Research About Smart Power Plant for Chinese Heavy-Duty Gas Turbine Development and Application

Author(s):  
Guo-Gang Shu ◽  
Peng-Fei Gu ◽  
Xue-Fei Zhai ◽  
Bao Heming ◽  
Cao Ying
Author(s):  
Federico Bonzani

The IGCC power plant of Ferrera Erbognone will be the first real commercial power plant in Italy to be operated without taking into account the high benefits once available according to the national law (CIP6/1992) specifically dealing with recovery fuel usage alternative to natural gas. The syngas will be provided by the nearby refinery using tar as main feedstock. Furthermore, according to the demands of the refinery it will be possible in the gasifier island to separate hydrogen in variable quantity from the syngas thus giving a high variability composition as output fuel. Also, if the maximum quantity of hydrogen will be separated, an integration with natural gas will be performed in order to get the maximum power output of the power plant. As a consequence, the syngas burner has been designed taking into account all the fuel characteristics depending on the different composition carried out. According to these, the burner has been optimised in order to fit the various syngas blends to be fuelled when running the engine. In order to verify the modifications carried out the burner has been tested both at atmospheric and full engine conditions since the NOx requirements for this project are the more stringent experienced with respect to the past projects (NOx to be below 25 ppm). During these test the main aspect to be in investigated have been: a) Minimum load when feeding the gas turbine with syngas. b) NOx emission from 60% load up to base load. c) Change over from natural gas to syngas and vice versa. The tests have been performed successfully: commissioning on site will start on November 2005. The paper describe the design and the testing phase highlighting the main features of the burner and the fuel system with respect to the plant requirements.


Author(s):  
Lawrence Willey ◽  
Michael Davi ◽  
Gordon Smith ◽  
John Almstead ◽  
Brahim Richani ◽  
...  

Quantification and measurement of startup and shutdown (SU/SD) emissions for heavy-duty combustion gas turbines, along with many associated significant issues, are examined in this paper. Included are the regulatory drivers that have prompted increased requests to Original Equipment Manufacturers (OEMs) from gas turbine operators, now required to account for SU/SD emissions in their power plant air permit applications. Also discussed are the complex array of influence parameters for the most popular gas turbine combustors relative to power plant installation and operability characteristics. These issues are presented along with additional background to support a recommended total mass of pollutant per SU/SD event criteria. The complexity of the Continuous Emissions Monitoring Systems (CEMS) equipment used to accurately measure transient emissions is also examined. This assessment of CEMS is designed to help gas turbine users and regulators understand the basic difficulties and complications in formulating which—if any—SU/SD emissions compliance criteria should be included in air permits.


2017 ◽  
Author(s):  
Andrew Detor ◽  
◽  
Richard DiDomizio ◽  
Don McAllister ◽  
Erica Sampson ◽  
...  

2011 ◽  
Vol 84-85 ◽  
pp. 259-263
Author(s):  
Xun Liu ◽  
Song Tao Wang ◽  
Xun Zhou ◽  
Guo Tai Feng

In this paper, the trailing edge film cooling flow field of a heavy duty gas turbine cascade has been studied by central difference scheme and multi-block grid technique. The research is based on the three-dimensional N-S equation solver. By way of analysis of the temperature field, the distribution of profile pressure, and the distribution of film-cooling adiabatic effectiveness in the region of trailing edge with different cool air injection mass and different angles, it is found that the impact on the film-cooling adiabatic effectiveness is slightly by changing the injection mass. The distribution of profile pressure dropped intensely at the pressure side near the injection holes line with the large mass cooling air. The cooling effect is good in the region of trailing edge while the injection air is along the direction of stream.


Author(s):  
I. Ispas ◽  
H. J. Zollinger

To evaluate the potential of the compressor of Sulzer’s Typ 3 gas turbine, a series of engine tests was analyzed with two computer codes. The comparison between measured and calculated performance map are given in the paper. The design goal was to find modifications, which can be applied easily to already operating engines. The simplest option-increase of shaft speed with the existing blades-would have caused high loss due to increased tip Mach number. The calculation revealed, that a newly designed first rotor blade is an appropriate modification to increase massflow and efficiency. No further change is required, because the calculations indicate, that all subsequent stages operate at near optimum incidence. The calculations were confirmed experimentally. The paper presents the new rotor blade and its influence on the compressor calculated and measured performance.


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