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1种新型燃油分配方案设计
引用本文:吴吉麟,陈斐,朱佳慧,李明磊,金林山.1种新型燃油分配方案设计[J].航空发动机,2020,46(3):54-58.
作者姓名:吴吉麟  陈斐  朱佳慧  李明磊  金林山
作者单位:中国航发控制系统研究所,江苏无锡214063,中国航发控制系统研究所,江苏无锡214063,无锡市运河实验中学,江苏无锡214000,中国航发控制系统研究所,江苏无锡214063,中国航发控制系统研究所,江苏无锡214063
基金项目:航空动力基础研究项目资助
摘    要:针对航空发动机分级燃烧燃油分配的高精度、变比例需求,提出了1种基于主、副油路分路计量的新型燃油分配设计方案,并对该方案进行了理论分析以及仿真和试验验证。结果表明:该方案的燃油分配精度高,燃油分配比例调节灵活,可以满足发动机日益复杂的低污染设计和控制的需求;在主、副油路同时供油时,燃油分配最小比例与泵后压力负相关,与副油路喷嘴节流特性正相关。

关 键 词:燃油分配  分级燃烧  调节器  燃油计量  航空发动机

Design of a New Fuel Distribution Scheme
Authors:WU Ji-lin  CHEN Fei  ZHU Jia-hui  LI Ming-lei  JIN Lin-shan
Institution:(AECC Aero Engine Control System Institute,Wuxi Jiangsu 214063,China;Wuxi Yunhe Experimental Middle School,Wuxi Jiangsu 214100,China)
Abstract:Aiming at the requirement of high precision and variable proportion of fuel distribution in fractional combustion of engine,a new type of fuel distribution design scheme was put forward based on shunt metering of the main and pilot fuel passage,and the theoretical analysis,simulation and test verification of the scheme were carried out.The results show that the fuel distribution accuracy is high and fuel distribution ratio adjustment is flexible of the scheme,which can meet the increasingly complex low emission design and control requirements of the engine.The minimum proportion of fuel distribution is negatively correlated with the pump discharge pressure and positively correlated with the nozzle restriction characteristics of the pilot fuel passage when the main and pilot fuel passage are supplied simultaneously.
Keywords:fuel distribution  fractional combustion  adjuster  fuel metering  aeroengine
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