초록 ▼

A combustor for burning heavy residual fuel to drive a gas turbine engine has an elongated, imperforate vaporizing tube with an air blast nozzle at one end of the tube adjacent a cannister type preheater means arranged to swirl air blasted residual fuel in the tube to produce vaporization while prev

A combustor for burning heavy residual fuel to drive a gas turbine engine has an elongated, imperforate vaporizing tube with an air blast nozzle at one end of the tube adjacent a cannister type preheater means arranged to swirl air blasted residual fuel in the tube to produce vaporization while preventing autoignition and wherein the vaporized fuel is processed through a primary crossed slot air mixer means for reducing the temperature of the air/fuel mixture passing from the vaporizing tube and to establish an equivalence ratio in the air/fuel mixture at a lean reaction zone combustion chamber for burning a lean air/fuel mixture from the primary air mixer means under controlled conditions and wherein a combustor torch igniter directs an igniting flame into the lean air/fuel mixture directed from the air mixer means so as to assure continuous combustion in the lean combustion zone so as to reduce hydrocarbon and carbon monoxide emissions from the combustion apparatus under varying conditions of gas turbine engine operation.

대표청구항 ▼

In a high vapor temperature liquid fuel combustor, the combination comprising, a vaporizing tube of predetermined length and cross section having an inlet and an outlet, a fuel nozzle at said inlet connected to a source of said fuel and to a source of compressed air and operative to separate said fu

In a high vapor temperature liquid fuel combustor, the combination comprising, a vaporizing tube of predetermined length and cross section having an inlet and an outlet, a fuel nozzle at said inlet connected to a source of said fuel and to a source of compressed air and operative to separate said fuel by air blast into a plurality of droplets and to direct a longitudinal stream of said droplets into said tube, a preheat combustor means operative to generate a preheat stream of heated products of combustion, means operative to direct said preheat stream into said tube generally at said inlet for interception of said droplet stream and mixture therewith whereby said mixture traverses said tube toward said outlet in a longitudinally moving swirl having a residence time in said tube proportional to said length and said cross section thereof and sufficient in duration for the heat from said preheat stream to vaporize said droplets without autoignition of said vapor, a primary air mixer connected to said tube outlet and to said compressed air source operative to combine said vaporized fuel and compressed air into a combustible mixture, first variable geometry means for regulating air flow into said primary air mixer thereby to control the equivalence ratio of said combustible mixture to reduce production of nitrous oxides, means defining a lean reaction zone for receiving said combustible mixture from said primary air mixer, means for igniting said mixture in said lean reaction zone to generate products of combustion, and second variable geometry means in a downstream portion of said lean reaction zone for regulating air flow from said compressed air source into said downstream portion to quench said products of combustion.