军民两用技术与产品
軍民兩用技術與產品
군민량용기술여산품
Dual Use Technologies & Products
2015年
18期
87-88
,共2页
大涵道比%航空发动机%技术成熟度评估
大涵道比%航空髮動機%技術成熟度評估
대함도비%항공발동궤%기술성숙도평고
high bypass ratio%engine%technology readiness assessment
结合大涵道比发动机研制特点，介绍了大涵道比涡扇发动机技术成熟度评估的方法，分析了关键技术单元选取、细则编制方法、细则满足情况判定方法。为技术成熟度评估在国内大涵道比涡扇发动机的应用方法提供了参考。
結閤大涵道比髮動機研製特點，介紹瞭大涵道比渦扇髮動機技術成熟度評估的方法，分析瞭關鍵技術單元選取、細則編製方法、細則滿足情況判定方法。為技術成熟度評估在國內大涵道比渦扇髮動機的應用方法提供瞭參攷。
결합대함도비발동궤연제특점，개소료대함도비와선발동궤기술성숙도평고적방법，분석료관건기술단원선취、세칙편제방법、세칙만족정황판정방법。위기술성숙도평고재국내대함도비와선발동궤적응용방법제공료삼고。
The method of high bypass ratio turbofan engine technology readiness assessment has been expanded,combined the feature of high bypass ratio engine. Selection of central technology element, compiling of detailed rules and determination of detailed rules satisfaction has been analyzed. The result provides a reference for application on technology readiness assessment of high bypass ratio engine.
