Abstract

A commercially available natural gas fueled gas turbine engine was operated on hydrogen. Three sets of fuel injectors were developed to facilitate stable operation while generating differing levels of fuel∕air premixing. One set was designed to produce near uniform mixing while the others have differing degrees of nonuniformity. The emission performance of the engine over its full range of loads is characterized for each of the injector sets. In addition, the performance is also assessed for the set with near uniform mixing as operated on natural gas. The results show that improved mixing and lower equivalence ratio decrease NO emission levels as expected. However, even with nearly perfect premixing, it is found that the engine, when operated on hydrogen, produces a higher amount of NO than when operated with natural gas. Much of this attributed to the higher equivalence ratios that the engine operates on when firing hydrogen. However, even the lowest equivalence ratios run at low power conditions, higher NO was observed. Analysis of the potential NO formation effects of residence time, kinetic pathways of NO production via NNH, and the kinetics of the dilute combustion strategy used are evaluated. While no one mechanism appears to explain the reasons for the higher NO, it is concluded that each may be contributing to the higher NO emissions observed with hydrogen. In the present configuration with the commercial control system operating normally, it is evident that system level effects are also contributing to the observed NO emission differences between hydrogen and natural gas.

Highlights

  • Gas turbine engines designed to operate on various fuel stocks are available commercially

  • At full power, the engine primary zone equivalence ratio when operated on hydrogen is much higher than it is for natural gas

  • Even at the very low equivalence ratios found at low power, the NO levels are still higher than they are for natural gas

Read more

Summary

INTRODUCTION

Gas turbine engines designed to operate on various fuel stocks are available commercially. Operate the MTG on a varying mixture of natural gas and hydrogen at full load to measure the effects on stack emission levels. The insert extends inside the injector from the exit plane to the point of fuel injection This insert contains one 1.78 cm diameter center hole in which all of the fuel and most of the air is mixed and released to the combustion chamber. The wide hydrogen stability limits allow the reaction to be sustained at much lower equivalence ratios (and correspondingly lower temperatures) than natural gas (as low as 0.09 vs 0.48 for natural gas).[7] To take advantage of this attribute, the air flow into the injectors was increased, resulting in equivalence ratios ranging from 0.21 to 0.7 across the 0-60kW power load range.

40 Radial 60kW
Findings
DISCUSSION
CONCLUSIONS
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call