INTERMEDIATE COOLING TURBINE INCLUDING HEAT STORAGE SYSTEM

To provide a heat storage system used together with a gas turbine engine having an intercooler.SOLUTION: A heat storage system may comprise: a secondary cooler 110 communicating with an intercooler 50; a heat energy storage tank 160 communicating with the secondary cooler and intercooler; and a temp...

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Bibliographische Detailangaben
Hauptverfasser:	DOUGLAS ALAN JONES, TANG CHING-JEN
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	To provide a heat storage system used together with a gas turbine engine having an intercooler.SOLUTION: A heat storage system may comprise: a secondary cooler 110 communicating with an intercooler 50; a heat energy storage tank 160 communicating with the secondary cooler and intercooler; and a temperature controller 245 arranged around a gas turbine engine 10, and communicating with the heat energy storage tank.SELECTED DRAWING: Figure 3 【課題】インタークーラを有するガスタービンエンジンと共に使用するための蓄熱システムを提供する。【解決手段】蓄熱システムは、インタークーラ５０と連通する二次冷却器１１０と、二次冷却器およびインタークーラと連通する熱エネルギ貯蔵タンク１６０と、ガスタービンエンジン１０の周りに配置され、熱エネルギ貯蔵タンクと連通する温度調節装置２４５とを含んでもよい。【選択図】図３