. Shul’pekov","doi":"10.17073/1997-308x-2021-4-20-29","DOIUrl":null,"url":null,"abstract":"The paper focuses on the theoretical and experimental study of the mechanisms of reaction mixture combustion in the ≪chemical oven≫ mode in a three-layer Ni–Al/Ti–Co/Ni–Al sample. Experimental studies were carried out in a reactor in an argon atmosphere at atmospheric pressure and an ambient temperature of 298 K on rectangular samples pressed from Ni–Al and Ti–Co powder mixtures in the form of a three-layer package. The Ti–Co acceptor layer was in the middle of the sample, and the Ni–Al donor layer was outside. The acceptor layer thickness was varied from 4.3 to 13 mm, while the donor layer thickness (4.7 mm) remained constant. It was found that as the acceptor layer thickness increases, the combustion wave front propagation velocity and reaction initiation temperature decrease, and the maximum temperature in the front remains constant and equal to the melting point of the final product. The time of acceptor layer heating before the reaction increases. The acceptor mixture reaction proceeds in the thermal explosion mode when the thickness of the acceptor layer exceeds that of the donor one. Maximum temperature in this case is higher than the melting point of the final product. The inner layer synthesis modes change with an increase in the acceptor layer thickness: stationary – pulsating – extinction. The mathematical model of the three-layer sample high-temperature synthesis in dimensional variables is constructed taking into account heat transfer with the environment. As a result of experimental studies and numerical calculations, the critical thickness of the inner layer was found to be 15 mm, at which the inner layer combustion becomes impossible at fixed sizes of donor layers. Critical conditions for the combustion wave propagation along the acceptor layer are weakly dependent on the external heating source. The experimental technique and mathematical model of the layered system combustion can be used to assess the critical conditions for the metal composite synthesis in the frontal combustion mode.","PeriodicalId":14693,"journal":{"name":"Izvestiya vuzov. Poroshkovaya metallurgiya i funktsional’nye pokrytiya","volume":"9 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2021-12-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Izvestiya vuzov. Poroshkovaya metallurgiya i funktsional’nye pokrytiya","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.17073/1997-308x-2021-4-20-29","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

The paper focuses on the theoretical and experimental study of the mechanisms of reaction mixture combustion in the ≪chemical oven≫ mode in a three-layer Ni–Al/Ti–Co/Ni–Al sample. Experimental studies were carried out in a reactor in an argon atmosphere at atmospheric pressure and an ambient temperature of 298 K on rectangular samples pressed from Ni–Al and Ti–Co powder mixtures in the form of a three-layer package. The Ti–Co acceptor layer was in the middle of the sample, and the Ni–Al donor layer was outside. The acceptor layer thickness was varied from 4.3 to 13 mm, while the donor layer thickness (4.7 mm) remained constant. It was found that as the acceptor layer thickness increases, the combustion wave front propagation velocity and reaction initiation temperature decrease, and the maximum temperature in the front remains constant and equal to the melting point of the final product. The time of acceptor layer heating before the reaction increases. The acceptor mixture reaction proceeds in the thermal explosion mode when the thickness of the acceptor layer exceeds that of the donor one. Maximum temperature in this case is higher than the melting point of the final product. The inner layer synthesis modes change with an increase in the acceptor layer thickness: stationary – pulsating – extinction. The mathematical model of the three-layer sample high-temperature synthesis in dimensional variables is constructed taking into account heat transfer with the environment. As a result of experimental studies and numerical calculations, the critical thickness of the inner layer was found to be 15 mm, at which the inner layer combustion becomes impossible at fixed sizes of donor layers. Critical conditions for the combustion wave propagation along the acceptor layer are weakly dependent on the external heating source. The experimental technique and mathematical model of the layered system combustion can be used to assess the critical conditions for the metal composite synthesis in the frontal combustion mode.
(Ni + Al)/(Co + Ti)/(Ni + Al)层状体系热耦合SHS过程的实验与理论研究
本文着重对Ni-Al / Ti-Co / Ni-Al三层样品在“化学烘箱”模式下反应混合物燃烧机理进行了理论和实验研究。在常压和298 K环境温度的氩气反应器中,对镍铝和钛钴粉末混合物压制成三层包体的矩形样品进行了实验研究。Ti-Co受体层位于样品的中间,Ni-Al给体层位于样品的外侧。受体层厚度变化范围为4.3 ~ 13 mm,而供体层厚度保持不变(4.7 mm)。研究发现,随着受体层厚度的增加,燃烧波前传播速度和反应起始温度降低,燃烧波前的最高温度保持不变,且等于最终产物的熔点。反应前受体层加热的时间增加。当受体层厚度超过供体层厚度时,受体混合反应以热爆炸模式进行。在这种情况下,最高温度高于最终产品的熔点。内层合成模式随受体层厚度的增加而变化:平稳-脉动-消光。建立了考虑环境传热的三层样品高温合成的量纲变量数学模型。通过实验研究和数值计算,得出了内层的临界厚度为15mm,在固定尺寸的供层下,内层燃烧是不可能的。燃烧波沿受热层传播的临界条件对外部热源的依赖性较弱。层状体系燃烧的实验技术和数学模型可用于评估金属复合材料在正面燃烧模式下合成的临界条件。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信