Method of operating a gas turbine combustor having an independent airstream to remove heat from the primary combustion zone

Claim 3

A method in accordance with claim 1 wherein: said third stream of air is passed in a first annular stream surrounding said wall of said primary combustion zone, and then introduced into said third zone; and said second stream of air is passed in a second annular stream surrounding but separated from said first annular stream of air.

Claim 4

A method in accordance with claim 1 wherein: said first stream of air is initially introduced into a swirl zone at the upstream end portion of said primary combustion zone and exits from said swirl zone as a swirling stream of air; said fuel is introduced in a downstream direction and axially of said swirling stream of air so as to effect controlled mixing of said fuel and said air at the interface therebetween; and said fuel and said air are expanded in a uniform and graduated manner, during at least a portion of said mixing thereof, from the volume in the region of the initial contact therebetween to the volume of said combustion zone.

Claim 5

A method according to claim 1 wherein the temperature of said second stream of air is greater than the temperature of said first stream of air.

Claim 6

A method according to claim 4 wherein the temperature of said second stream of air is at least about 100° F. greater than the temperature of said first stream of air.

Claim 7

A method according to claim 5 wherein the temperature of said second stream of air is from about 100° to about 1200° F. greater than the temperature of said first stream of air.

Claim 8

A method according to claim 6 wherein the temperature of said first stream of air is not greater than about 500° F.

Claim 9

A method according to claim 6 wherein the temperature of said first stream of air is not greater than about 700° F.

Claim 10

A method according to claim 1 wherein: the temperature of the inlet air to said primary combustion zone is within the range of about 1100° F. to about 1500° F.; and the temperature of said second stream of air is within the range of about 1100° F. to about 1500° F.

Claim 11

A method according to claim 2 wherein the temperature of said first stream of air is not greater than about 500° F., and the temperature of said second stream of air is within the range of from about 1100° F. to about 1300° F.

Claim 12

In a method for burning a fuel in a combustor, wherein in said method separate streams of air are established as a first stream of air, a second stream of air, and a third stream of air; said first stream of air is introduced into a primary combustion zone of said combustor; a fuel is introduced into said primary combustion zone; said fuel is burned; said second stream of air is maintained separate from said first stream of air and is introduced into a secondary combustion zone of said combustor located downstream from said primary combustion zone; said third stream of air, while being maintained separate from said first and second streams of air, is passed in a downstream direction over and in heat exchange with an outer wall of said primary combustion zone so as to remove heat from the interior of said primary combustion zone and heat said air; and said thus heated third stream of air is introduced into a third zone of said combustor located downstream from said secondary zone; the improvement comprising: introducing only a portion of said second stream of air into said secondary zone; combining another portion of said second stream of air with said heated third stream of air prior to the introduction of said third stream of air into said third zone; and then introducing said combined streams of air into said third zone.

Claim 13

In a method for burning a fuel in a combustor, wherein in said method separate streams of air are established as a first stream of air, a second stream of air, and a third stream of air; said first stream of air is introduced into a primary combustion zone of said combustor; a fuel is introduced into said primary combustion zone; said fuel is burned; said second stream of air is maintained separate from said first stream of air and is introduced into a secondary combustion zone of said combustor located downstream from said primary combustion zone; said third stream of air, while being maintained separate from said first and second streams of air, is passed in a downstream direction over and in heat exchange with an outer wall of said primary combustion zone so as to remove heat from the interior of said primary combustion zone and heat said air; and said thus heated third stream of air is introduced into a third zone of said combustor located downstream from said secondary zone; the improvement comprising: introducing only a portion of said second stream of air into said secondary zone; combining another portion of said second stream of air with said heated third stream of air prior to the introduction of said third stream of air into said third zone; and then introducing said combined streams of air into said third zone.

Claim 14

A method in accordance with claim 11 wherein: said third stream of air is passed in a downstream direction as an inner annular stream surrounding said wall of said primary combustion zone; and said second stream of air is passed in a downstream direction as an outer annular stream surrounding, but separated from, said inner annular stream of air.

Claim 15

In a method for burning a fuel in a combustor, wherein in said method separate streams of air are established as a first stream of air, a second stream of air, and a third stream of air; said first stream of air in introduced into a primary combustion zone of said combustor; a fuel is introduced into said primary combustion zone; said fuel is burned; said second stream of air is maintained separate from said first stream of air and is introduced into a secondary combustion zone of said combustor located downstream from said primary combustion zone; said third stream of air, while being maintained separate from said first and second streams of air, is passed in a downstream direction over and in heat exchange with an outer wall of said primary combustion zone so as to remove heat from the interior of said primary combustion zone and heat said air; and said thus heated third stream of air is introduced into a third zone of said combustor located downstream from said secondary zone; the improvement comprising: dividing said second stream of air into a first portion and a second portion; introducing only said first portion into said secondary zone, and combining said second portion with said heated third stream of air prior to the introduction of said third stream of air into said third zone, so as to reduce the pressure drop through said combustor; and then introducing said combined streams of air into said third zone.

Claim 16

In a method for burning a fuel in a combustor, wherein in said method separate streams of air are established as a first stream of air, a second stream of air, and a third stream of air; said first stream of air in introduced into a primary combustion zone of said combustor; a fuel is introduced into said primary combustion zone; said fuel is burned; said second stream of air is maintained separate from said first stream of air and is introduced into a secondary combustion zone of said combustor located downstream from said primary combustion zone; said third stream of air, while being maintained separate from said first and second streams of air, is passed in a downstream direction over and in heat exchange with an outer wall of said primary combustion zone so as to remove heat from the interior of said primary combustion zone and heat said air; and said thus heated third stream of air is introduced into a third zone of said combustor located downstream from said secondary zone; the improvement comprising: dividing said second stream of air into a first portion and a second portion; introducing only said first portion into said secondary zone, and combining said second portion with said heated third stream of air prior to the introduction of said third stream of air into said third zone, so as to reduce the pressure drop through said combustor; and then introducing said combined streams of air into said third zone.

Claim 17

A method according to claim 13 wherein: said third stream of air is passed in a downstream direction as an inner annular stream surrounding said wall of said primary combustion zone; and said second stream of air is passed in a downstream direction as an outer annular stream surrounding, but separated from, said inner annular stream of air.

Claim 18

A method according to claim 14 wherein: the temperature of said first stream of air is not greater than about 700° F.; and the temperature of said second stream of air is at least 100° F. greater than the temperature of said first stream of air.