A combustion engine includes at least one combustion chamber, a first bleed air supply fluidly coupled to a portion of the combustion engine upstream of the combustion chamber, a second bleed air supply fluidly coupled to a portion of the combustion engine downstream of the combustion chamber, and a turbine, the turbine includes a first compressor, a second compressor, and a first turbine mounted to a common shaft, wherein the first compressor and the second compressor are in a series flow arrangement. The turbine also includes an intercooler fluidly coupling a portion of the first compressor in series to a portion of the second compressor.

    一种燃烧发动机,其包括至少一个燃烧室、流体地联接于燃烧室上游的燃烧发动机的一部分的第一放出空气供应部、流体地联接于燃烧室下游的燃烧发动机的一部分的第二放出空气供应部,以及涡轮机,该涡轮机包括安装至公共轴的第一压缩机、第二压缩机以及第一涡轮,其中第一压缩机和第二压缩机呈串流布置。涡轮机还包括中间冷却器,该中间冷却器将第一压缩机的一部分串联地流体地联接于第二压缩机的一部分。


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    Titel :

    Combustion engine comprising turbine


    Weitere Titelangaben:

    包括涡轮机的燃烧发动机


    Beteiligte:

    Erscheinungsdatum :

    06.05.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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