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contributor authorA. S. Feitelberg
contributor authorM. A. Lacey
date accessioned2017-05-08T23:56:30Z
date available2017-05-08T23:56:30Z
date copyrightJuly, 1998
date issued1998
identifier issn1528-8919
identifier otherJETPEZ-26782#502_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120398
description abstractThe General Electric Company has developed and successfully tested a full-scale, F-class (2550°F combustor exit temperature), rich-quench-lean (RQL) gas turbine combustor, designated RQL2, for low heating value (LHV) fuel and integrated gasification combined cycle applications. Although the primary objective of this effort was to develop an RQL combustor with lower conversion of fuel bound nitrogen to NOx than a conventional gas turbine combustor, the RQL2 design can be readily adapted to natural gas and liquid fuel combustion. RQL2 is the culmination of a 5 year research and development effort that began with natural gas tests of a 2” diameter perforated plate combustor and included LHV fuel tests of RQL1, a reduced scale (6” diameter) gas turbine combustor. The RQL2 combustor includes a 14” diameter converging rich stage liner, an impingement cooled 7” diameter radially-stratified-quench stage, and a backward facing step at the entrance to a 10” diameter film cooled lean stage. The rich stage combustor liner has a novel double-walled structure with narrow circumferential cooling channels to maintain metal wall temperatures within design limits. Provisions were made to allow independent control of the air supplied to the rich and quench/lean stages. RQL2 has been fired for almost 100 hours with LHV fuel supplied by a pilot scale coal gasification and high temperature desulfurization system. At the optimum rich stage equivalence ration NOx emissions were about 50 ppmv (on a dry, 15 percent O2 basis), more than a factor of 3 lower than expected from a conventional diffusion flame combustor burning the same fuel. With 4600 ppmv NH3 in the LHV fuel, this corresponds to a conversion of NH3 to NOx of about 5 percent. As conditions were shifted away from the optimum, RQL2 NOx emissions gradually increased until they were comparable to a standard combustor. A chemical kinetic model of RQL2, constructed from a series of ideal chemical reactors, matched the measured NOx emissions fairly well. The CO emissions were between 5 and 30 ppmv (on a dry, 15 percent O2 basis) under all conditions.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe GE Rich-Quench-Lean Gas Turbine Combustor
typeJournal Paper
journal volume120
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2818173
journal fristpage502
journal lastpage508
identifier eissn0742-4795
keywordsGas turbines
keywordsCombustion chambers
keywordsFuels
keywordsEmissions
keywordsDesign
keywordsCombustion
keywordsNatural gas
keywordsFuel gasification
keywordsNitrogen
keywordsWall temperature
keywordsHeating
keywordsIntegrated gasification combined cycle
keywordsDiffusion flames
keywordsMetals
keywordsChannels (Hydraulic engineering)
keywordsTemperature
keywordsCooling
keywordsDesulfurization
keywordsIndustrial research
keywordsFoundry coatings
keywordsHigh temperature AND Coal
treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 003
contenttypeFulltext


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