航空发动机
航空髮動機
항공발동궤
AERO ENGINE
2011年
3期
8-11
,共4页
R0110重型燃气轮机%产品研制%压气机%燃烧室%透平
R0110重型燃氣輪機%產品研製%壓氣機%燃燒室%透平
R0110중형연기륜궤%산품연제%압기궤%연소실%투평
R0110 heavy-duty gas turbine%product development%compressor%combustor%turbine
通过阐述R0110重型燃气轮机的研制过程,总结了该燃气轮机的结构和性能特点。通过对各主要部件的设计、分析计算、试验研究,积累了大量的设计、试验和调试经验,解决了研发过程中所遇到的难点,初步掌握了重型燃气轮机研发的关键技术,基本建立了E+级重型燃气轮机研发设计平台,为重型燃气轮机的系列化发展以及合成气燃气轮机研制奠定了坚实的基础。
通過闡述R0110重型燃氣輪機的研製過程,總結瞭該燃氣輪機的結構和性能特點。通過對各主要部件的設計、分析計算、試驗研究,積纍瞭大量的設計、試驗和調試經驗,解決瞭研髮過程中所遇到的難點,初步掌握瞭重型燃氣輪機研髮的關鍵技術,基本建立瞭E+級重型燃氣輪機研髮設計平檯,為重型燃氣輪機的繫列化髮展以及閤成氣燃氣輪機研製奠定瞭堅實的基礎。
통과천술R0110중형연기륜궤적연제과정,총결료해연기륜궤적결구화성능특점。통과대각주요부건적설계、분석계산、시험연구,적루료대량적설계、시험화조시경험,해결료연발과정중소우도적난점,초보장악료중형연기륜궤연발적관건기술,기본건립료E+급중형연기륜궤연발설계평태,위중형연기륜궤적계렬화발전이급합성기연기륜궤연제전정료견실적기출。
The characteristics of structure and performance were summarized by expatiating the development of R0110 heavy-duty gas turbine.The plenty of experience on design,test and adjusment for every main components was gathered by the design,analysis and experiment research.The difficulty was solved during the development.The key technologies for heavy-duty gas turbine were mastered preliminary.The design platform of E+ class heavy-duty gas turbine was built.It lay a good foundation for the derivative development of heavy-duty gas turbine and the development of gas turbine burning synthesis gas.