Combustor process for low-level NOx and CO emissions

Claim 2

In a method for forming and burning a combustible mixture of a fuel and air in a combustion zone having a primary combustion region, a secondary combustion region located downstream from said primary combustion region, and a quench or dilution region located downstream from said secondary combustion region, to produce hot combustion gases containing heat energy which are passed to a heat energy utilization zone to utilize a portion of said heat energy, and wherein, there are established a first stream of air and a second stream of air, at least a portion of said first stream of air is introduced into said primary combustion region as the sole stream of primary combustion air introduced thereto, a stream of fuel is introduced into said primary combustion region, said second stream of air is passed in heat exchange relationship with an exhaust stream from said heat energy utilization zone to heat said second stream of air, and at least a portion of said heated second stream of air is passed into said quench or dilution region, the improvement comprising: introducing said at least a portion of said first stream of air into said primary combustion region at a temperature within the range of from ambient to about 700° F. and at a controlled rate, and adjusting said rate in accordance with the rate of introduction of said fuel to be sufficient, when said fuel is burned, to provide in said primary combustion region a combustion gas temperature within the range of from about 2500° to about 3000° F at which the rate of formation of NO x is reduced and at which the rate of oxidation of CO to CO 2 is not substantially reduced; and introducing another portion of said heated second stream of air into said secondary combustion region at a temperature greater than the temperature of said first stream of air and at a rate which are sufficient to provide in said secondary combustion region a combustion gas temperature at which the concentration of CO pollutant in the combustion gases in said secondary combustion region is reduced and at which the concentration of said NO x pollutant is not increased.

Claim 3

A method according to claim 1 wherein: said first stream of air is divided into a stream comprising primary air and another stream comprising secondary air; said primary air is introduced into said primary combustion region as said controlled first stream of air; and at least a portion of said secondary air is mixed with said another portion of said heated second stream of air to adjust the temperature thereof and the resulting mixture is introduced into said secondary combustion region.

Claim 4

A method according to claim 1 wherein: said controlled first stream of air is introduced into said primary combustion region in an amount within the range of from 1 to 50 volume percent of the total air introduced into said combustion zone; and said another portion of said heated second stream of air is introduced into said secondary combustion region in an amount within the range of from 10 to 60 volume percent of the total air introduced into said combustion zone.

Claim 5

A method according to claim 3 wherein: said controlled first stream of air is introduced into said primary combustion region in an amount within the range of from 1 to 35 volume percent of the total air introduced into said combustion zone.

Claim 6

A method according to claim 1 wherein: said controlled first stream of air is introduced into said primary combustion region in an amount within the range of from 2 to 35 volume percent of the total air introduced into said combustion zone; and said another portion of said heated second stream of air is introduced into said secondary combustion region in an amount within the range of from 15 to 45 volume percent of the total air introduced into said combustion zone.

Claim 7

A method according to claim 5 wherein: said first stream of air is introduced into said primary combustion region in an amount within the range of from 2 to 18 volume percent of the total air introduced into said combustion zone.

Claim 8

A method according to claim 1 wherein the temperature of said another portion of said heated second stream of air is at least 200° F. greater than the temperature of said controlled first stream of air.

Claim 9

A method according to claim 1 wherein the temperature of said another portion of said heated second stream of air is up to at least 1000° F. greater than the temperature of said controlled first stream of air.

Claim 10

A method according to claim 8 wherein: said controlled first stream of air is introduced into said primary combustion region in an amount within the range of from 2 to 18 volume percent of the total air introduced into said combustion zone; and said another portion of said heated second stream of air is introduced into said secondary combustion region in an amount within the range of from 15 to 45 volume percent of the total air introduced into said combustion zone.

Claim 11

A method according to claim 1 wherein said combustion gas temperature in said secondary combustion region is not less than about 2500° F., but is below about 3000° F.

Claim 12

In a method for forming and burning a combustible mixture of a fuel and air in a combustion zone having a primary combustion region, a secondary combustion region located downstream from said primary combustion region, and a quench or dilution region located downstream from said secondary combustion region, to produce hot combustion gases containing heat energy which are passed to a heat energy utilization zone comprising a turbine to utilize a portion of said heat energy, and wherein, there are established a first stream of air and a second stream of air, at least a portion of said first stream of air is introduced into said primary combustion region as the sole stream of primary combustion air introduced thereto, a stream of fuel is introduced into said primary combustion region, said second stream of air is passed in heat exchange relationship with an exhaust stream from said heat energy utilization zone to heat said second stream of air, and at least a portion of said heated second stream of air is passed into said quench or dilution region, the improvement comprising: introducing said at least a portion of said first stream of air into said primary combustion region at a temperature within the range of from ambient to about 700° F. and at a controlled rate, and adjusting said rate in accordance with (a) the rate of introduction of said fuel and (b) the speed of said turbine to be sufficient, when said fuel is burned, to provide in said primary combustion region a combustion gas temperature within the range of from about 2500° to about 3000° F. at which the rate of formation of NO x is reduced and at which the rate of oxidation of CO to CO 2 is not substantially reduced; and introducing another portion of said heated second stream of air into said secondary combustion region at a temperature greater than the temperature of said first stream of air and at a rate which are sufficient to provide in said secondary combustion region a combustion gas temperature at which the concentration of CO pollutant in the combustion gases in said secondary combustion region is reduced and at which the concentration of said NO x pollutant is not increased.

Claim 13

In a method for forming and burning a combustible mixture of a fuel and air in a combustion zone having a primary combustion region, a secondary combustion region located downstream from said primary combustion region, and a quench or dilution region located downstream from said secondary combustion region, to produce hot combustion gases containing heat energy which are passed to a heat energy utilization zone comprising a turbine to utilize a portion of said heat energy, and wherein, there are established a first stream of air and a second stream of air, at least a portion of said first stream of air is introduced into said primary combustion region as the sole stream of primary combustion air introduced thereto, a stream of fuel is introduced into said primary combustion region, said second stream of air is passed in heat exchange relationship with an exhaust stream from said heat energy utilization zone to heat said second stream of air, and at least a portion of said heated second stream of air is passed into said quench or dilution region, the improvement comprising: introducing said at least a portion of said first stream of air into said primary combustion region at a temperature within the range of from ambient to about 700° F. and at a controlled rate, and adjusting said rate in accordance with (a) the rate of introduction of said fuel and (b) the speed of said turbine to be sufficient, when said fuel is burned, to provide in said primary combustion region a combustion gas temperature within the range of from about 2500° to about 3000° F. at which the rate of formation of NO x is reduced and at which the rate of oxidation of CO to CO 2 is not substantially reduced; and introducing another portion of said heated second stream of air into said secondary combustion region at a temperature greater than the temperature of said first stream of air and at a rate which are sufficient to provide in said secondary combustion region a combustion gas temperature at which the concentration of CO pollutant in the combustion gases in said secondary combustion region is reduced and at which the concentration of said NO x pollutant is not increased.

Claim 14

In a method for forming and burning a combustible mixture of a fuel and air in a combustion zone having a primary combustion region, a secondary combustion region located downstream from said primary combustion region, and a quench or dilution region located downstream from said secondary combustion region, to produce hot combustion gases containing heat energy which are passed to a heat energy utilization zone comprising a turbine to utilize a portion of said heat energy, and wherein, there are established a first stream of air and a second stream of air, at least a portion of said first stream of air is introduced into said primary combustion region as the sole stream of primary combustion air introduced thereto, a stream of fuel is introduced into said primary combustion region, said second stream of air is passed in heat exchange relationship with an exhaust stream from said heat energy utilization zone to heat said second stream of air, and at least a portion of said heated second stream of air is passed into said quench or dilution region, the improvement comprising: introducing said at least a portion of said first stream of air into said primary combustion region at a temperature within the range of from ambient to about 700° F. and at a controlled rate, and adjusting said rate in accordance with the speed of said turbine to be sufficient, when said fuel is burned, to provide in said primary combustion region a combustion gas temperature within the range of from about 2500° to about 3000° F. at which the rate of formation of NO x is reduced and at which the rate of oxidation of CO to CO 2 is not substantially reduced; and introducing another portion of said heated second stream of air into said secondary combustion region at a temperature greater than the temperature of said first stream of air and at a rate which are sufficient to provide in said secondary combustion region a combustion gas temperature at which the concentration of CO pollutant in the combustion gases in said secondary combustion region is reduced and at which the concentration of said NO x pollutant is not increased.

Claim 15

In a method for forming and burning a combustible mixture of a fuel and air in a combustion zone having a primary combustion region, a secondary combustion region located downstream from said primary combustion region, and a quench or dilution region located downstream from said secondary combustion region, to produce hot combustion gases containing heat energy which are passed to a heat energy utilization zone comprising a turbine to utilize a portion of said heat energy, and wherein, there are established a first stream of air and a second stream of air, at least a portion of said first stream of air is introduced into said primary combustion region as the sole stream of primary combustion air introduced thereto, a stream of fuel is introduced into said primary combustion region, said second stream of air is passed in heat exchange relationship with an exhaust stream from said heat energy utilization zone to heat said second stream of air, and at least a portion of said heated second stream of air is passed into said quench or dilution region, the improvement comprising: introducing said at least a portion of said first stream of air into said primary combustion region at a temperature within the range of from ambient to about 700° F. and at a controlled rate, and adjusting said rate in accordance with the speed of said turbine to be sufficient, when said fuel is burned, to provide in said primary combustion region a combustion gas temperature within the range of from about 2500° to about 3000° F. at which the rate of formation of NO x is reduced and at which the rate of oxidation of CO to CO 2 is not substantially reduced; and introducing another portion of said heated second stream of air into said secondary combustion region at a temperature greater than the temperature of said first stream of air and at a rate which are sufficient to provide in said secondary combustion region a combustion gas temperature at which the concentration of CO pollutant in the combustion gases in said secondary combustion region is reduced and at which the concentration of said NO x pollutant is not increased.