
1. 中国民航大学 中欧航空工程师学院,天津,300300
2. 中国民航大学 航空工程学院,天津,300300
3. 中国民航大学 工程技术训练中心,天津,300300
Published:2026
移动端阅览
史磊, 卢志强, 彭鸿博, 等. 风扇叶片颗粒侵蚀特性的多因素分析与模拟[J]. 空气动力学学报, 2026, 44(4): 134−151.
Shi Lei, Lu Zhiqiang, Peng Hongbo, et al. Multi-factor analysis and simulation of particle erosion characteristics of fan blades[J]. 2026, 44(4): 134-151.
史磊, 卢志强, 彭鸿博, 等. 风扇叶片颗粒侵蚀特性的多因素分析与模拟[J]. 空气动力学学报, 2026, 44(4): 134−151. DOI: 10.7638/kqdlxxb-2024.0166
Shi Lei, Lu Zhiqiang, Peng Hongbo, et al. Multi-factor analysis and simulation of particle erosion characteristics of fan blades[J]. 2026, 44(4): 134-151. DOI: 10.7638/kqdlxxb-2024.0166.
为研究风扇叶片在砂尘条件下的颗粒物侵蚀特性,本文以大涵道比涡扇发动机风扇/增压级叶片为研究对象,采用欧拉-拉格朗日法实现颗粒追踪,参考国标规定的标准砂尺寸,分析了不同粒径、浓度、形状因子系数条件下颗粒对风扇叶片的侵蚀特性。结果表明:小粒径侵蚀范围较广,侵蚀程度相对较弱;大粒径侵蚀范围相对较小,但侵蚀程度更为严重;浓度增大时,侵蚀区域虽未有明显变化,但侵蚀速率增加明显,浓度每增加10 mg/m
3
,叶片磨损速率约增加1.35×10
–8
kg/s;形状因子系数减小时,颗粒物跟随性减弱,其侵蚀规律与粒径增大有相似特征,当形状因子系数为0.4时,撞击风扇叶片壁面颗粒数量相较于球形颗粒增加约0.41%,而磨损速率约为球形颗粒工况的1.13倍。本文系统揭示的颗粒多属性侵蚀规律,可为风扇/增压级叶片的抗侵蚀设计与维护策略制定提供理论参考。
The erosion of fan blades by particles such as sand and dust poses a significant threat to flight safety. In the present paper
the particle erosion characteristics of fan/compressor stage blades of a high bypass ratio turbofan engine subjected to sand and dust conditions were investigated in the Eulerian-Lagrangian framework. The effects of particle size
concentration
and shape factor coefficient on the erosion were analyzed. The results indicate that small particles exhibit a relatively wide erosion range but the erosion is comparatively less severe. By comparison
large particles demonstrate a relatively small erosio
n range
but more severe erosion. As the concentration increases
the erosion rate increases significantly while the erosion area remains relatively unchanged. For every increment of 10 mg/m
3
in the concentration
the blades’ wear rate increases by about 1.35 × 10
–8
kg/s. As the shape factor coefficient decreases
the following performance of particles weakens
yielding a variation trend of the erosion pattern similar to that observed with increasing particle size. In particular
compared to spherical particles
when the shape factor coefficient is 0.4
there is a mild increase of approximately 0.41% in the number of particles impinging on the fan blade surface and a considerable increase of 13% in the wear rate. The systematic revelation of the erosion patterns influenced by multiple particle attributes in this study can provide a theoretical reference for the anti-erosion design and maintenance strategy development of fan/booster stage blades.
Tabakoff W. Review: turbomachinery performance deterioration exposed to solid particulates environment[J]. Journal of Fluids Engineering, 1984, 106(2): 125−134. doi: 10.1115/1.3243088
Shi L, Guo S H, Yu P, et al. A review on leading-edge erosion morphology and performance degradation of aero-engine fan and compressor blades[J]. Energies, 2023, 16(7): 3068. doi: 10.3390/en16073068
Finnie I. Erosion of surfaces by solid particles[J]. Wear, 1960, 3(2): 87−103. doi: 10.1016/0043-1648(60)90055-7
Finnie I. Some reflections on the past and future of erosion[J]. Wear, 1995, 186: 1−10. doi: 10.1016/0043-1648(95)07188-1
Grant G, Tabakoff W. Erosion prediction in turbomachinery resulting from environmental solid particles[J]. Journal of Aircraft, 1975, 12(5): 471−478. doi: 10.2514/3.59826
Tabakoff W, Kotwal R, Hamed A. Erosion study of different materials affected by coal ash particles[J]. Wear, 1979, 52(1): 161−173. doi: 10.1016/0043-1648(79)90206-0
Tabakoff W, Lakshminarasimha A N, Pasin M. Simulation of compressor performance deterioration due to erosion[J]. Journal of Turbomachinery, 1990, 112(1): 78−83. doi: 10.1115/1.2927424
Saxena S, Jothiprasad G, Bourassa C, et al. Numerical simulation of particulates in multi-stage axial compressors[C]//ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition, 2016. doi: 10.1115/GT2016-57917
Ghenaiet A. Predicting dust erosion in a counter-rotating fan[C]//Proc of the Volume 6: Education; Electric Power; Energy Storage; Fans and Blowers, London, United Kingdom. American Society of Mechanical Engineers, 2024: V006T10A004. doi: 10.1115/gt2024-121816
Ghenaiet A. Modeling and simulation of sand particle trajectories and erosion in a transonic fan stage[J]. Journal of Turbomachinery, 2025, 147(7): 071012. doi: 10.1115/1.4066986
Ghenaiet A. Simulation of particle-laden flows and erosion in an axial fan stage considering the relative position of the blades[J]. The Aeronautical Journal, 2024, 128(1325): 1379−1416. doi: 10.1017/aer.2024.45
Blinov V L, Zubkov I S, Bogdanets S V, et al. Studies of erosive wear of the blading in axial compressors of gas turbines (review)[J]. Thermal Engineering, 2023, 70(6): 430−442. doi: 10.1134/S0040601523060022
Sun Haiou, Wang Meng, Wang Zhongyi, et al. Numerical research on two-phase flow and erosion characteristic of axial compressor[J]. Journal of Harbin Engineering University, 2018, 39(2): 310−316(in Chinese). doi: 10.11990/jheu.201605105
Li Chao, Bin Guangfu, Li Jian, et al. Influence of sand particle size on the erosive wear of compressor blade in an aero-turboshaft engine[J]. Journal of Mechanical Engineering, 2022, 58(19): 180−190(in Chinese). doi: 10.3901/JME.2022.19.180
Li C, Bin G F, Li J, et al. Erosion wear characteristics of the aero-compressor blades in full speed range[J]. Powder Technology, 2023, 418: 118227. doi: 10.1016/j.powtec.2023.118227
Xu Qiannan, Hu Feng, Xiao Youhong, et al. Analysis of dynamic characteristics of sand particles in air intake and compressor cascade of aero-engine[J]. Journal of Aerospace Power, 2021, 36(8): 1776−1782(in Chinese). doi: 10.13224/j.cnki.jasp.20210803
Cai L X, He Y, Hou Y F, et al. Research on particle motion and erosion characteristics in the blade passage of multistage axial compressors[C]// ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition, Rotterdam, Netherlands. 2022. doi: 10.1115/GT2022-82354
Yang P P, Yue W H, Chen A H, et al. Influence of SiO 2 and Al 2 O 3 particles on erosion wear of aero-compressor blades[J ] . Wear, 2023, 530: 204992. doi: 10.1016/j.wear.2023.204992
Yang P P, Li C, Yue W H, et al. Study on erosion wear characteristics of aero-compressor blades considering distortion degree[J]. Tribology International, 2023, 189: 108895. doi: 10.1016/j.triboint.2023.108895
Lu Zhiqiang, Shi Lei, Peng Hongbo, et al. Particulate erosion wear of fan rotor blades with different leading edge morphology[J]. Science Technology and Engineering, 2024, 24(22): 9654−9663(in Chinese). doi: 10.12404/j.issn.1671-1815.2304541
Cui Zhiwen, Zhao Lihao. Reviews on alignment of non-spherical particles in wall-bounded turbulence[J]. Acta Aerodynamica Sinica, 2021, 39(3): 99−108,I0003(in Chinese). doi: 10.7638/kqdlxxb-2021.0045
Lu Xianmin, Yang Jianzhi, Gu Hailin, et al. Study on drag characteristics of an ellipsoidal particle under wall constraint[J]. Acta Aerodynamica Sinica, 2024, 42(3): 19−29(in Chinese). doi: 10.7638/kqdlxxb-2023.0061
Lei Yinghaonan, Lei Sanhui, Zhang Shenghao, et al. Numerical study on compressible gas-solid two-phase flow based on a particle solver implemented in NNW-PHengLEI[J]. Acta Aerodynamica Sinica, 2023, 41(12): 37−47(in Chinese). doi: 10.7638/kqdlxxb-2022.0161
Li Yang, Xia Zhenhua. A neutrally buoyant finite-size spherical particle in three-dimensional lid-driven cavity flow[J]. Acta Aerodynamica Sinica, 2022, 40(3): 109−119(in Chinese). doi: 10.7638/kqdlxxb-2020.0435
Shi Lei, Guo Shuhan, Ma Pengyu, et al. Multi-objective optimization remodeling of eroded leading edge of supersonic fan blade[J]. Journal of Aerospace Power, 2025, 40(6): 330−342(in Chinese). doi: 10.13224/j.cnki.jasp.20220936
Peng Hongbo, Xue Bowei, Shi Lei, et al. Re-modeling optimization design of leading edge of titanium alloy fan blade[J]. Science Technology and Engineering, 2022, 22(23): 10301−10309(in Chinese). doi: 10.3772/j.issn.1002-0470.2023.11.008
Huang Hao, Feng Zhiwei, Ma Likun, et al. Effects of particle parameters on performance of axisymmetric supersonic gas-solid two-phase flow nozzle[J]. Journal of Propulsion Technology, 2023, 44(8): 48−55(in Chinese). doi: 10.13675/j.cnki.tjjs.22010045
Zeng Fei, Song Yuqin. Temperature of particles with different diameters along turbine flow path and impingement characteristics on turbine vanes and blades[J]. Journal of Propulsion Technology, 2020, 41(8): 1797−1806(in Chinese). doi: 10.13675/j.cnki.tjjs.190821
Yang Xiaojun, Liu Wenbo, Hu Yingqi, et al. Numerical simulation of particle deposition characteristics of high pressure turbine blades[J]. Journal of Propulsion Technology, 2022, 43(11): 164−175(in Chinese). doi: 10.13675/j.cnki.tjjs.210516
Finnie I, McFadden D H. On the velocity dependence of the erosion of ductile metals by solid particles at low angles of incidence[J]. Wear, 1978, 48(1): 181−190. doi: 10.1016/0043-1648(78)90147-3
Oka Y I, Okamura K, Yoshida T. Practical estimation of erosion damage caused by solid particle impact[J]. Wear, 2005, 259(1-6): 95−101. doi: 10.1016/j.wear.2005.01.039
Grant G, Tabakoff W. An experimental investigation of the erosive characteristics of 2024 aluminum alloy[R]. 1973.
Lin Jianzhong, Liang Xinnan, Zhao Bolong. Study on the wear characteristics of the centrifugal impellers with gas-solid two-phase flow[J]. Fluid Machinery, 1994, 22(1): 12−16(in Chinese). doi: CNKI:SUN:LTJX.0.1994-01-002
Li Qing, Tu Guohua, Li Tingting, et al. Particle solver in compressible high enthalpy flow(Part 1): the theoretical equations of point particle laden flow[J]. Acta Aerodynamica Sinica, 2023, 41(8): 71−86(in Chinese). doi: 10.7638/kqdlxxb-2022.0053
Mei Dan, Xing Futang. Numerical simulation research on erosive problem of gas-solid two phase flow fan[J]. Fluid Machinery, 2007, 35(10): 25−28(in Chinese). doi: 10.3969/j.issn.1005-0329.2007.10.006
Zhao Jingyu. Investigations of particle deposition mechanism on the flat plate wall with film cooling holes[D]. Xi'an: Northwestern Polytechnical University, 2017(in Chinese). doi: CNKI:CDMD:1.1018.791650
Wu He, Hao Zihan, Yang Xing, et al. Numerical study on coupling effects of particle deposition and film cooling over flat plate surfaces[J]. Journal of Aerospace Power, 2024, 39(5): 107−118(in Chinese). doi: 10.13224/j.cnki.jasp.20220462
Menter F R. Review of the shear-stress transport turbulence model experience from an industrial perspective[J]. 2009, 23(4): 305−316. doi: 10.1080/10618560902773387
Yu Hongjun. Analysis of "Service guide of general specification for aircraft turbojet turbofan turboprop and turboshaft engines"[J]. Aeronautic Standardization Quality, 2006(4): 20−24(in Chinese). doi: 10.3969/j.issn.1003-6660.2006.04.008
LV J H. Military helicopters with sand and dust environments—Introduction of the national military standard military helicopter sand and dust prevention requirements[C]// The 7th National Helicopter Annual Conference. Shenzhen: Chinese Society of Aeronautics and Astronautics, 2024: 2−4(in Chinese).
Li Zhendong, Xu Lei, Bao Shiyi. Numerical simulation research for the effect of particle shape on the erosion wear in elbow[J]. Chinese High Technology Letters, 2023, 33(11): 1202−1212(in Chinese). doi: 10.3772/j.issn.1002-0470.2023.11.008
0
Views
0
下载量
0
CSCD
Publicity Resources
Related Articles
Related Author
Related Institution
京公网安备11010802024621