期刊文献+

变循环发动机重量预估方法研究 被引量:3

Method Research of Variable Cycle Engine Weight Estimate
下载PDF
导出
摘要 重量是航空发动机设计必须控制的一个重要指标,重量预估在航空发动机结构方案设计阶段不可或缺。根据发动机部件法的思想,建立了基于统计的各部件气动—结构经验关系模型,结合变循环发动机结构设计关键几何参数和部件气动热力参数,发展了变循环发动机重量预估方法,采用C++语言开发了变循环发动机重量预估程序,计算了双外涵变循环发动机重量和尺寸。结果表明此方法能够预估双外涵变循环发动机重量,重量尺寸误差满足飞机和发动机工程需求。 Weight is an important control indicator of aircraft engine design, and weight estimate is unavoidable in the initial design phase of aeroengine. According to the idea of engine element-method, statistic -based aerodynamic and structure empirical relatio^hip of every assembly models were built. Combined with the key geometric parameters and aerothermodynamics parameters of assembly of variable cycle engine structure design, variable cycle engine weight estimate method was developed. Based on C++ program language variable cycle engine weight forecast program was developed and the weight and size of a double bypass variable cycle engine was calculated. Results show that the method could estimate the double bypass variable cycle engine weight and error could satisfy the plane and engine engineering demands.
出处 《机械设计与制造》 北大核心 2014年第8期15-18,共4页 Machinery Design & Manufacture
关键词 变循环 双外涵 涡扇发动机 部件法 重量预估 Variable Cycle Double Bypass Turbofan Engine Element-Method Weight Estimate
  • 相关文献

参考文献5

二级参考文献32

  • 1方昌德.变循环发动机[J].燃气涡轮试验与研究,2004,17(3):1-5. 被引量:65
  • 2方昌德.变循环发动机及其关键技术[J].国际航空,2004(7):49-51. 被引量:18
  • 3李志刚,陶增元,李剑.变几何部件对发动机性能的影响分析[J].航空发动机,2005,31(2):6-7. 被引量:10
  • 4Fishbaeh L H,Stitt L E,Stone J R,et al. NASA research in supersonic propulsion A decade of progress[R]. AIAA-82-1048.
  • 5Rallabhandi S K, Mavris D N. Simultaneous airframe and propulsion cycle optimization for supersonic aircraft design [R]. AIAA-2008-143.
  • 6French M W,Allen G L. NASA VCE test bed engine aerodynamic performance characteristics and results[R]. AIAA-81-1594.
  • 7Vdoviak J W, Knott P R, Ebacker J A. Aerodynamic/acoustic performance of YJ101/double bypass VCE with eoannualr plug nozzle[R]. NASA CR-159869,1981.
  • 8Vdoviak J W,Ebacker J A. VCE test bed engine for supersonic cruise research[C]//NASA Langley Research Center Supersonic Cruise Res.United States: NASA, 1979: 347-356.
  • 9Morris S J,Coen P G,Geiselhart K A. Performance potential of an advanced technology Mach 3 turbojet engine installed on a conceptual high speed civil transport[R]. NASA Technical Memorandum, November 4144,1989.
  • 10Krebs J N, Allan R D. Supersonic propulsion--1970 to 1977[R]. AIAA-77-832.

共引文献79

同被引文献15

引证文献3

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部