PROBLEM TO BE SOLVED: To suppress reduction of power generation performance while suppressing an increase in volume and weight.SOLUTION: A jet engine 21 comprises: a high-pressure compressor 28 which compresses gas; a combustor 32 which burns fuel by the gas that has been compressed; and a high-pressure turbine 33 which drives the high-pressure compressor 28 with combustion gas from the first combustor 32 serving as a driving source. A flow channel 23 is provided to take out, to the outside, part of the gas supplied to the combustor 32. A fuel cell system 22 comprises: a fuel cell 42; and a compressor 41 which introduces the gas as a working fluid for the fuel cell 42 via the flow channel 23 so as to supply the working fluid to an introduction port on an air electrode side of the fuel cell 42, with the working fluid controlled to be at a desired temperature.SELECTED DRAWING: Figure 2

    【課題】容積及び重量の増大を抑えつつ発電性能の低下を抑えること。【解決手段】ジェットエンジン21は、気体を圧縮する高圧圧縮機28と、圧縮された気体により燃料を燃焼する燃焼器32と、第1の燃焼器32よりの燃焼ガスを駆動源として高圧圧縮機28を駆動する高圧タービン33とを有する。流路23は、燃焼器32に供給される気体の一部を外部に取り出す。燃料電池システム22は、燃料電池42と、流路23を介して気体を燃料電池42の作動流体として導入し、作動流体を燃料電池42の空気極側の導入口に所望の温度に制御して供給する圧縮機41とを有する。【選択図】図2


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    Title :

    FUEL CELL SYSTEM, HYBRID SYSTEM, AIRCRAFT AND AUXILIARY POWER DEVICE MOUNTED ON AIRCRAFT


    Additional title:

    燃料電池システム、ハイブリッドシステム、航空機及び航空機に搭載される補助動力装置


    Contributors:

    Publication date :

    2017-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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