Gas Turbines - Materials, Modeling and Performance 2015
DOI: 10.5772/59002
|View full text |Cite
|
Sign up to set email alerts
|

The Influence of Inlet Air Cooling and Afterburning on Gas Turbine Cogeneration Groups Performance

Abstract: Gas turbine systems operate on the ideal thermodynamic cycle (consisting in two isentropic and two isobars) represented by Brayton cycle. The real Brayton cycle consists in quasiadiabatic expansion and compression processes, but unisentropic, and the heat transfer processes are not isobar processes, due to flow pressure losses. In addition, the air and hot gases are not perfect gases and not have the same flow rates. Brayton cycle thermal efficiency depends on: compression ratio; ambient temperature; air tempe… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
3
0

Year Published

2016
2016
2021
2021

Publication Types

Select...
5

Relationship

1
4

Authors

Journals

citations
Cited by 5 publications
(3 citation statements)
references
References 9 publications
0
3
0
Order By: Relevance
“…Preliminary experiments on natural gas, performed in COMOTI (Fig. 5) [16], showed a strongly turbulent flame. Thus in the numerical simulations the average temperature of the flue gases on the monitoring plane was compared with the reference temperature of 1043 K.…”
Section: Cfd Settingsmentioning
confidence: 98%
“…Preliminary experiments on natural gas, performed in COMOTI (Fig. 5) [16], showed a strongly turbulent flame. Thus in the numerical simulations the average temperature of the flue gases on the monitoring plane was compared with the reference temperature of 1043 K.…”
Section: Cfd Settingsmentioning
confidence: 98%
“…The combined cycle power plants often use suction air cooling. Using water spray mist for the suction air cooling is simple method and it can obtain high efficiency of air cooling (Jaber, et al, 2007 andBarbu, et al, 2015). The residual water droplet in the suction air causes serious damage to the compressor blade.…”
Section: Introductionmentioning
confidence: 99%
“…Because of the high operating temperatures of gas turbines and the need of an adequate cooling, combustion gases contain about 11-16% oxygen (by volume), which enables additional fuel combustion (post combustion) [1]. The post combustion burner can operate on natural gases as fuel, with exhaust gases from the gas turbine or fresh air.…”
Section: Introductionmentioning
confidence: 99%