Combustion gas turbine systems and operation method thereof

Combustion gas turbine systems and operation method thereof

  • CN 1,912,367 A
  • Filed: 08/10/2006
  • Published: 02/14/2007
  • Est. Priority Date: 08/10/2005
  • Status: Active Application
First Claim
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1. a combustion gas turbine systems (10) comprising:

  • A) compressor set (14) of a compression ambient air;

    B) firing chamber (16) that becomes the fluid connection with compressor set (14), this firing chamber (16) are accepted from the next pressurized air of compressor set (14), and first fuel that burns flows and generation firing chamber discharge air-flow;

    C) first turbine (18) that is arranged on downstream, firing chamber (16) makes this firing chamber discharge air-flow and partly expands;

    D) reheat machine (12) that becomes fluid to be communicated with first turbine (18) laterally flows to introduce one second fuel from the working air current of first turbine (18) in order to the edge, so that combustion fuel under the situation of this working air current is being arranged;

    AndE) one second turbine (20) makes the discharge flow expansion from this reheat machine (12).

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