Abstract A heater for heating gases such as turbine exhaust gases to facilitate the extraction of the heat energy carried by such gases or flue gases to reduce their corrosiveness. The heater is defined by burners installed on walls of the duct through which the gases flow. The burner can be operated with heavy fuel oil and normally uses no more primary air than is necessary to ignite the fuel oil atomized by the burner and sustain a flame. The flame is relatively long and narrow and is directed transversely to the gas flow into the duct. Upstream of the burner is a shield to protect the flame from the gas flow. The shield communicates with a register which collects an amount of gas sufficient to provide the balance of the combustion oxygen to fully combust all fuel. From the register the gas flows along inclined passages to the side of the shield facing the flame, the passages directing the gas in the direction of the flame and at an oblique angle in regard thereto. The flame shield is shaped to approximate the outline of the flame. Gas not collected by the register is guided by the shield past the flame so as to achieve a uniform heating of the gas and thereby prevent the formation of hot spots in the gas downstream of the heater. For operation in gas streams having a low oxygen content the burner is constructed so that the fuel-to-combustion oxygen ratio in the upstream and downstream portion of the flame (relative to the exhaust gas flow) is substantially equalized.
A method for heating an exhaust gas flow through a duct defined by opposing duct walls comprising the steps of: generating an elongated flame with a fuel and an off-stoichiometric amount of primary combustion air; extending the flame from one duct wall towards the other duct wall; flowing exhaust gas in the form of exhaust gas streams about the flame along paths boundaries of which substantially intersect peripheries of the flame; flowing secondary combustion air transversely to and directly into an upstream portion of the flame, relative to the gas flow through the duct, over substantially the full length of the flame; equalizing the fuel-to-combustion air ratio in an upstream portion and in the downstream portion of the flame relative to the gas flow through the duct to thereby substantially uniformly and completely combust all fuel.
Claim 2
Independent Claim
136 words
A method for heating an exhaust gas flow through a duct defined by opposing duct walls comprising the steps of: generating an elongated flame with a fuel and an off-stoichiometric amount of primary combustion air; extending the flame from one duct wall towards the other duct wall; flowing exhaust gas in the form of exhaust gas streams about the flame along paths boundaries of which substantially intersect peripheries of the flame; flowing secondary combustion air transversely to and directly into an upstream portion of the flame, relative to the gas flow through the duct, over substantially the full length of the flame; equalizing the fuel-to-combustion air ratio in an upstream portion and in the downstream portion of the flame relative to the gas flow through the duct to thereby substantially uniformly and completely combust all fuel.
Claim 3
Dependent Claim
32 words
A method according to claim 1 wherein the step of equalizing comprises the step of biasing relatively more fuel into the upstream portion of the flame than into the downstream portion thereof.
Claim 4
Dependent Claim
34 words
A method according to claim 1 wherein the step of equalizing comprises the step of biasing relatively more primary combustion air into the downstream portion of the flame than into the upstream portion thereof.