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METHOD OF CONVERTING THERMAL ENERGY TO WORK IN GAS-TURBINE PLANT AND GAS-TURBINE PLANT PROPER

机译:燃气轮机厂热能转化工作方法及燃气轮机厂适当性

摘要

FIELD: manufacture of gas turbines. SUBSTANCE: oxidizer (air) is fed to compressor where it is compressed. To reduce this work, superheated water is injected into compressor stages where oxidizer temperature is high. Oxidizer being compressed is partially bled from intermediate compressor stages. Oxidizer from last compressor stage remaining after preheating in regenerative heat exchanger is fed to combustion chamber of compressor stages; preheated fuel is simultaneously fed to this combustion chamber. Fuel is partially burnt in compressor stages at air-excess coefficient lesser than 1 and products of incomplete combustion of fuel are directed to turbomachine for converting their heat to work. Then products of incomplete combustion pass in succession all expansion stages of turbomachine to whose nozzle tabs preheated additional portions of oxidizer are supplied and after-burning of fuel at air-excess coefficient lesser than 1 takes place. Final after-burning of fuel at air-excess coefficient more than 1 is effected in last stage of turbomachine. EFFECT: enhanced efficiency. 5 cl, 1 dwg
机译:领域:燃气轮机制造。物质:氧化剂(空气)被送入压缩机进行压缩。为了减少这项工作,将过热水注入氧化剂温度高的压缩机级。压缩的氧化剂从中间的压缩机级中部分排出。来自最后一个压缩机级的氧化剂在再生热交换器中进行预热后剩下的氧化剂被送入压缩机级的燃烧室。同时将预热的燃料送入该燃烧室。燃料在压缩机阶段以小于1的空气过量系数进行部分燃烧,燃料不完全燃烧的产物被引导至涡轮机以将其热量转化为功。然后,不完全燃烧的产物依次通过涡轮机的所有膨胀级,在这些膨胀级的喷嘴翼片中预加了氧化剂的附加部分,然后发生空气过剩系数小于1的燃料后燃。在涡轮机的最后阶段进行空气系数大于1的最终燃料后燃。效果:提高效率。 5厘升,1载重吨

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