A full states performance model for aero engine
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摘要: 采用基于脊背特性的压气机和涡轮部件性能的参数表示方法建立了航空燃气涡轮发动机全状态性能仿真计算模型.使用该模型对某单轴涡喷发动机的地面节流特性进行了计算模拟,并且与传统的发动机性能模型的计算结果进行了对比.结果表明:主要截面参数的平均相对误差不超过07%,说明该模型在慢车以上转速与传统模型具有相同的计算精度.使用该模型同时对该单轴涡喷发动机的空中风车状态、地面起动加速的全过程、以及减速全过程进行了数值模拟,验证了该模型的全状态性能仿真能力,计算结果定性地符合发动机在各个不同工作状态的物理特征及变化趋势.Abstract: A full states performance simulation model for aero engine was established by using the parametric representation based on the backbone characteristics of compressor and turbine. Part loading performance of a turbojet engine at sea level static condition was simulated through the model. Compared with the traditional model, results showed the average errors of the main parameters were no more than 07%, indicating the full states model had the same precision as the traditional model above idle speed. The simulations for windmill state, ground starting and acceleration to maximum power, and deceleration from maximum power to zero were performed respectively by using the full states model. The ability of simulating full states performance of engine was verified. The results are qualitatively consistent with the operative characteristics and physical laws of the engine.
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[1] 郭秉衡,许彪,张登洲.双转子涡喷发动机风车特性的计算与分析[J].航空学报,1995,16(5):528-533. GUO Bingheng,XU Biao,ZHANG Dengzhou.Calculation and analysis of windmilling characteristics of twinspool turbojet engine[J].Acta Aeronautica et Astronautica Sinica,1995,16(5):528-533.(in Chinese) [2] 彭靖波,谢寿生.基于RBF神经网络的压气机特性仿真[J].推进技术,2006,27(1):30-32. PENG Jingbo,XIE Shousheng.Compressor characteristics simulation based on RBF neural network[J].Journal of Propulsion Technology,2006,27(1):30-32.(in Chinese) [3] 周文祥,黄金泉,窦建平.涡扇发动机部件级起动模型[J].航空动力学报,2006,21(2):248-253. ZHOU Wenxiang,HUANG Jinquan,DOU Jianping.Development of componentlevel startup model for a turbofan engine[J].Journal of Aerospace Power,2006,21(2):248-253.(in Chinese) [4] 周文祥,黄金泉.涡扇发动机高空起动模型研究[J].航空动力学报,2007,22(8):1384-1390. ZHOU Wenxiang,HUANG Jinquan.Research on the startup model of turbofan engine at high altitude[J].Journal of Aerospace Power,2007,22(8):1384-1390.(in Chinese) [5] Bretschneider S,John R.Method of extrapolating low speed compressor curves based on improved similarity laws[R].Montreal:ASME Turbo Expo,2015. [6] Saxton W R.A new method to control turbofan engine starting by varying compressor surge vale bleed[D].Blacksburg,Virginia,USA:Virginia Polytechnic Institute and State University,2001. [7] Chappel M A,McLaughlin P W.Approach to modeling continuous turbine engine operation from startup to shutdown[J].Journal of Propulsion and Power,1993,9(3):466-471. [8] Agrawal R K,Yunis M.A generalized mathematical model to estimate gas turbine starting characteristics[J].Journal of Engineering for Gas Tubines and Power,1982,104(1):194-201. [9] ZHAO Qishou.Calculation of windmilling characteristics of turbojet engines[J].Journal of Engineering for Power,1981,103(1):1-12. [10] Jones G,Pilides P,Curnock B.Compressor extrapolation of compressor characteristics to the lowspeed region for subidle performance Modeling[R].Amsterdam:ASME Turbo Expo,2002. [11] Choi M S,Kang I S,Lim J S,et al.Analysis of windmilling characteristics for a twinspool turbofan engine[R]Singapore City:ASME Aisa Congress and Exhibition,1997. [12] 王占学,王永杰,乔渭阳,等.涡扇发动机低转速部件特性扩展和风车状态性能模拟[J].推进技术,2006,27(2):146-149. WANG Zhanxue,WANG Yongjie,QIAO Weiyang,et al.Extrapolating component maps into the low speed and simulation of windmilling performance of turbofan engine[J].Journal of Propulsion Technology,2006,27(2):146-149.(in Chinese) [13] 杨欣毅,沈伟,刘海峰,等.一种弹用涡喷发动机风车起动数值仿真方法[J].航空动力学报.2010,25(8):1776-1782. YANG Xinyi,SHEN Wei,LIU Haifeng,et al.Numerical method for modeling missile turbojet engine windmill start process[J].Journal of Aerospace Power,2010,25(8):1776-1782.(in Chinese ) [14] 黄向华,郑绪生.基于逐级叠加法的航空发动机起动模型研究[J].航空学报,2005,26(5):540-544. HUANG Xianghua,ZHENG Xusheng.Research on startup model of aircraft engine based on stagestacking method[J].Acta Aeronautica et Astronautica Sinica.2005,26(5):540-544. [15] 陈玉春,王朝蓬,黄兴鲁,等.功率提取法在涡喷发动机起动特性模拟及控制规律设计中的应用[J].航空动力学报,2010,25(6):1277-1283. CHEN Yuchun,WANG Zhaopeng,HUANG Xinglu,et al.Application of power extraction method in starting process simulation and control law design of turbojet engines[J].Journal of Aerospace Power,2010,25(6):1277-1283.(in Chinese) [16] 雷积红,陈策,李军,等.基于BP神经网络的涡扇发动机部件特性研究[J].燃气涡轮试验与研究,2003,16(4):15-17. LEI Jihong,CHEN Ce,LI Jun,et al.A study of turbofan component characteristic based on back propagation network[J].Gas Turbine Experiment and Research,2003,16(4):15-17.(in Chinese) [17] 时瑞军,周剑波,张秋贵,等.单轴涡喷发动机起动过程数学建模研究[J].燃气涡轮试验与研究,2010,23(3):1-4. SHI Ruijun,ZHOU Jianbo,ZHANG Qiugui,et al.Analysis on the modeling method of single spool turbojet engine startup process[J].Gas Turbine Experiment and Research,2010,23(3):1-4.(in Chinese) [18] Converse G L,Giffin R G.Extended parametric representation of compressor fans and turbines :Volume ⅠCMGEN users manual[R].NASACR-174645,1984. [19] Converse G L.Extended parametric representation of compressor fans and turbines:Volume Ⅱ PART users manual[R].NASACR-174646,1984. [20] Converse G L.Extended parametric representation of compressor fans and turbines:Volume Ⅲ MODFAN users manual[R].NASACR-174647,1984. [21] Jones G B.Performance modeling of windmilling gas turbines[D].Cranfield,Bedfordshire,UK:Cranfield University,2001.
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