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论文:2021,Vol:39,Issue(4):858-864 |
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引用本文： |
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郑光华, 水飞, 胡金鑫, 刘鑫, 肖华中. 不同结构探针对压气机进口级流场及测量结果的影响[J]. 西北工业大学学报 |
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ZHENG Guanghua, SHUI Fei, HU Jinxin, LIU Xin, XIAO Huazhong. Effects of probes with different structures on the flow field and measurement results of imported compressors[J]. Northwestern polytechnical university |
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| 不同结构探针对压气机进口级流场及测量结果的影响 |
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| 郑光华1, 水飞1, 胡金鑫1, 刘鑫1, 肖华中2 |
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1. 西北工业大学 动力与能源学院, 陕西 西安 710129;
2. 中国航发湖南动力机械研究所 总体研究部, 湖南 株洲 412002 |
| 摘要: |
| 采用数值模拟的方法，研究了某涡轴发动机压气机进口级流道中2种不同类型的总压探针和总温探针的测量精度以及这两种探针对流场的影响，分析探针在巡航、最大连续、起飞3个典型工作状态下，探针结构以及安装位置对探针测量结果的影响。研究结果表明：发动机进口流量越大，探针的测量误差越大；相较于总温探针，总压探针测量准确度受流量的影响更大；速度均匀度受发动机工况的影响较小，主要与插入的探针结构有关；越靠近支板的总压探针，测量误差越大；探针安装位置对出口处总压损失系数的影响较小。 |
| 关键词:
压气机进口级
总压探针
总温探针
测量误差
速度均匀度
总压损失系数
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| Effects of probes with different structures on the flow field and measurement results of imported compressors |
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| ZHENG Guanghua1, SHUI Fei1, HU Jinxin1, LIU Xin1, XIAO Huazhong2 |
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1. School of Power and Energy, Northwestern Polytechnical University, Xi'an 710129, China;
2. General Research Department, China National Aero-Developmerot, Zhuzhou 412002, China |
| Abstract: |
| In this paper, the measurement accuracy of two different types of total pressure probe and total temperature probe in turboshaft engine compressor inlet channel and the influence of these two probes on the flow field through numerical simulation was studied. At the same time, the influence of the probe structure and installation position on probe measurement results under three typical working conditions of cruise, maximum continuous and takeoff was analyzed. The simulation results showed that the higher the engine inlet flow rate, the greater the measurement error of the probe. Comparing with the total temperature probe, the total pressure probe measurement accuracy is more influenced by the flow rate. The velocity uniformity is less affected by the engine operating conditions and is mainly related to the structure of the inserted probes. The closer the total pressure probe to the support plate, the greater the measurement error. The probe installation position has a small effect on the total pressure loss coefficient at the outlet. |
| Key words:
compressor inlet level
total pressure probe
total temperature probe
measurement error
speed uniformity
total pressure loss coefficient
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| 收稿日期: 2020-11-10
修回日期:
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| DOI: 10.1051/jnwpu/20213940858 |
| 通讯作者:
Email： |
| 作者简介: 郑光华(1978-),西北工业大学副教授,主要从事涡轮叶片新型冷却、涡轮气动热力学研究。
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| 作者相关文章 |
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| 郑光华 在本刊中的所有文章 |
| 水飞 在本刊中的所有文章 |
| 胡金鑫 在本刊中的所有文章 |
| 刘鑫 在本刊中的所有文章 |
| 肖华中 在本刊中的所有文章 |
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参考文献: |
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[1] 王振华,王亮. 航空发动机试验测试技术发展探讨[J]. 航空发动机,2014,40(6):47-51 WANG Zhenhua, WANG Liang. Development of aeroengine testing measurement technology[J]. Aeroengine,2014,40(6):47-51(in Chinese)
[2] 陈光. 航空发动机发展综述[J]. 航空制造技术,2000(6):24-27 CHEN Guang. Survey on aero-engine development[J]. Aeronautical Manufacturing Technology, 2000(6):24-27(in Chinese)
[3] 赵安家. 大气总温测试系统误差对发动机调整与性能影响的研究[J]. 飞机设计,2015,35(6):33-38 ZHAO Anjia. Impact form total temperature test system errors on the adjustment and performance of the engine[J]. Aircaft Design, 2015,35(6):33-38(in Chinese)
[4] 李正. 压气机级间叶型受感部堵塞比对压气机性能的影响[D]. 南京:南京航空航天大学,2012 LI Zheng. Airfoil-probe blockage ratio effects on the performance of compressor[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012(in Chinese)
[5] 杨荣菲,赵建通,向宏辉, 等. 进口探针支杆对1.5级压气机气动性能的影响[J]. 推进技术,2017,38(5):1038-1046 YANG Rongfei, ZHAO Jiantong, XIANG Honghui. Effects of Inlet probe support on aerodynamic performance of 1.5-stage compressor[J]. Journal of Propulsion Technology, 2017, 38(5):1038-1046(in Chinese)
[6] 张伟昊,杨伟平,曹保武, 等. 屏蔽式总温探针流动与换热分析[J]. 航空科学技术,2018,29(7):67-72 ZHANG Weihao, YANG Weiping, CAO Baowu, et al. Flow and heat transfer analysis of shielded total temperature probe[J]. Aviation Science and Technology, 2018, 29(7):67-72(in Chinese)
[7] 王肖,惠呈程,吕文召, 等. 亚声速条件下总压探针堵塞效应的数值研究[C]//中国航天第三专业信息网第四十届技术交流会暨第四届空天动力联合会议, 2019:10 WANG Xiao, HUI Chengcheng, LYU Wenzhao, et al. Numerical study on the plugging effect of the total pressure probe under subsonic speed[C]//China Aerospace Third Professional Information Network's 40th Technical Exchange Conference and the Fourth Aerospace Power Joint Conference Proceedings, 2019:10(in Chinese)
[8] VENKATESWARAN S. Experimental study of casing boundary layers in a multistage axial compressor[J]. Journal of Fluids Engineering, 1991,113(2):102-110
[9] WALL M M. Proximity effects on the measuring accuracy of wedge probes[C]//Proceeding of the Fourth Asian Congress of Fluid Mechanics, 1989:50
[10] 郑光华,王肖,郭林, 等. 亚声速条件下总压探针临壁效应的数值研究[J]. 航空工程进展,2020,11(2):256-263 ZHENG Guanghua, WANG Xiao, GUO Lin, et al. Numerical study on the wall effect of total pressure probe under subsonic speed[J]. Advances in Aeronautical Engineering, 2020, 11(2):256-263(in Chinese) |
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