基于AMESim的某型发动机燃油调节器液压延迟器仿真分析  

Hydraulic Retarder for an Aero-engine Fuel Controller Based on AMESim Simulation

作　　者：乔云 冯茵 高若延 林文 QIAO Yun;FENG Yin;GAO Ruoyan;LIN Wen(AECC Xi'an Areo-engine Control Technology Co.,Ltd.,Xi'an,Shaanxi Province,710077 China)

机构地区：[1]中国航发西安航空动力控制科技有限公司,陕西西安710077

出　　处：《科技创新导报》2020年第33期1-3,55,共4页Science and Technology Innovation Herald

摘　　要：液压延迟装置是液压控制系统的重要组成部分。以某型发动机燃油调节器的液压延迟器为研究对象,运用AMESim建模仿真软件,建立了液压延迟器仿真模型,研究分析液压延迟器驱动力矩的决定因素和极限值。液压延迟器的驱动力矩在极限值范围内决定于负载的大小,层板对液压延迟器驱动力矩的稳态无影响,只影响动态响应时间。Hydraulic retarder is an essential part of hydraulic control system.This paper takes the hydraulic retarder of a certain type of aero-engine fuel regulator as the object of study,builds the simulation model of the hydraulic retarder using the AMESim modeling simulation software,and studies determinants and limit values of the driving moment of the hydraulic retarder.The driving moment of the hydraulic retarder is determined by the load in the limit values.The laminate has no effect on the steady state of the hydraulic retarder,only affects the dynamic response time.

关 键 词：航空发动机 燃油调节器 液压延迟器 AMESIM 驱动力矩 

分 类 号：V235[航空宇航科学与技术—航空宇航推进理论与工程]