Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

High pressure test results of a catalytically assisted ceramic combustor for a gas turbine

Journal Article · · Journal of Engineering for Gas Turbines and Power
DOI:https://doi.org/10.1115/1.2818490· OSTI ID:678042
; ; ;  [1]; ;  [2]
  1. Central Research Inst. of Electric Power Industry, Yokosuka, Kanagawa (Japan)
  2. Kansai Electric Power Co., Inc., Amagasaki, Hyogo (Japan)
A catalytically assisted ceramic combustor for a gas turbine was designed to achieve low NOx emission under 5 ppm at a combustor outlet temperature over 1300 C. This combustor is composed of a burner system and a ceramic liner behind the burner system. The burner system consist of 6 catalytic combustor segments and 6 premixing nozzles, which are arranged in parallel and alternately. The ceramic liner is made up of the layer of outer metal wall, ceramic fiber, and inner ceramic tiles. Fuel flow rates for the catalysts and the premixing nozzles are controlled independently. Catalytic combustion temperature is controlled under 1000 C, premixed gas is injected from the premixing nozzles to the catalytic combustion gas and lean premixed combustion over 1300 C is carried out in the ceramic liner. This system was designed to avoid catalytic deactivation at high temperature and thermal and mechanical shock fracture of the honeycomb monolith of catalyst. A combustor for a 10 MW class, multican type gas turbine was tested under high pressure conditions using LNG fuel. Measurements of emission, temperature, etc. were made to evaluate combustor performance under various combustion temperatures and pressures. This paper presents the design features and the test results of this combustor.
Sponsoring Organization:
USDOE
OSTI ID:
678042
Report Number(s):
CONF-980615--
Journal Information:
Journal of Engineering for Gas Turbines and Power, Journal Name: Journal of Engineering for Gas Turbines and Power Journal Issue: 3 Vol. 121; ISSN JETPEZ; ISSN 0742-4795
Country of Publication:
United States
Language:
English

Similar Records

High pressure test results of a catalytic combustor for gas turbine
Journal Article · Wed Jul 01 00:00:00 EDT 1998 · Journal of Engineering for Gas Turbines and Power · OSTI ID:665320

On-engine evaluation of emission characteristics of a variable geometry lean-premixed combustor
Journal Article · Tue Dec 31 23:00:00 EST 1996 · Journal of Engineering for Gas Turbines and Power · OSTI ID:483752

Test results of low NO[sub x] catalytic combustors for gas turbines
Journal Article · Fri Jul 01 00:00:00 EDT 1994 · Journal of Engineering for Gas Turbines and Power; (United States) · OSTI ID:6960167