航空重油活塞发动机标定系统设计  

Design of Calibration System for Aircraft Heavy Fuel Piston Engine

作　　者：刘杰[1,2] 黄维强 闫研 韩志强 LIU Jie;HUANG Weiqiang;YAN Yan;HAN Zhiqiang(Key Laboratory of Fluid and Power Machinery of Ministry of Education,Xihua University,Chengdu,Sichuan,610039,China;Key Laboratory of Vehicle Measurement,Control and Safety of Sichuan Province)

机构地区：[1]西华大学流体及动力机械教育部重点实验室,四川成都610039 [2]汽车测控与安全四川省重点实验室

出　　处：《小型内燃机与车辆技术》2023年第6期72-77,共6页Small Internal Combustion Engine and Vehicle Technique

基　　金：国家自然科学基金资助项目(51776177,51876145)。

摘　　要：针对航空重油活塞发动机的开发需要,设计了航空重油活塞发动机标定系统,具体包括标定系统硬件设计、通讯协议设定、上位机设计和下位机设计4个部分,系统开发完成后对功能进行验证。验证实验证明,标定系统能够针对航空重油活塞发动机多种工况需求,高效精确地完成参数监控和数据标定,完全能够满足实验项目开发需求。Aiming at the development needs of aircraft heavy fuel piston engine,the calibration system of aircraft heavy fuel piston engine is designed,including hardware design,communication protocol setting,upper computer design and lower computer design.After the development of the system,the function is verified.The verification experiment proves that the calibration system can effectively and accurately complete the parameter monitoring and data calibration according to the requirements of various working conditions of aircraft heavy fuel piston engine,which can fully meet the development requirements of the experimental project.

关 键 词：标定系统 航空重油 参数监控 数据标定 

分 类 号：V233.74[航空宇航科学与技术—航空宇航推进理论与工程]