Combustion method and burner for carrying out the method
View Patent ↗In a combustion method, in a burner ( 12, 20 ), a fuel/air mixture flowing through a flow passage ( 13 ) is made to react in a first combustion stage in a catalytic reactor ( 15 ), and downstream of the catalytic reactor ( 15 ) fuel is burnt together with the exhaust gas from the catalytic reactor ( 15 ) in a second combustion stage to form a homogenous flame ( 17 ) by self-ignition. If the fuel from the fuel/air mixture is only partially burnt in the first combustion stage in the catalytic reactor ( 15 ), and the unburnt remainder of the fuel is burnt in the second combustion stage, combustion can be stabilized by virtue of the fact that the fuel-containing exhaust gas from the catalytic reactor ( 15 ), between the outlet of the catalytic reactor ( 15 ) and the homogenous flame ( 17 ) is passed through devices 916, 19 ) which aerodynamically stabilize the homogenous flame ( 17 ).
1. A combustion method, comprising:
reacting a fuel/air mixture flowing through a flow passage in a first combustion stage in a catalytic reactor;
burning fuel downstream of the catalytic reactor together with the exhaust gas from the catalytic reactor in a second combustion stage to form a homogenous flame by self-ignition;
wherein reacting comprises partially burning the fuel from the fuel/air mixture in the first combustion stage in the catalytic reactor, creating an unburnt remainder of the fuel;
wherein the unburnt remainder of the fuel is burned in the second combustion stage; and
passing fuel-containing exhaust gas from the catalytic reactor, between the outlet of the catalytic reactor and the homogenous flame, through devices which aerodynamically stabilize the homogenous flame.
2. The method as claimed in claim 1 , wherein the aerodynamically stabilizing devices comprise vortex generators arranged at the output of the catalytic reactor.
3. The method as claimed in claim 2 , wherein the aerodynamically stabilizing devices comprise a step-like widening in the flow passage arranged between the vortex generators and the homogenous flame.
4. The method as claimed in claim 1 , wherein the exhaust gas at the outlet of the catalytic reactor comprises O 2 , N 2 , CO, CO 2 , H 2 O, and unburnt fuel.
5. The method as claimed in claim 1 , wherein exhaust gas emerges from the catalytic reactor at a flow velocity of less than or equal to 50 m/s.
6. The method as claimed in claim 1 , wherein exhaust gas emerges from the catalytic reactor at a temperature of between 600° C. and 950° C.
7. The method as claimed in claim 1 , further comprising:
guiding fuel past the outside of the catalytic reactor; and
adding said guided fuel to the exhaust gas downstream of the catalytic reactor.
8. The method as claimed in claim 1 , further comprising:
introducing H 2 /CO from a fuel-rich catalytic pilot burner into the medium flowing through the flow passage.
9. A burner useful for carrying out a method as claimed in claim 1 , the burner comprising:
a flow passage;
a catalytic reactor in the flow passage for catalyzing a fuel/air mixture when flowing through the flow passage; and
means for aerodynamically stabilizing a homogenous flame which forms downstream of the catalytic reactor, the stabilizing means arranged downstream of the catalytic reactor, the stabilizing means comprising vortex generators.
10. The burner as claimed in claim 9 , further comprising:
a step-widening of the flow passage downstream of the vortex generators.
11. The burner as claimed in claim 9 , wherein the vortex generators are configured and arranged to primarily effect mixing.
12. The burner as claimed in claim 9 , wherein the vortex generators are configured and arranged to primarily effect breakdown of vortices.