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Article Navigation >  Journal of Traffic and Transportation Engineering  > 2008  >  8(3): 28-32
Rong Xiang, Zuo Hong-fu, Zhang Hai-jun. Control method of time on wing for civil aeroengine[J]. Journal of Traffic and Transportation Engineering, 2008, 8(3): 28-32.
Citation: Rong Xiang, Zuo Hong-fu, Zhang Hai-jun. Control method of time on wing for civil aeroengine[J]. Journal of Traffic and Transportation Engineering, 2008, 8(3): 28-32.
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Control method of time on wing for civil aeroengine

  • School of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, Jiangsu, China

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  • Author Bio:

    Rong Xiang(1979-), male, doctoral student, +86-25-84895772-803, rongxiang@nuaa.edu.cn

    Zuo Hong-fu(1959-), male, PhD, professor, +86-25-84891098, rms@nuaa.edu.cn

  • Received Date: 2007-12-26
  • Publish Date: 2008-06-25
    Abstract
  • In order to apply condition based maintenance (CBM) to control civil aeroengine time on wing (TOW), the features of aeroengine CBM and TOW were discussed, and the proportional intensity model was established to describe the relation among TOW, condition monitoring variables and failure intensity. TOW control limit due to performance deterioration and optimal preventive maintenance (PM) interval under minimizing expected total maintenance cost per unit time were implemented. The operation data of a CF6-80C2A5 engine were studied. It is pointed that the less failure intensity is, the lower TOW control limit is; moreover, the cost rate between PM and corrective maintenance can affect optimal PM interval; sufficient engine operation data are the keys of accurate TOW control, such as engine removal and on wing history records, maintenance cost, requirements of airworthiness and manufacturer, and time limits of life limited parts etc.

     

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    • References(14)
  • [1]
    梁剑. 基于成本优化的民用航空发动机视情维修决策研究[D]. 南京: 南京航空航天大学, 2005.
    [2]
    左洪福, 张海军, 戎翔. 基于比例风险模型的航空发动机视情维修决策[J]. 航空动力学报, 2006, 21(4): 716-721. doi: 10.3969/j.issn.1000-8055.2006.04.018

    Zuo Hong-fu, Zhang Hai-jun, Rong Xiang. Condition based aero-engine maintenance decision method using proportional hazards model[J]. Journal of Aerospace Power, 2006, 21(4): 716-721. (in Chinese) doi: 10.3969/j.issn.1000-8055.2006.04.018
    [3]
    Rong Xiang, Zuo Hong-fu, Zhang Hai-jun, et al. Research on an integrated model-based CBM decision support system for aeroengine[C]//Wang Wen-bin, Jia Xi-sheng, Huang Hong-zhong. Proceeding of the First International Conference on Maintenance Engineering. Beijing: Science Press, 2006: 216-221.
    [4]
    富涛, 许春生. 在翼航空发动机剩余寿命预测[J]. 中国民航飞行学院学报, 2006, 17(3): 18-21. https://www.cnki.com.cn/Article/CJFDTOTAL-MHFX200603004.htm

    Fu Tao, Xu Chun-sheng. Residual life prediction for aero-engine on wing[J]. Journal of Civil Aviation Flight University of China, 2006, 17(3): 18-21. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-MHFX200603004.htm
    [5]
    李建国, 叶新农, 徐可君. 涡扇发动机寿命管理研究[J]. 海军航空工程学院学报, 2005, 20(4): 468-472.

    Li Jian-guo, Ye Xin-nong, Xu Ke-jun. Life management research of military turbofan engine[J]. Journal of Naval Aero-nautical Engineering Institute, 2005, 20(4): 468-472. (in Chinese)
    [6]
    Vittal S, Hajela P, Joshi A. Reviewof approaches to gas tur-bine life management[C]//AIAA. Proceeding of 10 th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. New York: AI AA, 2004: 1-11.
    [7]
    Jiang S T, Landers T L, Rhoads T R. Assessment of repairable-systemreliability using proportional intensity models: a review[J]. IEEE Transactions on Reliability, 2006, 55(2): 328-336. doi: 10.1109/TR.2006.874938
    [8]
    Jiang S T, Landers T L, Rhoads T R. Semi-parametric proportional intensity models robustness for right-censored recurrent failure data[J]. Reliability Engineering and System Safety, 2005, 90(1): 91-98. doi: 10.1016/j.ress.2004.11.017
    [9]
    Percy D F, Kobbacy K A H, Ascher HE. Using proportional-intensities models to schedule preventive-maintenance intervals[J]. I MA Journal of Mathematics Applied in Business and Industry, 1998, 9(3): 289-302.
    [10]
    Naeem M, Singh R, Probert D. Consequences of aero-engine deteriorations for military aircraft[J]. Applied Energy, 2001, 70(2): 103-133. doi: 10.1016/S0306-2619(01)00028-9
    [11]
    Wang Wen-bin, Zhang Wen-juan. A model to predict the residual life of aircraft engines based upon oil analysis data[J]. Naval Research Logistics, 2005, 52(3): 276-284.
    [12]
    Jaw L C. Recent advancementsin aircraft engine health man-agement(EHM)technologies and recommendations for the next step[C]//ASME. Proceeding of Turbo Expo2005: 50th ASMEInternational Gas Turbine & Aeroengine Techni-cal Congress. New York: ASME, 2005: 1-13.
    [13]
    Weckman G R, Shell R L, Marvel J H. Modeling the reliability of repairable systems in the aviationindustry[J]. Computers and Industrial Engineering, 2001, 40(1/2): 51-63.
    [14]
    Guo Huai-rui, Liao Hai-tao, Zhao Wen-biao, et al. A new stochastic model for systems under general repairs[J]. IEEE Transactions on Reliability, 2007, 56(1): 182-188.
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