초록 ▼

A low pollution combustor is shown for controlling gas turbine pollutant emission, especially NOx. Fuel is injected and mixed with air upstream of the combustion zone. An axially movable baffle controls the air flow so that the fuel-air ratio is precisely controlled passing into the primary combusti

A low pollution combustor is shown for controlling gas turbine pollutant emission, especially NOx. Fuel is injected and mixed with air upstream of the combustion zone. An axially movable baffle controls the air flow so that the fuel-air ratio is precisely controlled passing into the primary combustion zone. A baffle recirculation zone prevents overheating of the walls. Dilution air is provided downstream of the primary zone for temperature dilution of the gases and to inhibit further formation of nitrogen oxides.

대표청구항 ▼

A low pollution combustor adapted to receive airflow from the compressor stage of a gas turbine engine and to discharge heated airflow therefrom to the turbine stage of the engine comprising: a cylindrical combustor housing having forward and rear portions; an aerodynamically contoured inlet mounted

A low pollution combustor adapted to receive airflow from the compressor stage of a gas turbine engine and to discharge heated airflow therefrom to the turbine stage of the engine comprising: a cylindrical combustor housing having forward and rear portions; an aerodynamically contoured inlet mounted on the forward portion of the combustor housing and adapted to direct airflow into the housing; said inlet having a diverging cross section; a support structure fixed at the entrance of the inlet; a baffle mounted on the support structure for axial sliding movement thereon, said baffle extending into the inlet and being contoured to form in cooperation with the inlet a gradually restricted channel for the airflow as it flows through the inlet, said airflow being accelerated thereby to create a zone of recirculating airflow in the forward portion of the combustor housing; fuel injecting means mounted in the inlet channel to premix fuel with the airflow prior to said airflow entering the forward portion of the combustor housing; a plurality of swirl vanes mounted in the inlet upstream of the fuel injecting means to enhance the mixing of air and fuel; control means connected to the baffle to adjust the axial position of the baffle thereby varying the fuel to air ratio of the airflow entering the combustor; and secondary fuel injection means mounted in the baffle to inject fuel into the recirculation zone.