氧乙炔与等离子烧蚀试验的系统评价研究

doi:10.11896/cldb.21020107

材料导报

2022, Vol. 36

Issue (11): 21020107-5 https://doi.org/10.11896/cldb.21020107

高分子与聚合物基复合材料

氧乙炔与等离子烧蚀试验的系统评价研究

马康智, 李春, 倪立勇, 杨震晓, 曲栋, 文波, 李炜

航天材料及工艺研究所,北京 100076

Research and Systematical Evaluation of Oxyacetylene and Plasma Ablation Tests

MA Kangzhi, LI Chun, NI Liyong, YANG Zhenxiao, QU Dong, WEN Bo, LI Wei

Institute of Aerospace Materials and Technology, Beijing 100076, China

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摘要针对航天用复合材料烧蚀性能考核应用需求,本工作搭建了氧乙炔及等离子烧蚀热流密度测试平台,系统评价了影响烧蚀热流密度的主要因素,比较了两种烧蚀方式热流密度的差异,建立了烧蚀条件与热流密度的数学物理模型,提出了烧蚀热流密度的控制策略。结果表明:氧乙炔烧蚀及等离子烧蚀的热流密度均随烧蚀距离的缩短而增大,与烧蚀距离的倒数呈抛物线关系。距离较远时,氧乙炔烧蚀热流密度较大;距离较近时,等离子烧蚀热流密度超过氧乙炔。F4等离子喷枪烧蚀热流密度的变化规律与9M喷枪规律类似,但随着烧蚀距离、电流及辅气流量的变化更为显著。此外,辅气(H₂)流量增加及电流增大均使等离子烧蚀热流密度增大。

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关键词: 氧乙炔烧蚀等离子烧蚀热流密度距离 H₂流量电流

Abstract: Aiming to evaluate the ablation performance of aerospace composite materials, a heat flux testing device for oxyacetylene and plasma ablation tests was established in this work. The main factors affecting the ablative heat flux were systematically evaluated, and the differences between oxyacetylene and plasma ablation tests were compared. Mathematical and physical models of heat flux as a function of ablation conditions were deducted, and the control strategy was proposed for oxyacetylene and plasma ablation tests. Results show that the heat flux for oxyacetylene and plasma ablation tests increases with the decrease of ablative distance, and shows a parabola relationship with the reciprocal of distance. The ablative heat flux of oxyacetylene is higher than that of plasma ablation at a longer distance, but becomes lower at a shorter distance. The heat flux for F4 plasma torch is similar to the 9M torch, but the change is more significant with the change of ablative distance, spraying current and auxiliary gas (H₂) flow rate. Moreover, the increase of auxiliary gas flow rate and the spraying current also enhances the heat flux of plasma ablation.

Key words: oxyacetylene ablation plasma ablation heat flux distance H₂ flow rate current

发布日期: 2022-06-09

ZTFLH:

TB302

基金资助: 国家自然科学基金(51971013)

通讯作者: lichun@buaa.edu.cn

作者简介: 马康智,航天科技集团公司一院航天材料及工艺研究所高级工程师。2010年9月至2013年6月,在北京理工大学获得材料科学与工程专业工学硕士学位。以第一作者在国内外学术期刊上发表论文10余篇,申请国家发明专利8项,其中授权4项。从事耐烧蚀、耐腐蚀、抗冲击、耐磨等功能涂层材料及涂层制备工艺技术的研究工作,主持和参研多项装发“十三五”预研项目及航天一院科研基金项目等。
李春,航天科技集团公司一院航天材料及工艺研究所工程师。2011年9月至2020年8月,在北京航空航天大学获得材料科学与工程专业工学学士学位和博士学位。发表SCI论文10余篇,共申请国家发明专利3项,其中授权1项。长期从事热喷涂、热障涂层、以及超高温热结构材料等领域的研究工作,参与研究多项国家自然基金面上项目以及国防科技工业项目。

引用本文:

马康智, 李春, 倪立勇, 杨震晓, 曲栋, 文波, 李炜. 氧乙炔与等离子烧蚀试验的系统评价研究[J]. 材料导报, 2022, 36(11): 21020107-5.
MA Kangzhi, LI Chun, NI Liyong, YANG Zhenxiao, QU Dong, WEN Bo, LI Wei. Research and Systematical Evaluation of Oxyacetylene and Plasma Ablation Tests. Materials Reports, 2022, 36(11): 21020107-5.

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http://www.mater-rep.com/CN/10.11896/cldb.21020107 或 http://www.mater-rep.com/CN/Y2022/V36/I11/21020107

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