0
RESEARCH PAPERS: Gas Turbines: Combustion and Fuels

Development of an Aeroderivative Gas Turbine Dry Low Emissions Combustion System

[+] Author and Article Information
G. Leonard, J. Stegmaier

GE Aircraft Engine Business, Cincinnati, OH 45241

J. Eng. Gas Turbines Power 116(3), 542-546 (Jul 01, 1994) (5 pages) doi:10.1115/1.2906853 History: Received March 10, 1993; Online April 24, 2008

Abstract

This paper gives the development status of GE’s new aeroderivative premixed combustion system. This system consists of a new fuel staged annular combustor, compressor rear frame, first-stage turbine nozzle, electronic staging controller, and fuel delivery system. Component test results along with a description of the combustion system are presented. This new system will reduce NOx emissions by 90 percent relative to the original aircraft engine combustion system while maintaining low emissions of CO and UHCs. Tests of a LM6000 gas turbine equipped with the new system are planned for early 1994.

Copyright © 1994 by The American Society of Mechanical Engineers
Your Session has timed out. Please sign back in to continue.

References

Figures

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In