首页> 外国专利> HIGH PRESSURE RATIO TWIN SPOOL INDUSTRIAL GAS TURBINE ENGINE WITH DUAL FLOW HIGH SPOOL COMPRESSOR

HIGH PRESSURE RATIO TWIN SPOOL INDUSTRIAL GAS TURBINE ENGINE WITH DUAL FLOW HIGH SPOOL COMPRESSOR

机译:高流量双涡轮增压高比例双涡轮增压工业燃气轮机发动机

摘要

An industrial gas turbine engine for electrical power production includes a high pressure spool and a low pressure spool in which the low pressure spool can be operated from full power mode to zero power mode when completely shut off, where the low pressure spool is operated at high electrical demand to supply compressed air to the high pressure compressor of the high pressure spool, and where turbine exhaust is used to drive a second electric generator from steam produced in a heat recovery steam generator. The high pressure spool includes a high pressure compressor with a inner compressed air flow path and an outer compressed air flow path in which a higher pressure supplies cooling to a turbine airfoil that is then discharged into a combustor of the engine.
机译:用于电力生产的工业燃气涡轮发动机包括高压阀芯和低压阀芯,其中当完全关闭时,低压阀芯可以从全功率模式运行到零功率模式,其中低压阀芯在高压下运行。将压缩空气供应到高压阀芯的高压压缩机的电力需求,其中涡轮机废气用于从热量回收蒸汽发生器中产生的蒸汽驱动第二发电机。高压滑阀包括具有内部压缩空气流动路径和外部压缩空气流动路径的高压压缩机,其中较高的压力向涡轮机翼片提供冷却,然后将该涡轮机翼片排放到发动机的燃烧器中。

著录项

  • 公开/公告号WO2018222192A1

    专利类型

  • 公开/公告日2018-12-06

    原文格式PDF

  • 申请/专利权人 FLORIDA TURBINE TECHNOLOGIES INC.;

    申请/专利号WO2017US35348

  • 发明设计人 OROSA JOHN A.;BROSTMEYER JOSEPH D.;

    申请日2017-06-01

  • 分类号F02C3/06;F01D5/02;F01D5/14;F01D25/12;F02C7/18;F02C6/08;

  • 国家 WO

  • 入库时间 2022-08-21 11:57:54

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