金属热处理 ›› 2026, Vol. 51 ›› Issue (2): 313-318.DOI: 10.13251/j.issn.0254-6051.2026.02.047

• 数值模拟 • 上一篇    下一篇

真空气淬冷却模式对流场与温度场的影响

白鹭1, 张小娟1, 周钟平1, 王婧2, 何敏1, 向超1   

  1. 1.上海航天动力技术研究所, 上海 201109;
    2.上海交通大学 材料科学与工程学院, 上海 200240
  • 收稿日期:2025-09-05 修回日期:2026-01-04 发布日期:2026-03-05
  • 作者简介:白 鹭(1994—),女,工程师,硕士,主要从事材料制造工作

Effect of vacuum gas quenching cooling mode on flow field and temperature field

Bai Lu1, Zhang Xiaojuan1, Zhou Zhongping1, Wang Jing2, He Min1, Xiang Chao1   

  1. 1. Shanghai Space Propulsion Technology Research Institute, Shanghai 201109, China;
    2. School of Materials Science and Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
  • Received:2025-09-05 Revised:2026-01-04 Published:2026-03-05

摘要: 采用温度曲线实测与热处理仿真相结合的方式,建立了大长径比薄壁燃烧室壳体多发件炉条件下真空气淬过程中炉内温度场、流场仿真分析模型。为减小壳体淬火畸变,采用改变设备出风口组合方式的方法,改善淬火过程充气及内循环阶段的流场及温度场分布。结果表明,原始4风口装炉3个壳体条件下,由于设备本身结构特点,燃烧室壳体存在阴阳面差异及炉内上下区域差异,各位置壳体的冷却速度整体呈现为阳面上>阳面下>阴面上>阴面下。冷却模式调整后,3风口模型和原始模型效果相近,对流场、温度场影响效果甚微,而1风口模型影响较大,可提升壳体背风面的冷却速度18%以上,温差降低31.5%以上,提高了壳体的温度均匀性。经产品应用验证畸变程度减小22.2%,力学性能均满足设计指标要求,该改进措施对燃烧室壳体的力学性能基本没有影响。

关键词: 真空气淬, 冷却模式, 流场, 温度场, 淬火畸变

Abstract: Combination of temperature curve measurement and heat treatment simulation was adopted to establish a simulation analysis model for the temperature and flow fields inside the vacuum gas quenching process of thin-walled combustion chamber shells with large aspect ratios under multiple-charge furnace loading. In order to reduce the quenching distortion of the shell, a method of changing the air outlet combination of the equipment was used to improve the flow filed and temperature field distribution in the inflation and domestic circulation stages of the quenching process. The results show that under the condition of the original four air outlets and charging 3 shells, due to the structural characteristics of the equipment itself, there are differences in front and back surfaces of the combustion chamber shell and differences in the upper and lower regions of the furnace, and the overall cooling rate of the shells at different positions follows the order of upper windward>lower windward>upper leeward>lower leeward. After adjusting the cooling mode, the results show that the effect of the three air outlets model is similar to the original model, and the effect on the flow field and temperature field is minimal, while the one air outlet model has a greater impact. Under the one air outlet model, the cooling rate of the leeward side of the shell is increased by more than 18%, and the temperature difference is reduced by more than 31.5%, which improves the temperature uniformity of the shell. The distortion degree of the product is reduced by 22.2%, and the mechanical properties meet the requirements of design index, indicating that the optimized mode has a little effect on the mechanical properties of the combustion chamber shell.

Key words: vacuum gas quenching, cooling mode, flow field, temperature field, quenching distortion

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