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某型间冷燃气轮机热力计算方法研究
引用本文:郑培英,聂海刚,高凤树.某型间冷燃气轮机热力计算方法研究[J].航空发动机,2008,34(1):13-15,52.
作者姓名:郑培英  聂海刚  高凤树
作者单位:沈阳发动机设计研究所,沈阳,110015
摘    要:为提高航改燃气轮机的性能,以现有的简单循环的某型燃气轮机为基础开展了间冷循环研究:采用牛顿迭代法和循环迭代算法,分别对以该燃气轮机核心机为基础发展的间冷循环燃气轮机进行了热力计算和比较,并进行了该间冷循环燃气轮机的设计点方案论证。

关 键 词:燃气轮机  间冷循环  性能计算
修稿时间:2007年8月9日

Thermal Dynamic Calculation Method on an Intercooled Gas Turbine
Authors:ZHENG Pei-ying  NIE Hai-gang  GAO Feng-shu
Abstract:Based on an exiting single cycle gas turbine,the intercooled cycle was investigated to improve the performance of the aero-derived gas turbine.The thermal dynamic calculation and comparison were conducted respectively by using Newton iteration method and cyclic iterative method for the intercooled cycle gas turbine derived from the core gas turbine.The design point concept of the intercooled cycle gas turbine was demonstrated.
Keywords:gas turbine  intercooled cycle  performance calculation  
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