燃油总管智能试验系统设计与应用  

Design and application of the intelligent test system for fuel manifold

作　　者：侯俊林 周家林 黄德润 关猛 许承慧 HOU Jun-lin;ZHOU Jia-lin;HUANG De-run;GUAN Meng;XU Cheng-hui(AECC Sichuan Gas Turbine Establishment,Mianyang 621000,China)

机构地区：[1]中国航发四川燃气涡轮研究院,四川绵阳621000

出　　处：《燃气涡轮试验与研究》2021年第6期26-30,36,共6页Gas Turbine Experiment and Research

摘　　要：针对航空发动机燃烧室燃油总管试验器传统手动试验模式与高效率、低强度、自动化、智能化试验要求日益凸显的矛盾,采用智能油路匹配技术、智能阀门控制技术、试验状态模拟技术以及测控一体化技术,设计开发了一套燃油总管智能试验系统。经调试,系统各项技术指标均达到设计要求。该系统现已成功应用于多种型号航空发动机燃油总管试验,系统功能完善、运行状态良好,能够很好满足航空发动机科研试验需求且具有十分广泛的应用前景。There is a growing contradiction between the traditional manual test mode and the high efficien⁃cy,low intensity,automation and intelligent test requirements for the fuel manifold tester of areo-engine.Using intelligent fuel route matching technology,intelligent valve control technology,test state simulation technology and measurement and control integrated technology,a set of fuel manifold intelligent test system was developed.After commissioning,all indexes of the system met the design requirements.The system now has been successfully applied to several types of areo-engine fuel manifold tests.The system function is great,and the operation condition is good.So the system could meet the test requirements of aero-engine and has a very wide range of application prospects.

关 键 词：航空发动机 燃烧室 燃油总管 智能试验 专家系统 测控一体化 

分 类 号：V232.2[航空宇航科学与技术—航空宇航推进理论与工程]