Volume 28 Issue 9
Sep.  2013
Turn off MathJax
Article Contents
MA Qian-rong, WU Hu, LIU Tao, ZHOU Wen-xiang. Correction method of influence of simulation bias on performance of turboshaft engine test in ATF[J]. Journal of Aerospace Power, 2013, 28(9): 1997-2002.
Citation: MA Qian-rong, WU Hu, LIU Tao, ZHOU Wen-xiang. Correction method of influence of simulation bias on performance of turboshaft engine test in ATF[J]. Journal of Aerospace Power, 2013, 28(9): 1997-2002.

Correction method of influence of simulation bias on performance of turboshaft engine test in ATF

  • Received Date: 2013-03-29
  • Publish Date: 2013-09-28
  • Simulation bias can cause the performance difference during turboshaft engine tests in altitude test facility(AFT).Based on numerical simulation and tests research of a turboshaft engine,a performance correction method of combining the resemble conversion with small deviation analysis was put forward.The results show that the differences of output power and specific fuel consumption were drop from about 3.0% obtained by the resemble conversion to about 1.0%,so this combination method is reasonable and scientific for correcting the influence of simulation bias on the engine performance.

     

  • loading
  • [1]
    Volponi A J.Gas turbine parameter corrections[J].Journal of Engineering for Gas Turbines and Power,1999,121(4):613-621.
    [2]
    Ushiyma I.Theoretically estimating the performance of gas turbines under varying atmospheric conditions[J].Journal of Engineering for Power,1976,98(1):69-78.
    [3]
    Kyritsis V E,Pilidis P.An analytical approach for gas turbine parameter corrections[J].ASME Paper GT2008-50716,2008.
    [4]
    Casoni A,Colitto N,Elliott J,et al.Corrected parameter control for two shaft gas turbines[J].Proceedings of the ASME,Turbo Expo,2004,4(2):741-748.
    [5]
    刘大响.试车环境对发动机性能的影响及修正方法[M].北京:航空工业出版社,1989.
    [6]
    张逸民,陈大光,刘大响,等.航空发动机试车性能修正[R].四川江油:航空工业部第六二四研究所,1983.
    [7]
    Attia M S,Eustace R W.The predicted and measured effects of increasing back pressure on the performance of a turboshaft engine[J].ASME Paper GT2010-22323,2010.
    [8]
    黄开明,黄金泉,任丹,等.涡轴发动机性能参数的等效换算[J].航空动力学报,2010,25(9):2036-2040. HUANG Kaiming,HUANG Jinquan,REN Dan,et al.Performance parameter equivalent correction of turbo-shaft engine[J].Journal of Aerospace Power,2010,25(9):2036-2040.(in Chinese)
    [9]
    黄开明.涡轴发动机性能与控制规律仿真及试验研究[D].南京:南京航空航天大学,2009. HUANG Kaiming.Simulation and experiment research of turbo-shaft engine performance and control law[D].Nanjing:Nanjing Univeristy of Aeronautics and Astronautics,2009.(in Chinese)
    [10]
    涅恰耶夫.航空动力装置控制规律与特性[M].单凤桐,程振海,译.北京:国防工业出版社,1999.
    [11]
    廉小纯,吴虎.航空燃气轮机原理[M].北京:国防工业出版社,2000.
    [12]
    契尔凯茲.航空涡轮喷气发动机原理和计算中小偏差法的应用[M].杨克立,译.北京:国防工业出版社,1959.
    [13]
    宋江涛,雷勇.基于小偏差法的航空发动机气路故障诊断方法[J].科学技术与工程,2008,8(6):1501-1503. SONG Jiangtao,LEI Yong.Fault diagnosis of aeroengine gas path based on small deviation method[J].Science Technology and Engineering,2008,8(6):1501-1503.(in Chinese)
    [14]
    吴学辉,李志刚,陶增元.参数小偏差对某高推重比航空发动机性能的影响分析[J].航空动力学报,2005,20(6):1028-1031. WU Xuehui,LI Zhigang,TAO Zengyuan.Analysis of the effects of parameter small deviations on a high thrust-weight ratio aeroengine performance[J].Journal of Aerospace Power,2005,20(6):1028-1031.(in Chinese)
    [15]
    国防科学技术工业委员会.GJB4879-2003航空涡轮喷气和涡轮风扇发动机高空模拟试验要求[S].北京:国防科学技术工业委员会,2003.
    [16]
    杜鹤龄.航空发动机高空模拟[M].北京:国防工业出版社,2002.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1627) PDF downloads(1607) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return