航空发动机高温部件系统模拟技术
Simulation technique for the high temperature components in aero-engine
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摘要: 对航空发动机高温部件系统模拟技术进行研究,在涡轮等高温部件及其冷却系统组成的流固系统研究中采用整体域划分思路,并对两部分组成的整体域统一求解.将该方法在某模型中进行分析验证,应用到某涡轮系统及周围冷却空气模拟中,并对强弱耦合两种耦合模拟方法的结果进行了比较分析.Abstract: The method to simulate the air system of jet engine was studied,and new approach was applied into the combined fluid area and solid area to predict the characteristic of high temperature components and the cooling air system of jet engine.The conservation equations of solid components and the cooling air system were solved in a coupled manner.The method was validated and then was applied to predict the characteristics of turbine disk in engine,and meanwhile the comparison between the simulated results from the strongly coupled method and the weakly coupled method was worked out.
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Key words:
- jet engine /
- air system /
- simulation /
- coupled /
- turbine /
- improvement
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[1] Schallhorn P A,Hass N E.Forward looking pressure regulator algorithm for improved modeling performance within the generalized fluid system simulation program .Florida USA:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,AIAA Paper 2004-3667,2004. [2] Holt K,Majumdar A.Numerical modeling and test data comparison of propulsion test article helium pressurization system .Huntsville,USA:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,AIAA Paper 2000-3719,2000. [3] TAO Zhi,HOU Shengping.A new approach to simulate the fluid network of unsteady flow //ICHMT International Symposium on Advances in Computational Heat Transfer.Marrakech,Morocco:ICHMT,2008:154-157. [4] 陶智,侯升平.流体网络法在发动机空气冷却系统设计中的应用[J].航空动力学报,2009,24(1):1-6. TAO Zhi,HOU Shengping.Study on application of fluid network to the design of air system in engine[J] .Journal of Aerospace Power,2009,24(1):1-6.(in Chinese) [5] 侯升平,陶智.非稳态流体网络方法在发动机空气冷却系统中的应用[J].航空动力学报,2009,24(3):494-498. HOU Shengping,TAO Zhi.Study on application of unsteady fluid network to the air system in engine[J].Journal of Aerospace Power,2009,24(3):494-498.(in Chinese) [6] 侯升平,陶智.非稳态流体网络模拟新方法及其应用[J].航空动力学报,2009,24(6):1253-1257. HOU Shengping,TAO Zhi.A new simulation approach to the unsteady fluid network and the application [J].Journal of Aerospace Power,2009,24(6):1253-1257.(in Chinese) [7] 侯升平,陶智.流固网络一体化模拟方法探索应用[J].航空动力学报,2010,25(3):509-514. HOU Shengping,TAO Zhi.Simulation approach to the fluid thermal network and the application[J].Journal of Aerospace Power,2010,25(3):509-514.(in Chinese) [8] Miltiadis V P.Feedback control of thermal systems modeled via the network approach[J].Journal of Dynamic Systems,Measurement,and Control,2004,126(3):509-519. [9] Athavale M M,Ho Y H.Analysis of coupled seals,secondary and powerstream flow fields in aircraft and aerospace turbomachines .NASA/CR Paper 2005-212716,2005. [10] Tetlow M R,Evans M E.Monte Carlo analysis for a booster flyback guidance system .Reno,USA:43rd AIAA Aerospace Science Meeting and Exhibit,AIAA Paper 2005-819,2005. [11] Gamble E J,Giel D.Systematic optimization approach for scramjet/ramjet heat exchanger analysis tool (SRHEATTM) .Hartford,USA:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,AIAA Paper 2008-5173,2008. [12] 侯升平.航空发动机空气系统适航性设计改进建议[J].航空标准化与质量,2011,241(1):34-36. HOU Shengping.Design improvement proposal of air system of jet engine based on airworthiness requirement[J].Aeronautic Standardization & Quality,2011,241(1):34-36.(in Chinese)
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