离心式压气机是柴油机的核心部件,其性能直接关系到柴油机效率和动力输出。传统的预测柴油机离心压气机二维计算方法存在精度与复杂度的限制,需改进才能提高预测准确性。本文基于改进的流线曲率法对2种离心式压气机通流特性进行预测分析,并与试验结果进行对比。结果表明,改进的流线曲率法对离心式压气机气动性能的预测结果与试验结果吻合较好,改进后的流线曲率法在近设计工况下的预测相对误差不超过5%,验证了该方法的可靠性和准确性,说明改进的流线曲率法不仅提高了离心式压气机性能预测的精度,还拓宽了适用工况范围,且该方法能够为柴油机离心压气机部件的设计及优化过程提供有力支持,缩短研制周期并降低研制费用。
The centrifugal compressor, as a key component of the diesel engine, directly affects the efficiency and power output of the diesel engine. The traditional two-dimensional calculation method for predicting the aerodynamic performance of the diesel centrifugal compressor needs to be improved to enhance the prediction accuracy. In this paper, the aerodynamic performance of two centrifugal compressors was predicted and analyzed based on the improved streamline curvature method, and the results were compared with the experimental data. The results show that the predicted aerodynamic performance of the centrifugal compressor using the improved streamline curvature method is in good agreement with the experimental results, and the relative error of the prediction at the near design condition is less than 5%. This verifies the reliability and accuracy of the improved method, indicating that the improved streamline curvature method not only improves the prediction accuracy of the centrifugal compressor performance, but also broadens the applicable operating range. The method can provide strong support for the design and optimization process of the centrifugal compressor of the diesel engine, shorten the research and development cycle, and reduce the research and development costs.
2025,47(9): 102-107 收稿日期:2024-7-8
DOI:10.3404/j.issn.1672-7649.2025.09.018
分类号:V231.3
基金项目:国家自然科学基金青年项目(52205271)
作者简介:解放(1994-)男,硕士,工程师,研究方向为机械结构设计
参考文献:
[1] 高丽敏, 杨光, 王浩浩, 等. 波纹对高亚音叶型气动敏感位置和宽度研究[J]. 工程热物理学报, 2023, 44(1): 78-85.
[2] WU C H. A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-, radial-, and mixed-flow types[R]. NACA-TN-2604, 1952.
[3] QUINTANILLA V , BRIGGS K , MORRIS M , et al. Performance of a supercritical carbon dioxide compressor using a streamline curvature based throughflow method[J]. Applied Thermal Engineering, 2024, 24(12): 22-29.
[4] HOSEIN B , VAHID E , ALIREZA T , et al. Improved streamline curvature method for prediction of gas turbines performance[J]. Arabian Journal for Science and Engineering, 2023, 49(2): 2749-2766.
[5] RASOOL H , ALI N , ULLAH K. Bifurcations of streamlines in peristaltic flow without lubrication approximation: A case study[J]. ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 2023, 10(4): 1-2.
[6] 戎毅, 廖凯龙, 孙恩慧, 等. 基于流线曲率法的超临界二氧化碳离心压缩机通流计算方法[J]. 热力发电, 2024, 53(2): 124-132.
[7] 巫骁雄, 刘波, 唐天全. 流线曲率法在多级跨声速轴流压气机特性预测中的应用[J]. 推进技术, 2017(10): 2235-2245.
[8] 王剑. 基于流线曲率法的周向弯曲叶片的性能计算[D]. 上海: 上海交通大学, 2012.
[9] 郑覃, 杨小贺, 叶俊, 等. 变外涵工况下风扇增压级双涵匹配机理[J]. 航空动力学报, 2022, 37(9): 1946-1956.
[10] 张超炜. 离心压气机性能预测模型及气动设计方法研究[D]. 北京: 中国科学院大学(中国科学院工程热物理研究所), 2020.
[11] 黄孟璇. 基于神经网络与遗传算法的压气机正问题优化设计研究[D]. 南京, 南京航空航天大学, 2018.
[12] 费腾, 季路成, 周玲. 神经网络模型在压气机通流特性分析中的应用[J]. 航空动力学报, 2022, 37(6): 1260-1272.
[13] 韩昌富, 刘波, 张博涛. 损失及落后角代理模型在多级轴流压气机特性预测中的应用[J]. 推进技术, 2020, 41(7): 1493-501.
[14] 朱智富, 马朝臣, 张志强, 等. 车用涡轮增压器喘振判断方法的研究[J]. 内燃机工程, 2010, 31(4): 59-62+68.
[15] 谢卫红, 周进, 王毅. 高压比离心压气机气动特性研究[J]. 机械工程与自动化, 2018(2): 32-34+37.