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Turbine Project Data
Advanced Combustion System for Next Generation Gas Turbine

Advanced Combustion System for Next Generation Gas Turbine
DE- FC26-01NT41020

Next-generation gas turbines will operate at higher pressure ratios and hotter turbine inlet temperatures – conditions that will tend to increase nitrogen oxide emissions. To conform to future air quality requirements, lower-emitting combustion technology will be required.

In October 2000, General Electric was selected to develop a prototype combustor that will reduce smog-causing nitrogen oxide emissions well below current systems. The goal is to cut emissions by 50 percent or more compared to state-of-the-art lean premixed gas turbine combustors. Currently General Electric's dry low-NOx combustion technology, which the company pioneered in the early 1990s, has been installed on more than 250 gas turbines. The most advanced dry low-NOx designs reduce nitrogen oxide emissions to less than 10 parts per million (on a dry, 15 percent oxygen basis).

General Electric researchers will evaluate several combustor concepts at small scales and use them to refine computer models and generate a design database. From this data, prototype combustors, employing new designs, will be built and evaluated over a variety of conditions. The best design will be selected for full-scale design evaluation.

PROJECT INFORMATION
Project ID: DE- FC26-01NT41020
Performer Contact: General Electric Corporate Research and Development, Niskayuna NY
Alok M. Srivastava (518) 387-7535
srivastava@cre.ge.com
SCNG Contact: Norman T. Holcombe (412) 386-4557
norman.holcombe@netl.doe.gov
Project Timeline: Start: 06/11/01
End:  12/30/03
Total Project Cost:
Total: $2,447,889
DOE Share: $1,182,510
Non-DOE: $1,265,379
Additional Information: General Electric Gas Turbines
Final Report