Low emission combustor

Claim 2

In a gas turbine engine having a compressor, a turbine, a regenerator, and means for circulating turbine exhaust and compressor discharge through said regenerator whereby said compressor discharge is regeneratively heated to a temperature proportional to turbine exhaust temperature, the combination comprising, an inlet plenum maintained at compressor discharge pressure by said regenerated compressor discharge, a catalytic combustion chamber open to said inlet plenum and having a catalyst therein exposed to flow therethrough, said catalyst being operative at temperatures above a minimum temperature to sustain an ultra lean air/fuel ratio combustion reaction within said catalytic combustion chamber, a diffusion flame combustion chamber open to said inlet plenum, means defining a common exhaust plenum between each of said catalytic combustion and said diffusion flame combustion chambers and said turbine so that parallel flow paths are established whereby products of combustion developed in one of said catalytic combustion and said diffusion flame combustion chambers are diluted and cooled by regenerated compressor discharge flowing through the other, and fuel supply means operative in a first mode during engine start-up to meter fuel only to said diffusion flame combustion chamber and to effect ignition therein until said regenerated compressor discharge achieves a temperature corresponding to a temperature of said catalyst above said minimum temperature and thereafter in a second mode to meter fuel to only said catalytic combustion chamber for catalyst sustained combustion therein.

Claim 3

In a gas turbine engine having a compressor, a turbine, a regenerator, and means for circulating turbine exhaust and compressor discharge through said regenerator whereby said compressor discharge is regeneratively heated to a temperature proportional to turbine exhaust temperature, the combination comprising, an inlet plenum maintained at compressor discharge pressure by said regenerated compressor discharge, a catalytic combustion chamber open to said inlet plenum and including a prechamber and a monolith having a plurality of catalyst coated passages therethrough wherein said catalyst is exposed to flow through said catalytic combustion chamber and operative at a temperature above a minimum temperature to sustain an ultra lean air/fuel ratio combustion reaction within said passages, a diffusion flame combustion chamber open to said inlet plenum, means defining a common exhaust plenum between each of said catalytic combustion and said diffusion flame combustion chambers and said turbine so that parallel flow paths are established whereby products of combustion developed in one of said catalytic combustion and said diffusion flame combustion chambers are diluted and cooled by regenerated compressor discharge flowing through the other, and fuel supply means operative in a first mode during engine start-up to meter fuel only in to said diffusion flame combustion chamber and to effect ignition therein until said regenerated compressor discharge achieves a temperature corresponding to a temperature of said catalyst above said minimum temperature and thereafter in a second mode to meter fuel only into said prechamber for mixture with said regenerated compressor discharge and subsequent catalyst sustained combustion in said catalyst coated passages.

Claim 4

In a gas turbine engine having a compressor, a turbine, a regenerator, and means for circulating turbine exhaust and compressor discharge through said regenerator whereby said compressor discharge is regeneratively heated to a temperature proportional to turbine exhaust temperature, the combination comprising, an inlet plenum maintained at compressor discharge pressure by said regenerated compressor discharge, a catalytic combustion chamber open to said inlet plenum and including a prechamber and a monolith having a plurality of catalyst coated passages therethrough wherein said catalyst is exposed to flow through said catalytic combustion chamber and operative at a temperature above a minimum temperature to sustain an ultra lean air/fuel ratio combustion reaction within said passages, a diffusion flame combustion chamber open to said inlet plenum, means defining a common exhaust plenum between each of said catalytic combustion and said diffusion flame combustion chambers and said turbine so that parallel flow paths are established whereby products of combustion developed in one of said catalytic combustion and said diffusion flame combustion chambers are diluted and cooled by regenerated compressor discharge flowing through the other, and fuel supply means operative in a first mode during engine start-up to meter fuel only in to said diffusion flame combustion chamber and to effect ignition therein until said regenerated compressor discharge achieves a temperature corresponding to a temperature of said catalyst above said minimum temperature and thereafter in a second mode to meter fuel only into said prechamber for mixture with said regenerated compressor discharge and subsequent catalyst sustained combustion in said catalyst coated passages.

Claim 5

In a gas turbine engine having a compressor, a turbine, a regenerator, and means for circulating turbine exhaust and compressor discharge through said regenerator whereby said compressor discharge is regeneratively heated to a temperature proportional to turbine exhaust temperature, the combination comprising, an inlet plenum maintained at compressor discharge pressure by said regenerated compressor discharge, a catalytic combustion chamber open to said inlet plenum and including a prechamber and a monolith having a plurality of catalyst coated passages therethrough wherein said catalyst is exposed to flow through said catalytic combustion chamber and operative at a temperature above a minimum temperature to sustain an ultra lean/air fuel ratio combustion reaction within said passages, a diffusion flame combustion chamber open to said inlet plenum, means for swirling exhaust from said catalytic combustion chamber in a first direction, means for swirling exhaust from said diffustion flame combustion chamber in a second direction generally counter to said first direction, means defining an exhaust plenum between each of said catalytic combustion and said diffusion flame combustion chambers and said turbine wherein said counter swirling exhausts intersect so that products of combustion developed in one of said catalytic combustion and said diffusion flame combustion chambers and swirling in a corresponding one of said first and said second directions is diluted and cooled by regenerated compressor discharge flowing through the other and swirling in the other of said corresponding first and second directions, and fuel supply means operative in a first mode during engine start-up to meter fuel only into said diffusion flame combustion chamber and to effect ignition therein until said regenerated compressor discharge achieves a temperature corresponding to a temperature of said catalyst above said minimum temperature and thereafter in a second mode to meter fuel only into said prechamber for mixture with said regenerated compressor discharge and subsequent catalyst sustained combustion in said catalyst coated passages.

Claim 6

In a gas turbine engine having a compressor, a turbine, a regenerator, and means for circulating turbine exhaust and compressor discharge through said regenerator whereby said compressor discharge is regeneratively heated to a temperature proportional to turbine exhaust temperature, the combination comprising, an inlet plenum maintained at compressor discharge pressure by said regenerated compressor discharge, a catalytic combustion chamber open to said inlet plenum and including a prechamber and a monolith having a plurality of catalyst coated passages therethrough wherein said catalyst is exposed to flow through said catalytic combustion chamber and operative at a temperature above a minimum temperature to sustain an ultra lean/air fuel ratio combustion reaction within said passages, a diffusion flame combustion chamber open to said inlet plenum, means for swirling exhaust from said catalytic combustion chamber in a first direction, means for swirling exhaust from said diffustion flame combustion chamber in a second direction generally counter to said first direction, means defining an exhaust plenum between each of said catalytic combustion and said diffusion flame combustion chambers and said turbine wherein said counter swirling exhausts intersect so that products of combustion developed in one of said catalytic combustion and said diffusion flame combustion chambers and swirling in a corresponding one of said first and said second directions is diluted and cooled by regenerated compressor discharge flowing through the other and swirling in the other of said corresponding first and second directions, and fuel supply means operative in a first mode during engine start-up to meter fuel only into said diffusion flame combustion chamber and to effect ignition therein until said regenerated compressor discharge achieves a temperature corresponding to a temperature of said catalyst above said minimum temperature and thereafter in a second mode to meter fuel only into said prechamber for mixture with said regenerated compressor discharge and subsequent catalyst sustained combustion in said catalyst coated passages.

Claim 7

The combination recited in claim 3 wherein each of said catalytic combustion and said diffusion flame combustion chambers are disposed on a common axis.

Claim 8

The combination recited in claim 3 wherein said catalytic combustion chamber is disposed on a first axis and said diffusion flame combustion chamber is disposed on a second axis and said first and said second axes define an acute angle therebetween.