JPS61198502U - - Google Patents

Info

Publication number
JPS61198502U
JPS61198502U JP8178985U JP8178985U JPS61198502U JP S61198502 U JPS61198502 U JP S61198502U JP 8178985 U JP8178985 U JP 8178985U JP 8178985 U JP8178985 U JP 8178985U JP S61198502 U JPS61198502 U JP S61198502U
Authority
JP
Japan
Prior art keywords
heat recovery
exhaust
recovery boiler
gas turbine
gas
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP8178985U
Other languages
Japanese (ja)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP8178985U priority Critical patent/JPS61198502U/ja
Publication of JPS61198502U publication Critical patent/JPS61198502U/ja
Pending legal-status Critical Current

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  • Engine Equipment That Uses Special Cycles (AREA)
  • Combustion Of Fluid Fuel (AREA)

Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本考案の一実施例を示した説明図、第
2図は従来の技術の一例を示した説明図である。 1……ガスタービン、2……排熱回収ボイラ、
3……スチームタービン、4……排ガスライン、
5……追焚装置、6……モレキユラーシーブ、7
……ガス供給ライン。
FIG. 1 is an explanatory diagram showing an embodiment of the present invention, and FIG. 2 is an explanatory diagram showing an example of a conventional technique. 1...Gas turbine, 2...Exhaust heat recovery boiler,
3...Steam turbine, 4...Exhaust gas line,
5... Reheating device, 6... Molecular sieve, 7
...Gas supply line.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ガスタービンと、このガスタービンの排ガス系
に設けられた排熱回収ボイラと、この排熱回収ボ
イラで発生した蒸気によつて駆動される蒸気使用
機械と、前記ガスタービンと該排熱回収ボイラを
結ぶ排ガス系の途中に設けられた追焚装置とを有
するコンバインドサイクルにおいて、該排熱回収
ボイラの排ガス出口側に設けられて該排熱回収ボ
イラからの排ガスを分子ふるい分けして残存酸素
量が容積比で16%以上になつたガスを前記追焚
装置に燃焼用空気の代りとして供給するモレキユ
ラーシーブを備えていることを特徴とする、ガス
タービンの熱回収装置。
A gas turbine, an exhaust heat recovery boiler provided in the exhaust gas system of the gas turbine, a steam-using machine driven by the steam generated by the exhaust heat recovery boiler, and the gas turbine and the exhaust heat recovery boiler. In a combined cycle that has a reheating device installed in the middle of the exhaust gas system, the exhaust gas from the exhaust heat recovery boiler is molecularly sieved to determine the amount of residual oxygen by volume. A heat recovery device for a gas turbine, comprising a molecular sieve that supplies gas with a ratio of 16% or more to the reheating device as a substitute for combustion air.
JP8178985U 1985-06-01 1985-06-01 Pending JPS61198502U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8178985U JPS61198502U (en) 1985-06-01 1985-06-01

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8178985U JPS61198502U (en) 1985-06-01 1985-06-01

Publications (1)

Publication Number Publication Date
JPS61198502U true JPS61198502U (en) 1986-12-11

Family

ID=30628903

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8178985U Pending JPS61198502U (en) 1985-06-01 1985-06-01

Country Status (1)

Country Link
JP (1) JPS61198502U (en)

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