Performance and emission characteristics of butanol/Jet A blends in a gas turbine engine

2014 ◽  
Vol 118 ◽  
pp. 135-140 ◽  
Author(s):  
C.J. Mendez ◽  
R.N. Parthasarathy ◽  
S.R. Gollahalli
Author(s):  
Carlos J. Mendez ◽  
Ramkumar N. Parthasarathy ◽  
Subramanyam R. Gollahalli

Alcohols serve as an alternate energy resource to the conventional petroleum-based fuels. The objective of this study was to document the performance and emission characteristics of blends of n-propanol and Jet A fuel in a small-scale gas turbine engine. The experiments were conducted in a 30kW gas turbine engine with a single-stage centrifugal flow compressor, annular combustion chamber and a single-stage axial flow turbine. In addition to neat propanol and Jet A fuel, three blends, with 25%, 50% and 75% of propanol by volume, were used as the fuels. The thrust, thrust-specific fuel consumption, and the concentrations of CO and NOx in the exhaust were measured and compared with those measured with Jet A fuel. The engine was operated at the same throttle settings with all the fuels. The operational range of engine rotational speed was shifted downwards with the addition of propanol due to its lower heating value. The thrust specific fuel consumption increased with the addition of propanol, while the CO emission index increased and NOx emission index decreased.


Author(s):  
Iman K. Reksowardojo ◽  
Long H. Duong ◽  
Tatang H. Soerawidjaja ◽  
Tri T.G. Nguyen ◽  
Osamu Fujita ◽  
...  

2010 ◽  
Vol 87 (5) ◽  
pp. 1701-1709 ◽  
Author(s):  
Zehra Habib ◽  
Ramkumar Parthasarathy ◽  
Subramanyam Gollahalli

Author(s):  
Muhammad Hanafi Azami ◽  
Zahid Noorazman ◽  
Mark Savill ◽  
Yi-Guang Li ◽  
Mohd Razi Hilmi

2020 ◽  
Vol ahead-of-print (ahead-of-print) ◽  
Author(s):  
Anderson A. ◽  
Karthikeyan A. ◽  
Ramesh Kumar C. ◽  
Ramachandran S. ◽  
Praveenkumar T.R.

Purpose The purpose of this study is to predict the performance and emission characteristics of micro gas turbine engines powered by alternate fuels. The micro gas turbine engine performance, combustion and emission characteristics are analyzed for the jet fuel with different additives. Design/methodology/approach The experimental investigation was carried out with Jet A-1 fuel on the gas turbine engines at different load conditions. The primary blends of the Jet A-1 fuels are from canola and solid waste pyrolysis oil. Then the ultrasonication of highly concentrated multiwall carbon nanotubes is carried with the primary blends of canola (Jet-A fuel 70%, canola 20% and 10% ethanol) and P20E (Jet-A 70% fuel, 20% PO and 10% ethanol). Findings The consumption of the fuel is appreciable with the blends at a very high static thrust. The 39% reduction in thrust specific fuel consumption associated with a 32% enhance in static thrust with P20E blend among different fuel blends. Moreover, due to the increase in ethanol concentration in the blends PO20E and C20E lead to a 22% rise in thermal efficiency and a 9% increase in higher oxygen content is observed. Practical implications The gas turbine engine emits very low emission of gases such as CO, CO2 and NOx by using the fuel blends, which typically reduces the fossil fuel usage limits with reduced pollutants. Originality/value The emission of the gas turbine engines is further optimized with the addition of hydrogen in Jet-A fuel. That is leading to high specific fuel exergy and owing to the lower carbon content in the hydrogen fuel when compared with that of the fossil fuels used in gas turbine engines. Therefore, the usage of hydrogen with nanofluids was so promising based on the results obtained for replacing fossil fuels.


Author(s):  
Eraldo Cruz dos Santos ◽  
Marco Antônio Rosa do Nascimento

Brazil is the most advanced country in terms of technology, production and use of ethanol as fuel. Alcohol can be obtained from various forms of biomass, being sugarcane a current economic reality. The environmental benefits associated with the use of alcohol are enormous, as approximately 2.3 tons of CO2 are no longer emitted to the atmosphere for each ton of ethanol, without taking into account emissions of other gases such as SO2. Sugarcane is the second largest source of renewable energy in Brazil, with 12.6% of participation in the current energy matrix, considering the ethanol fuel and cogeneration of electricity from sugarcane bagasse. The aim of this work is an experimental analysis of thermal performance/emissions of a 30 kW regenerative cycle gas turbine engine using ethanol as fuel. The tests were carried out in the laboratories of the Federal University of Itajubá – UNIFEI, Brazil, on steady state condition under different load levels, considering the properties of ethanol in compliance with Brazilian legislations. The results shown that there were no significant changes in the thermal performance of the gas turbine engine and the emissions ware a slight increase in CO and a reduction in concentrations of NOx.


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