Performance and Emission Characteristics of Alcohol/Jet A Blends in a Small-Scale Gas Turbine Engine

Author(s):  
Carlos Mendez ◽  
Ramkumar Parthasarathy ◽  
Subramanyam 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.


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

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

2021 ◽  
pp. 5-16
Author(s):  
Yu.М. Temis ◽  
A.V. Solovjeva ◽  
Yu.N. Zhurenkov ◽  
A.N. Startsev ◽  
M.Yu. Temis ◽  
...  

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

1979 ◽  
Author(s):  
M. G. Coombs

This paper describes the development of a silicon carbide heat exchanger for the CCPS-40-1 closed-cycle gas turbine engine. This effort was part of a program to explore the use of closed-cycle power systems for utilities. The program consists of heat exchanger design, the development of a design approach for large ceramic components, the establishment of a material data base, and the development of the required fabrication technology. Small-scale ceramic heat exchangers were operated at material temperatures up to 2300 F.


Author(s):  
Valentyn Barannik ◽  
Maksym Burlaka ◽  
Leonid Moroz ◽  
Abdul Nassar

Central-station power plants (CSPP) are the main provider of energy today. In the process of power generation at central-power stations, about 67% of primary energy is wasted. Distributed cogeneration or combined heat and power (CHP) systems are an alternative to central-station power plants. In these systems, an electrical generation system located in a residence or at a commercial site consumes natural gas to generate electricity locally and then the exhaust heat is utilized for local heating needs (in contrast to being wasted at central-stations). Microturbines offer a number of potential advantages compared to other technologies for small-scale power generation. For example, compact size and low-weight leading to reduced civil engineering costs, a small number of moving parts, lower noise and vibration, multi-fuel capabilities, low maintenance cost as well as opportunities for lower emissions. Inverter generators allow using micro-turbines of different shaft rotation speed that opens opportunities to unit optimization at off-design modes. The common approach to predict the off-design performance of gas turbine unit is the mapping of the compressor and the turbine separately and the consequent matching of common operation points. However, the above-mentioned approach might be rather inaccurate if the unit has some secondary flows. In this article an alternative approach for predicting off-design performance without using component maps is presented. Here the off-design performance is done by direct calculation of the components performances. On each off-design mode, the recalculation of the characteristic of all scheme components, including a compressor, gas turbine, combustor, recuperator and secondary flow system is performed. The different approaches for obtaining the performance at off-design modes considering the peculiarities of the gas turbine engine are presented in this paper.


Sign in / Sign up

Export Citation Format

Share Document