体积对轴流风机瞬态性能影响的建模与验证

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Dai Yuchen, Song Manxiang, Jin Donghai, G. Xingmin, Liu Xiaoheng
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引用次数: 1

摘要

自1976年Greziter教授首次提出预测压缩系统动态行为的理论模型以来,体积效应对压气机流动不稳定性的贡献得到了广泛的研究,但体积效应对压气机加减速性能的作用却没有受到太多关注。因此,本文从Greitzer集总参数法出发,结合发动机实际仿真部件对Greitzer模型进行改进,建立了考虑压气机体积效应的发动机瞬态仿真模型(简称非定常模型)。在实际涡扇发动机上进行了加减速瞬态试验,验证了非定常模型的正确性。与不考虑压气机体积效应(称为准稳态模型)的瞬态仿真相比,仿真结果与实验数据更加吻合,证实了在发动机瞬态建模中引入压气机体积效应的重要性。并通过压气机进出口质量流量曲线进一步解释了非定常模型与准定常模型偏差的原因。研究结果可为发动机瞬态模型的发展提供参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modeling and validation of the volume effect on the axial fan transient performance
Abstract Since Professor Greziter first proposed a theoretical model to predict the dynamic behavior of a compression system in 1976, the contribution of the volume effect to compressor flow instabilities has been widely studied, but the role of volume effect on the compressor performance during acceleration and deceleration has not received much attention. Therefore, starting from the Greitzer lumped parameter approach and integrating with real engine simulated components to improve the Greitzer’s model, an engine transient simulation model accounting for the compressor volume effect (referred to as the unsteady model) is developed in this paper. Based on a real turbofan engine, transient examination comprising acceleration and deceleration has been conducted for the validation of the unsteady model. The simulation results show better agreement with the experimental data compared with the transient simulation without considering the compressor volume effect (referred to as the quasi-steady model), which confirms the importance of introducing the compressor volume effect into the engine transient modeling. And the cause of the deviation between unsteady model and quasi-steady model are further explained by the compressor inlet and outlet mass flow curve. The results may further contribute to the development of engine transient model.
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来源期刊
International Journal of Turbo & Jet-Engines
International Journal of Turbo & Jet-Engines 工程技术-工程:宇航
CiteScore
1.90
自引率
11.10%
发文量
36
审稿时长
6 months
期刊介绍: The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines. The International Journal of Turbo & Jet Engines is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.
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