THE INCOMING GAS TEMPERATURE CALCULATION FOR GAS TURBINE OF A LARGE-CAPACITY COMBINED CYCLE UNIT

SHI Yan-zhou1; YANG Guo-rong2; YAO Xiao-lin1; CHEN Xian2; ZHONG Ping1; JIANG Bin31.Xi'an Thermal Power Research Institute Co Ltd

doi:10.19666/j.rlfd.2009.02.005

English Version Reader LoginJournal Login

您当前的位置：

首页 >

文章列表页 >

THE INCOMING GAS TEMPERATURE CALCULATION FOR GAS TURBINE OF A LARGE-CAPACITY COMBINED CYCLE UNIT

更新时间：2025-09-28

- THE INCOMING GAS TEMPERATURE CALCULATION FOR GAS TURBINE OF A LARGE-CAPACITY COMBINED CYCLE UNIT
- Thermal Power Generation Vol. 38, Issue 2, Pages: 17-20(2009)
- 作者机构：
  
  1. 西安热工研究院有限公司
  2. 华能上海燃机发电有限责任公司
  3. 浙江省兰溪市供电局
- 作者简介：
- 基金信息：
- DOI：10.19666/j.rlfd.2009.02.005
  CLC： TK472
- Published：2009
- 稿件说明：
移动端阅览
SHI Yan-zhou1, YANG Guo-rong2, YAO Xiao-lin1, et al. THE INCOMING GAS TEMPERATURE CALCULATION FOR GAS TURBINE OF A LARGE-CAPACITY COMBINED CYCLE UNIT[J]. Thermal power generation, 2009, 38(2): 17-20.
DOI：

SHI Yan-zhou1, YANG Guo-rong2, YAO Xiao-lin1, et al. THE INCOMING GAS TEMPERATURE CALCULATION FOR GAS TURBINE OF A LARGE-CAPACITY COMBINED CYCLE UNIT[J]. Thermal power generation, 2009, 38(2): 17-20. DOI： 10.19666/j.rlfd.2009.02.005.

摘要

燃气轮机燃气透平应运行在设计的进气温度下

以保证燃气轮机热通道部件较长的使用寿命和运行经济性。由于燃气透平进气温度很高且无可靠仪表进行直接测量

因此采用了热平衡方法进行间接计算。经在多台大型燃气-蒸汽联合循环机组性能考核试验中应用证明

使用热平衡方法间接计算燃气透平进气温度切实可行。

Abstract

The gas turbine incoming gas temperature should be maintained at lower than 130 ℃ in operation

so as to ensure longer service life and better economic efficiency of the parts situated in thermal passage of the gas turbine.In view of the incoming gas temperature being too high and still hasn't reliable instrument for directly measuring the said gas temperature

hence

an indirect calculation method of the incoming gas temperature has been carried out by using the heat-balancing method.This method has already used for performance assessment test of many large-capacity combined cycle units.Proving it is reliable and feasible.

关键词

Keywords

references

Views

214

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

STUDY ON VELOCITY UNIFORMITY IN INLET FLUE DUCT OF HEAT RECOVERY BOILER FOR LARGE-SCALE GAS TURBINE

CAUSE ANALYSIS OF REINFORCING WIRES FAILURE FOR INCOMING GAS SAFETY ISOLATING STRAINER OF THE GAS TURBINE

MEASURES FOR REDUCING UNCERTAINTY IN INTEGRATED PERFORMANCE TEST OF COMBINED CYCLE UNIT

HEAT,ELECTRICITY AND COOL TRIPLE CO-GENERATION SCHEME BY USING NATURAL GAS FOR RESIDENTIAL QUATERS AND ANALYSIS OF ITS TECHNOECONOMIC PERFORMANCE

A SUMMARY AND PROSPECTS OF STUDY ON START-UP PROCESS FOR GAS TURBINES

Related Author

ZHAO Jian-yun

PAN Wei

CHI Zuo-he

CHEN Peng

GAN Meng-bi

GAO Yan et al

LIU Xiaohong

YANG Shoumin

Related Institution

Zhejiang University

Hangzhou Boiler Group Co., Ltd

South China University of Technology

Moon Bay Gas Turbine Power Plant

AI问答

⁰