Thermodynamic study of an adiabatic piston engine with heat recovery for aeronautical application

2000 ◽  
Author(s):  
Roberto Andriani ◽  
Liliana Ferri ◽  
Umberto Ghezzi
Keyword(s):  
Heat Recovery ◽  
Thermodynamic Study ◽  
Piston Engine ◽  
Adiabatic Piston

Thermodynamic study on the effect of cold and heat recovery on performance of liquid air energy storage

2018 ◽  
Vol 221 ◽  
pp. 86-99 ◽  
Author(s):  
Xiaodong Peng ◽  
Xiaohui She ◽  
Lin Cong ◽  
Tongtong Zhang ◽  
Chuan Li ◽  
...  
Keyword(s):  
Energy Storage ◽  
Heat Recovery ◽  
Thermodynamic Study

Thermodynamic Study of Influence of Steam Injection in Combustion Chamber of Simple Gas/Steam Combined Cycle

2004 ◽  
Author(s):  
J. P. Yadav ◽  
Onkar Singh
Keyword(s):  
Combustion Chamber ◽  
Gas Turbine ◽  
Steam Generator ◽  
Heat Recovery ◽  
Steam Injection ◽  
Combined Cycle ◽  
Thermodynamic Study ◽  
Specific Work ◽  
Heat Recovery Steam Generator ◽  
Topping Cycle

Steam injection is seen as one of the popular ways for power augmentation by number of turbine manufacturers and number of steam injected turbines such as Allison 501-K, GE LM 2500, and LM5000 are already in use. This paper presents the thermodynamic study of influence of steam injection in combustion chamber of topping cycle in a simple gas / steam combined cycle power plants upon the efficiency and specific work out put of topping cycle, bottoming cycle and combined cycle. The simple gas / steam combined cycle power plant configuration considered for the study has topping cycle gas turbine with film cooled stages employing air / steam as coolants and single pressure steam generation in the heat recovery steam generator (HRSG). Air for cooling has been bled out from compressor depending upon the requirement and the steam requirement as coolant is met from the steam generated in heat recovery steam generator (HRSG). Thermodynamic analysis of the simple combined cycle configuration considered has been completed with the variation in various parameters such as cycle pressure ratio, type of coolant used for gas turbine stages, mass fraction of the steam being injected in combustion chamber of topping cycle. Results obtained have been plotted suitably for the critical evaluation of influence of one parameter upon the other.

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