초록 ▼

An external combustion system for a stationary gas turbine engine includes a rich zone combustor, a water or steam quench stage, a lean zone combustor and a dilution stage. Fuel such as natural gas or liquid hydrocarbon, which forms no ash or slag, burns in a primary air supply in the rich zone comb

An external combustion system for a stationary gas turbine engine includes a rich zone combustor, a water or steam quench stage, a lean zone combustor and a dilution stage. Fuel such as natural gas or liquid hydrocarbon, which forms no ash or slag, burns in a primary air supply in the rich zone combustor at an equivalence ratio exceeding 1 which inhibits rapid formation of of oxides of nitrogen. The effluent from the rich zone combustor is a stream of combustible gas including carbon monoxide and hydrogen. The combustible gas stream is quenched in the quench stage and mixed with a secondary supply of compressed air in the lean zone combustor. The combustible gas ignites spontaneously in the lean zone combustor and burns at an equivalence ratio of less than 1 and at a temperature below the range characterized by rapid formation of oxides of nitrogen. The discharge from the lean zone combustor is a stream of hot gas motive fluid which is diluted in the dilution stage and introduced into the turbine section of the engine.

대표청구항 ▼

In combination with a source of compressed air and a source of one of a gaseous and a liquid fuel, a combustion system comprising: a rich zone combustor, means connecting said rich zone combustor to said source of compressed air and to said source of one of said gaseous and said liquid fuel, said fu

In combination with a source of compressed air and a source of one of a gaseous and a liquid fuel, a combustion system comprising: a rich zone combustor, means connecting said rich zone combustor to said source of compressed air and to said source of one of said gaseous and said liquid fuel, said fuel being burned in a primary portion of said compressed air in said rich zone combustor at an equivalence ratio exceeding 1 and at on the order of about 2800 degrees F. whereby rapid formation of oxides of nitrogen is inhibited and a continuous stream of combustible hot gas issues from said rich zone combustor, a quench stage connected to said rich zone combustor having a throat portion therein receiving said continuous stream of combustible hot gases, means on said quench stage defining a curtain of one of water and steam stretching across said throat portion and intercepting all of said continuous stream of combustible hot gas to reduce the temperature of said continuous stream of combustible hot gas from on the order of about 2800 degrees F. entering said quench stage to on the order of about 1900 degrees F. exiting said quench stage, a lean zone combustor connected to said quench stage receiving therefrom the total outflow of said quenched combustible hot gas and to said source of compressed air operative to mix said quenched combustible hot gas and a secondary portion of said compressed air to initiate spontaneous combustion of said quenched combustible hot gas in said lean zone combustor at an equivalent ratio of less than 1, said spontaneous combustion generating a continuous stream of non-combustible hot gas motive fluid at a temperature not exceeding about 3000°F., and duct means connected to said lean zone combustor for transporting said non-combustible hot gas motive fluid to a consuming device.