微型燃气轮机稳态控制规律研究与特性计算  

Steady Control Law Research and Performance Calculation of the Micro-turbine Generator

作　　者：王朝蓬[1] 陈玉春[1] 赵强[1] 

机构地区：[1]西北工业大学动力与能源学院,西安710072

出　　处：《科学技术与工程》2010年第9期2255-2259,共5页Science Technology and Engineering

摘　　要：为了研究微型燃气轮机的稳态控制规律及高度气候特性,建立了单轴微型燃气轮机(以下简称微燃机)的性能计算模型,并编制了相应的计算程序。对某型微燃机进行了仿真计算,得到其最大状态、节流状态及慢车状态控制规律,并对该微燃机的气候、高度特性进行了计算分析。通过与试验数据比较,该仿真结果合理,符合实际运行情况,对该微燃机的性能预测和实验有一定的理论指导意义。To research the steady control law and altitude,atmosphere characteristics of micro-turbine generator（MTG）,the simulation model of its performance calculation was built,and compute programs was compiled. Through simulating and calculating of certain MTG,the control laws of its maximum state,throttle state and idle state were obtained,altitude and atmosphere characteristics were calculated and analized. Compared with the testing data,it indicated that the simulation results were reasonable and appliable,and could provide some theoretic guidance to the characteristics anticipation and test of MTG.

关 键 词：微型燃气轮机 控制规律 特性 

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]