整机结构设计的评估方法——结构效率

张大义; 马艳红; 梁智超; 洪杰

整机结构设计的评估方法——结构效率

北京航空航天大学能源与动力工程学院, 北京 100191

基金项目: 航空科学基金(2009ZB51019)

计量
- 文章访问数: 1700
- HTML浏览量: 100
- PDF量: 502
- 被引次数: 0
出版历程
- 收稿日期: 2009-09-14
- 修回日期: 2009-12-14
- 刊出日期: 2010-10-28

Evaluation method on whole engine structural design——structural efficiency

School of Jet Propulsion, Beijng University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 从整机动力学的角度,提出一种量化各种结构改进设计对整机性能收益的评估方法——结构效率,其内涵应当包括发动机质量有效承载项,模态参与项以及变形量协调项,并建立初步分析方法.通过某转子/支承系统的结构优化算例,指出了结构效率在整机结构设计中的优越性,并对结构概率的进一步研究前景和研究重点进行了论述.
- 整机动力学 /
- 结构设计 /
- 振动 /
- 间隙 /
- 结构效率
Abstract: An evaluation method named structural efficiency was presented to quantify the benefit of whole engine structures according to the dynamics.The meaning of structural efficiency encompasses engine strength,modal participation and deformation coordination synthetically.Further corresponding elementary numerical method was given.The advantages of structural efficiency on whole engine design were obtained through a rotor/supporting structural optimization case.Besides,the research prospects and research emphases were discussed in detail.
- dynamics on whole engine /
- structural design /
- vibration /
- clearance /
- structural efficiency

HTML

参考文献(12)

[1]	刘大响,金捷.21世纪世界航空动力技术发展趋势与展望[J].中国工程科学,2004,6(9):1-8.LIU Daxiang,JIN Jie.The devel opment trends and prospect of worldaer opropulsi on technology in the 21st century[J].Engineering Science,2004,6(9):1-8.(in Chinese)
[2]	陈萌,马艳红,刘书国,等.航空发动机整机有限元模型转子动力学分析[J].北京航空航天大学学报,2007,33(9):1013-1016.CHEN Meng,MAY anhong,LIU Shuguo,et al.Rotordynamic analysis of whole aeroengin emodels based on finit eelement method[J].Journal of Beijing University of A eronautics and Astronautics,2007,33(9):1013-1016.(in Chinese)
[3]	Storace A F.Turbineengines tructural efficiency determination[R].AIA A89 2571,1989.
[4]	Li S K,Cheng Y S.Solving the puzzles of structural efficiency[J].European Journal of Operational Research,2007,180(2):713-722.
[5]	Ylvinger S.Indus try performance and structural efficiency measures:solutions to problems in firm models[J].European Journal of Operat ional Research,2000,121(1):164-174.
[6]	朱梓根,李文明,李其汉,等.航空涡喷、涡扇发动机结构设计准则:第六册-转子系统[M].北京:中国航空工业总公司发动机系统工程局,1997:319-323.
[7]	Engin T,Gur M,Schol z R.Effects of tip clearance and impeller geometry on the performance of semi open ceramiccentrifugal fan impellers at elevated temperat ures[J].Experimental Thermal and Fluid Science,2006,30(6):565-577.
[8]	Li S K,Ng Y C.M easuring the productive efficiency of a group of firms[J].International A dvances in Economic Research,1995,1(4):377-390.
[9]	Fre R,Zelenyu k V.On aggregate Farrell efficiencies[J].European Journal of Operational Research,2003,146:615-620.
[10]	Kwak J S,Ahn J,Han J C.Effects of rimlocation,rim height,and tip clearance on the tip and near tip region heatt ransfer of agasturbine blade[J].International Journal of Heat and Mass Trans fer,2004,47(26):5651-5663.
[11]	LI Wei,QIAO Weiyang,SUN Dawei.Tip clearance flows in turbinecas cades[J].Chinese Journal of Aeronautics,2008,21(3):193-199.
[12]	Srini vasan M R,Gopal G.Structural efficiency of incom plete block designs[J].Stati stics&Probability Letters,1996,30(3):211-214.