Combustor development for dual fuel combustion with gas oil and biomass gasification products
暂无分享,去创建一个
A cyclone combustor was designed to enable the use
of dual fuels in small gas turbines. Multiple
tangential inlets enable gasified products of biomass
and gas oil to be introduced separately into the
combustion chamber. An integrated vortex collector
pocket (VCP) was positioned just before a tangential
off take. As the flow moves past the VCP the fine
particles are removed from the flow. The tangential
off take will draw the flow past the VCP and produce
near uniform exit conditions.
Results showed the combustor produced a stable
swirling flame, with good mixing patterns for all
cases, with LCV wood gas, gas oil and when running
with a combination of both fuels. Areas of high
temperature in the combustor were identified, where
refractory material would be needed. The VCP
performance was good, collecting particles below 10-
5m. The tangential off-take from the combustor
potentially decreases the pressure drop across the
system by efficiently funnelling the swirling flow
into a square duct with low losses whilst pro ducing a
near uniform velocity profile. Although not used in
these first trials the addition of an outlet diffuser then
offers potential of reducing the pressure drop by
some 30 to 40%. Maximum pressure drops across the
combustor of 0.1 bar were found which was an
acceptable value for the process. Uniform velocity
and temperature profiles were present at the
combustor exit for all cases with exit temperatures
between 1300 and 1350 K. The modelling shows the
combustor design is appropriate for use with dual
fuels and can change between fuels when running
while still maintaining similar combustion patterns
and stable exit conditions. The use of a VCP in the
combustor removes the finer particles without the
need for a further cyclone separator, which would
increase the pressure drop of the system. The exhaust
gas can be fired directly into an appropriate gas
turbine.
[1] A. F. Al-Shaikhly,et al. Development of a Dual Fuel LBTU Gas/Diesel Burning Combustion System for a 4.2 MW Gas Turbine , 1994 .
[2] C. E. Neilson,et al. LM2500 gas turbine modifications for biomass fuel operation , 1998 .
[3] Alan S. Feitelberg,et al. Design and Performance of Low Heating Value Fuel Gas Turbine Combustors , 1996 .