Novel inlet air cooling with gas turbine engines using cascaded waste-heat recovery for green sustainable energy

Energy ◽  
2015 ◽  
Vol 93 ◽  
pp. 770-785 ◽  
Author(s):  
Yousef S.H. Najjar ◽  
Ahmad M. Abubaker ◽  
Ahmad F.S. El-Khalil
Author(s):  
Dariusz Kozak ◽  
Paweł Mazuro

Current commercial and heavy-duty powertrains are geared towards emissions reduction. Energy recovery from exhaust gases has great potential, considering the mechanical work to be transferred back to the engine. For this purpose, an additional turbine can be implemented behind a turbocharger; this solution is called turbocompounding (TC). This paper considers the adaptation of turbine wheels and gearboxes of small turboshaft and turbojet engines into a two-stage TC system for a six-cylinder opposed-piston engine that is currently under development. The initial conditions are presented in the first section, while a comparison between small turboshaft and turbojet engines and their components for TC is presented in the second section. Based on the comparative study, a total number of 7 turbojet and 8 turboshaft engines were considered for the TC unit.


2019 ◽  
Vol 55 (1) ◽  
pp. 34-39 ◽  
Author(s):  
A. M. Radchenko ◽  
Y. Zongming ◽  
B. S. Portnoi

The efficiency of deep cooling air at the inlet of gas turbine unite to the temperature of 10 °С by waste heat recovery combined absorption-ejector chiller was analyzed in climatic conditions at Kharkov site, Ukraine, and Beijing site, China, and compared with the moderate cooling to the temperature of 15°C  in  traditional absorption lithium-bromide chiller. The  refrigerant  ejector chiller is chosen  as the most simple and  reliable in operation chiller. It  was used as the low-temperature stage for subcooling the air precooled in absorption lithium-bromide chiller to the temperature about 15 °C. Both waste heat recovery absorption  lithium-bromide chiller and ejector chiller use the  heat of  gas turbine unite exhaust gas to produce a cooling capacity. Air cooling at the inlet of gas turbine unite  was investigated for varying climatic conditions during the year.  The current values of  temperature depression with  cooling  ambient air to different temperatures of 10 °C and 15 °C and corresponding cooling capacities required were calculated. The comparison of  the  effect  due to gas turbine unite inlet air cooling was performed by annual fuel saving and power production growth. With  this the current values of turbine power output increase and specific fuel consumption decrease due to cooling inlet air from current varying ambient  temperatures to the temperatures of 10 °C and 15 °C were calculated.  It  was  shown that annual fuel saving and power production growth have increased by 1,8 times for Kharkov (Ukraine) site climatic conditions and  by 1,6 times  for Beijing (China)  site due  to  deep cooling air to the temperature of 10 °C  by  absorption-ejector chiller as compared with cooling inlet air to the temperature of 15 °C by absorption lithium-bromide chiller.


2021 ◽  
Vol 198 ◽  
pp. 117515
Author(s):  
Chendi Yang ◽  
Yuanyuan Deng ◽  
Ning Zhang ◽  
Xiaopeng Zhang ◽  
Gaohong He ◽  
...  

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