高性能经济可承受先进加力燃烧室技术GOTChA分解  

GOTChA analysis of high performance affordable advanced afterburner technology

作　　者：邓爱明 王中豪 张军华 胡斌[1] 赵庆军[1,2,3] 黄勇 DENG Ai-ming;WANG Zhong-hao;ZHANG Jun-hua;HU Bin;ZHAO Qing-jun;HUANG Yong(Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China;University of Chinese Academy of Sciences,Beijing 100049,China;Key Laboratory of Light-duty Gas-turbine,Chinese Academy of Sciences,Beijing 100190,China;Beihang University,Beijing 100191,China)

机构地区：[1]中国科学院工程热物理研究所,北京100190 [2]中国科学院大学,北京100049 [3]中国科学院轻型动力重点实验室,北京100190 [4]北京航空航天大学,北京100191

出　　处：《燃气涡轮试验与研究》2019年第5期53-57,共5页Gas Turbine Experiment and Research

基　　金：国家重点研发计划(2016YFB0901402);航空动力基金(No.6141B090312)

摘　　要：为加强加力燃烧室技术方案论证,明确加力燃烧室研究内容,提出了加力燃烧室技术的综合评价指标。采用敏感度分析方法定量分析了加力燃烧室工作参数对发动机性能的影响。建立了加力燃烧室三个阶段的技术指标体系,给出了高性能经济可承受先进加力燃烧室技术GOTChA分解图,明确了加力燃烧室研发面临的技术挑战及需要的方法。研究结果可用于指导加力燃烧室技术方案论证,以增强专项计划组织效率,规范项目管理工作。In order to enhance the validation of afterburner concept and determine definite research contents,comprehensive evaluation index of afterburner was proposed.Using sensitivity method,the impact of afterburner parameters on engine performance was quantitatively analyzed.Afterburner technology index system of three stages was built and the GOTChA breakdown drawings of high performance affordable advanced afterburner were also given out.The technology challenges and necessary methods for afterburner development were identified.The study results could be provided as guideline for afterburner technology concept validation in order to increase special plan organization efficiency and normalize program management.

关 键 词：航空发动机 加力燃烧室 评价指标 项目管理 GOTChA VAATE 涡轮基组合循环 

分 类 号：V232[航空宇航科学与技术—航空宇航推进理论与工程]