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军用航空发动机再制造工程管理的认识与实践 被引量:7

Recognition and practice on remanufacturing engineering management of military aero-engine
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摘要 军用特别是歼击机发动机的设计、制造、维修比其他所有航空发动机都更难掌握,被极少数国家垄断,核心技术概不转让,表现为高风险、高投入、高壁垒、高成本。我国军用航空发动机的设计与制造还没有走出自主研发道路,长期靠测仿与进口满足需求。国内某企业经过二十多年不懈努力,已实现我国所有歼击机发动机(包括在研机使用的发动机)的自主维修,技术、能力、质量、效率、成本等达到或超过引进国水平,从无到有、由弱到强;特别是数十项具有自主知识产权的再制造技术研发与工程化应用,为军用航空发动机自主维修水平的跨越式提升发挥了不可替代的作用。 Design, manufacture and maintenance of military fighter engine are particularly a lot more difficult to learn than those of other military aero-engines. Owing to military aero-engine is monopolized by very few countries and its core technology is never transferred, it features high risk, high investment, high barrier and high cost. Currently, design and manufacture of military aero-engine in China have not reached the level of independent research and development, instead, the method of long-term dependence on copying or import- ing others' military engine is adopted to meet the needs. However, after over twenty years of unremitting efforts of some domestic enterprise, Chinese all fighter engines including engines powered in designing aircraft have completely achieved the level of independent maintenance, whose maintenance technology, ability, quality, efficiency and cost have reached or surpassed those of importing nations, with a change developing from nothing and an improvement from weak to strong. In particular, more than ten projects concerning research and develop- ment of remanufacturing technology and the engineering application with the feature of independent intellectual property rights have promoted leapfrog improvement of Chinese military aero-engine independent maintenance level, whose function cannot be substituted.
作者 向巧
出处 《中国工程科学》 北大核心 2013年第11期67-73,共7页 Strategic Study of CAE
关键词 军用航空发动机 再制造 工程 管理 military aero-engine remanufacturing engineering management
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  • 1LUO R Y, YANG Z, LI L F. Effect of additives on mechanical properties of oxidation - resistance carbon/carbon composite fabricated by rapid CVD method[J] . Carbon, 2000,38:2109 - 2115.
  • 2LUO R Y, LIU T, LI J S, et al. Thermophysical properties of carbon/carbon composites and physical mechanism of thermal expansion and thermal conductivity[J] . Carbon, 2004,42 : 2887 - 2895.
  • 3SCHMIDT DL, DAVIDSON KE, THEIBERT LS. Unique applications of carbon- carbon composite materials[J] . SAMPE J, 1999,35 (3): 27 - 39.
  • 4VAIDYARAMAN S, LACKEY W J, AGRAWAL P K, et al. 1 - D model for forced flow - thermal gradient chemical vapor infiltration process for carbon/carbon composites[J]. Carbon, 1996, 34(9): 1123 - 1133.
  • 5TAINYAN H, CHOUTSU W. Modeling of an improved chemical vapor infiltration process for ceramic composites fabrication[J] . J Am Ceram Soc, 1990; 73(6): 1489 - 1498.
  • 6CURRIER R P. Overlap model for chemical vapor infiltration of fibrous yarns[J] . J Am Ceram Soc, 1990, 73 (8): 2274 - 2282.
  • 7STARR T L. Gas transport model for chemical vapor infiltration[J]. J Mater Res, 1995, 10(9): 2360 - 2366.
  • 8GUPTE S M, TSAMOPOULOS J A. Forced -flow chemical vapor infiltration of porous ceramic materials[J] . J Electroehem Soc, 1990, 137 ( 11 ) : 3675 - 3682.
  • 9项目管理协会.组织级项目管理成熟度模型(OPM3)》[M].吴之明,席相霖,肖文毅,等译.北京:电子工业出版社,2009.
  • 10侯向辉,李贺军,李克智,姜开宇,康沫狂.单向碳/碳复合材料CVI致密化模拟研究[J].复合材料学报,1999,16(2):129-134. 被引量:7

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同被引文献40

  • 1方洪渊,王霄腾,范成磊,杨建国.LF6铝合金薄板平面内环焊缝焊接应力与变形的数值模拟[J].焊接学报,2004,25(4):73-76. 被引量:9
  • 2王宝瑞,雷华东,黄文荣,郭鹏.LF6铝镁合金电子束焊接接头的性能与组织初探[J].现代制造工程,2004(10):59-61. 被引量:3
  • 3何继善,陈晓红,洪开荣.论工程管理[J].中国工程科学,2005,7(10):5-10. 被引量:61
  • 4向巧. 军用航空装备基地级修理柔性化保障模式的构建[J].航空杂志,2011(7):50-51.
  • 5何继善,王孟钧,王青娥. 中国工程管理现状与发展[M]. 北京:高等教育出版社,2013.
  • 6刘云山.增强问题意识坚持问题导向[N].学习时报,2014-05-19.
  • 7Khairiyah Mohd-Yusof, Mahyuddin Arsat,Mohamad Termizi Borhan,Erik de Graaff, Anette Kolmos,Fatin Aliah Phang. Proceedings_PBL Across_Cultures[M]. Aalborg,Denmark, Aalborg University Press,2013.
  • 8秦现生,等.质量管理学[M].第4版,北京:科学出版社,2007:320.
  • 9刘大响,等.航空发动机-飞机的心脏[M].北京:航空工业出版礼,2010.
  • 10向巧.构建新型航空发动机维修工程管理体系[N].中国航空报,2013-10-17.

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