CHINESE JOURNAL OF ENERGETIC MATERIALS
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铝锂合金稳定化包覆及其推进剂应用
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1.哈尔滨工业大学化工与化学学院, 黑龙江 哈尔滨 150001;2.湖北航天化学技术研究所, 湖北 襄阳 441003

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国家自然科学基金(22175059)


Stabilization Coating of Aluminum-Lithium Alloy and its Application in Propellant
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1.School of Chemistry and Chemical Engineering,Harbin Institute of Technology,Harbin 150001, China;2.Hubei Institute of Aerospace Chemotechnology,Xiangyang 441003, China

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    摘要:

    Al-5Li合金是一种理想的合金燃料,具有放热量高、燃烧时会产生微爆的特点,替代铝粉可显著提高推进剂的燃烧效率。然而Al-5Li合金粉体具有较高的反应活性,易与推进剂组分反应,致使推进剂内存在气孔裂纹等结构缺陷,无法直接应用于推进剂中。为了提高Al-5Li合金的稳定性及相容性,采用7%长链烷酸(PA)对Al-5Li合金粉末进行表面包覆,得到了具有高稳定性、高相容性的Al-5Li@7PA样品,表面致密无裂纹,PA分子通过化学键作用附着在合金表面,包覆后样品可稳定存在于70 ℃热水中30 min。与Al-5Li相比,包覆后样品的燃烧热提升了4.55%;相容性和装药性方面,Al-5Li@7PA样品与HTPB(端羟基聚丁二烯)的相容性等级由5级提升至1级,药柱内无任何气孔裂纹等缺陷,表明包覆后的Al-5Li合金满足了推进剂装药需求。推进剂燃烧性能测试表明,与Q3 Al粉相比,Al-5Li@7PA推进剂的燃速和燃温分别提升了10.28%和45.41%,燃烧产物残渣粒径更小。

    Abstract:

    As a ideal alloy fuel, Al-5Li alloy can significantly improve the combustion efficiency of propellant with the characteristics of high heat release and micro-explosion during combustion compared with Al. However, Al-5Li alloy powders have high reactivity which is easier to react with the components of propellant, preventing it from being used in propellants directly with some structure related defects, such as pores and cracks. In order to improve the stability and compatibility of Al-5Li alloy, the Al-5Li@7PA samples with high stability and compatibility were obtained through the coating treatment of 7% long-chain alkanoic acid (PA). The surface is dense and crack-free, and PA molecules adhere to the alloy surface through chemical bonding. The coated samples can be stable in hot water for 30 min. It"s worth noting that the heat of combustion of Al-5Li@7PA samples has an increase of 4.55% compared with the raw Al-5Li. At the aspects of compatibility and chargeability, the compatibility level with HTPB of Al-5Li@7PA samples has increased from level 5 to level 1, and there are no defects such as pores and cracks in the grain column, indicating that the coated Al-5Li alloy meets the propellant charging requirements. Propellant combustion performance test shows that the combustion rate and temperature of Al-5Li@7PA have increased by 10.28% and 45.41% compared with Q3 Al propellant respectively, and the particle size of the combustion product residue is smaller.

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引用本文

李佳贺,杜芳,唐长盛,等.铝锂合金稳定化包覆及其推进剂应用[J].含能材料, 2024, 32(1):2-11. DOI:10.11943/CJEM2023223.
LI Jia-he, DU Fang, TANG Chang-sheng, et al. Stabilization Coating of Aluminum-Lithium Alloy and its Application in Propellant[J]. Chinese Journal of Energetic Materials, 2024, 32(1):2-11. DOI:10.11943/CJEM2023223.

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历史
  • 收稿日期: 2023-10-27
  • 最后修改日期: 2023-12-02
  • 录用日期: 2023-11-29
  • 在线发布日期: 2023-11-30
  • 出版日期: 2024-01-25