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    Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 009::page 91015-1
    Author:
    Tanaka, Toshimitsu
    ,
    Takata, Ryo
    ,
    Hirado, Takuma
    ,
    Kawanami, Akira
    DOI: 10.1115/1.4067638
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this article, a hermetic and oil-free turbine generator for a cryogenic organic Rankine circle (ORC) is suggested and investigated. The generator mainly consists of a high-speed generator, a two-stage supersonic turbine, and magnetic bearings. Based on the hermetic design concept, these components are in a common casing. To upgrade the cooling capability of the generator, heat dissipation fins are installed between the first and second stages of the turbine. Performance of the turbine generator was preliminarily investigated by CFD calculations. These results show that the turbine efficiency peaks at 16,000 rpm under the design pressure ratio condition. Under the same condition, it is also predicted that comparatively high static pressure recovery coefficient and low total pressure loss can be obtained through the flow path with the fins. Moreover, a series of experimental campaign were conducted on an ORC test rig using −196 °C liquid nitrogen and 50 °C warm water as cold source and heat source, respectively. These results indicate that the target power output was achieved and the installed heat dissipation fins are effective to enhance the cooling capability of the generator. It was also indicated that under comparatively high loaded conditions, the turbine power output can be increased by heat transferred from the generator.
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      Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4306026
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    contributor authorTanaka, Toshimitsu
    contributor authorTakata, Ryo
    contributor authorHirado, Takuma
    contributor authorKawanami, Akira
    date accessioned2025-04-21T10:21:48Z
    date available2025-04-21T10:21:48Z
    date copyright2/17/2025 12:00:00 AM
    date issued2025
    identifier issn0889-504X
    identifier otherturbo-24-1292.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306026
    description abstractIn this article, a hermetic and oil-free turbine generator for a cryogenic organic Rankine circle (ORC) is suggested and investigated. The generator mainly consists of a high-speed generator, a two-stage supersonic turbine, and magnetic bearings. Based on the hermetic design concept, these components are in a common casing. To upgrade the cooling capability of the generator, heat dissipation fins are installed between the first and second stages of the turbine. Performance of the turbine generator was preliminarily investigated by CFD calculations. These results show that the turbine efficiency peaks at 16,000 rpm under the design pressure ratio condition. Under the same condition, it is also predicted that comparatively high static pressure recovery coefficient and low total pressure loss can be obtained through the flow path with the fins. Moreover, a series of experimental campaign were conducted on an ORC test rig using −196 °C liquid nitrogen and 50 °C warm water as cold source and heat source, respectively. These results indicate that the target power output was achieved and the installed heat dissipation fins are effective to enhance the cooling capability of the generator. It was also indicated that under comparatively high loaded conditions, the turbine power output can be increased by heat transferred from the generator.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability
    typeJournal Paper
    journal volume147
    journal issue9
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4067638
    journal fristpage91015-1
    journal lastpage91015-9
    page9
    treeJournal of Turbomachinery:;2025:;volume( 147 ):;issue: 009
    contenttypeFulltext
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