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Improvements in and relating to gas turbine cycles with interstage reheating

机译:级间再加热对燃气轮机循环的改进

摘要

412,970. Gas turbine plant. BRITISH THOMSON - HOUSTON CO., Ltd., Crown House, Aldwych, London, and SAMUELSON, F., 44, Hillmorton Road, Rugby. Jan. 6, 1933, No. 547. [Class 110 (iii).] In a gas turbine plant comprising a multi-stage turbine or two or more turbines, the working gases are reheated between stages by mixing them with gases drawn direct from the combustion chamber. In Fig. 1 a high pressure turbine 13 supplied by a combustion chamber 7 drives a generator 14 and its exciter 15, and a low pressure turbine 17 drives a compressor 1 for the charge air. This air, which may be preheated by the exhaust gases, is passed in part by a damper-controlled port 4 to the combustion chamber 7 in which fuel introduced by a pipe 3 is burnt, and in part by a dampercontrolled port 9 to a chamber 11 surrounding the combustion-chamber at the end 8 of which it mixes with part of the combustion-products and passes by a conduit 12 to the turbine 13. In their passage through the conduit 16 between the turbines 13, 17, the working gases are reheated by combustion products introduced from the chamber 7 by a pipe 18. These products may be fed in by an injector in order to increase the pressure in the pipe, and the supply may be controlled by a damper 19, or by a needle valve, which may be actuated automatically by a thermostat. In a modification, four turbines are arranged in series, two of them driving the power generator, and the other two driving series charge compressors at different speeds. Reheaters are arranged between the turbines as described above. The last turbine discharges into a chimney in order to reduce the back pressure. Fig. 5 shows an arrangement in which the turbine stages are supplied by conduits 31, 35, 39, 43 and in which the injectors 34, 38, 42 for the supply of interstage reheating gases are controlled by interconnected valves 44, 45, 46. The valveoperating cam-shaft 50 is actuated by a thermostat in the gas system, and a manual adjustment 54 is provided for each valve. More than one thermostat may be provided. Interstage combustion chambers for reheating may also be provided.
机译:412,970。燃气轮机厂。英国汤姆森-休斯敦有限公司,伦敦阿尔德维奇的Crown House和橄榄球的希尔默顿路44号,萨缪尔森。 1933年1月6日,第547号。[类别110(iii)。]在包括多级涡轮机或两台或更多台涡轮机的燃气轮机设备中,通过将工作气体与直接从中抽出的气体混合,在工作级之间进行重新加热。燃烧室。在图1中,由燃烧室7供应的高压涡轮13驱动发电机14及其激励器15,而低压涡轮17驱动用于增压空气的压缩机1。可能由废气预热的空气部分通过风门控制端口4进入燃烧室7,在燃烧室7中燃烧通过管道3引入的燃料,部分通过风门控制端口9进入燃烧室。如图11所示,工作气体在燃烧室的端部8处与燃烧产物的一部分混合并通过导管12到达涡轮13。在它们通过涡轮16、17、17之间的导管16时,工作气体为通过管道18从燃烧室7引入的燃烧产物将其再加热。这些产物可以通过喷射器供入,以增加管道中的压力,并且可以通过风门19或针形阀控制供应。可以由恒温器自动启动。在一个变型中,四个涡轮机串联布置,其中两个驱动发电机,而另两个驱动串联充气压缩机以不同的速度。如上所述,在涡轮之间布置有再热器。最后一个涡轮机排入烟囱,以降低背压。图5示出一种布置,其中涡轮级由导管31、35、39、43供应,并且其中用于供应级间再热气体的喷射器34、38、42由互连的阀44、45、46控制。气门操纵凸轮轴50由气体系统中的恒温器致动,并且为每个气门提供手动调节装置54。可以提供一个以上的恒温器。也可以提供用于再加热的级间燃烧室。

著录项

  • 公开/公告号GB412970A

    专利类型

  • 公开/公告日1934-07-06

    原文格式PDF

  • 申请/专利号GB19330000547

  • 发明设计人

    申请日1933-01-06

  • 分类号F02C3/32;F02C6/00;

  • 国家 GB

  • 入库时间 2022-08-24 06:55:57

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