燃气涡轮试验与研究
燃氣渦輪試驗與研究
연기와륜시험여연구
GAS TURBINE EXPERIMENT AND RESEARCH
2011年
3期
45-49
,共5页
民用发动机%增压压气机%试验件%结构设计
民用髮動機%增壓壓氣機%試驗件%結構設計
민용발동궤%증압압기궤%시험건%결구설계
civil aero-engine%booster%rig%structure design
主要介绍了某增压压气机试验件结构设计,包括了重点考虑的关键技术和解决方法,以及试验件首次总装中出现的问题和解决措施。该增压压气机试验件圆满完成试验验证,全面达到设计性能指标,填补了我国增压压气机设计技术的空白,为民用发动机的研制提供了必要的技术储备。
主要介紹瞭某增壓壓氣機試驗件結構設計,包括瞭重點攷慮的關鍵技術和解決方法,以及試驗件首次總裝中齣現的問題和解決措施。該增壓壓氣機試驗件圓滿完成試驗驗證,全麵達到設計性能指標,填補瞭我國增壓壓氣機設計技術的空白,為民用髮動機的研製提供瞭必要的技術儲備。
주요개소료모증압압기궤시험건결구설계,포괄료중점고필적관건기술화해결방법,이급시험건수차총장중출현적문제화해결조시。해증압압기궤시험건원만완성시험험증,전면체도설계성능지표,전보료아국증압압기궤설계기술적공백,위민용발동궤적연제제공료필요적기술저비。
This paper introduced the key technologies and solutions to the design of a LPC rig structure, as well as problems and debugging process in the first assembly of test specimen. The test demonstration was successfully accomplished and designing performance indices were reached. This filled the gap of LPC design technology in china, providing a solid and reliable technology base for the development of civil aero-engines.