期刊文献+

批生产及翻修发动机稳定性检查方法的研究

An Investigation on Compressor Stall Margin Acceptance Test of Production and Overhaul Engine
下载PDF
导出
摘要 在国内外发动机稳定性评定技术的基础上,分析研究了发动机的可用稳定裕度应等于或大于多个降稳因子的需要稳定裕度之和。其中包括批生产和翻修后发动机制造、装配公差对喘振裕度的影响。基于这种认识,参照第三代发动机的使用实践,提出了批生产试车和翻修后发动机试车的失速边界的验收方法。即在畸变条件下发动机在稳定工况及遭遇加速“bodie”加速操作时检查稳定性的方法和验收准则。此外也提出了控制发动机试车质量的技术途径。 based on engine stability assessment at home and abroad, this paper considers the surge margin available equal to or exceed the sum of required surge margins for all instability losses including the influrnce of manufacture and assemble tolerance on engine stability in production and overhaul. Based on this understanding and the practice from third generation engines, this paper suggests a procedure to run engine compressor stall margin acceptance test after production and overhaul. This procedure is a criterion to check and accept engine stability at steady state condition and 'bodie' maneuvers under inlet total pressure distortion condition. In addition, it provides a technique to control the quality of engine test.
出处 《燃气涡轮试验与研究》 2001年第2期26-33,共8页 Gas Turbine Experiment and Research
关键词 航空发动机 稳定性 批生产 评定技术 稳定裕定 装配公差 翻修 engine stability production overhaul
  • 相关文献

参考文献8

  • 1Joseph F. Boytos, etal. J52 - P - 8 Engine Compressor Stall Margin Acceptance Tests, Naval air Systems Command , 1972
  • 2Goldsmith E L, & Seddon J. Practical Intake Aerodynamic Design, Blackwell Scientific Publications. 1993
  • 3Inlet Total- Pressure- Distortion Considerations For gas -Turbine Engines, Aerospace Information Report, air 1419
  • 4Gordon C. Oates, Aircraft Propulsion Systems Technology and Design, AIAA Education series. 1989
  • 5刘大响主编.航空发动机设计手册第7册进排气装置.北京:航空工业出版社,2000
  • 6国标GJB241-87,航空涡轮喷气和涡轮风扇发动机通用规范
  • 7DEF STAN 00-971飞机燃气涡轮发动机通用规程.航空航天工业部第三零一研究所,1993
  • 8(苏)尤.阿.李特维诺夫弗奥.鲍罗维克.航空涡轮喷气发动机的特性和使用性能.北京国防工业出版社,1986

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