弹用涡喷/涡扇发动机系统效能评估建模与分析  

Modeling and Analysis of System Effectiveness Evaluation of Missile Turbojet/Turbofan Engines

作　　者：李佳妮 屈高敏 冯兴 李继广 邵朋院 谭健 LI Jia-ni;QU Gao-min;FENG Xing;LI Ji-guang;SHAO Peng-yuan;TAN Jian(AECC Hunan Aviation Powerplant Research Institute,Zhuzhou Hunan,412002,China;College of Mechanical&Electrical Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;School of Aircraft Engineering,Xi'an Aeronautical Institute,Xi'an 710077,China)

机构地区：[1]中国航发湖南动力机械研究所,湖南株洲412002 [2]南京航空航天大学机电学院,南京210016 [3]西安航空学院飞行器学院,西安710077

出　　处：《航空发动机》2024年第6期26-31,共6页Aeroengine

基　　金：陕西省自然科学青年基金(2021JQ-858,2021JQ-845);陕西省自然科学基础研究计划(2023-JC-QN-0031)资助。

摘　　要：为了评估弹用涡喷/涡扇发动机的系统效能,采用分层理论构建了一套完整的弹用涡喷/涡扇发动机系统效能评估指标体系以及系统效能评估模型。从可用性、可信性和固有能力等3方面对弹用涡喷/涡扇发动机系统效能体系进行表征,采用X个小项体现3方面的指标,并采用分层理论确定不同指标对发动机效能的影响权重,建立弹用涡喷/涡扇发动机系统效能的评估模型。对现有的8种弹用涡喷/涡扇发动机进行效能定量评估和对比分析。结果表明:涡扇发动机的性能高于涡喷发动机的,推重比和燃油经济性是影响固有能力的重要因素,验证了模型的有效性和可行性。该研究可为未来弹用涡喷/涡扇发动机的新研和改进改型提供了有力的决策支撑。In order to evaluate the system effectiveness of missile turbojet/turbofan engines,a complete set of missile turbojet/turbofan engine system effectiveness evaluation index system and system effectiveness evaluation model were constructed in a hierarchical theory.The system effectiveness of missile turbojet/turbofan engines was characterized by three aspects:availability,dependability,and capability,X sub-items were used to reflect the indexes of the three aspects,Hierarchy theory was used to determine the influence weights of different indexes to the engine effectiveness,and the model for missile turbojet/turbofan engine system effectiveness evaluation was established.Quantitative evaluation and comparative analysis of the effectiveness of 8 existing turbojet/turbofan engines were conducted.The results show that the effectiveness of the turbofan engine is greater than that of the turbojet engine,the thrust to weight ratio and fuel economy are important factors affecting capability,verifying the effectiveness and feasibility of the model.This study can provide strong decision support for future new programs and improvement programs for missile turbojet/turbofan engines.

关 键 词：弹用涡喷发动机 弹用涡扇发动机 指标体系 系统效能评估 定量分析 

分 类 号：V235.1[航空宇航科学与技术—航空宇航推进理论与工程]