YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Cooling System of a High-Pressure Centrifugal Compressor: Development and Impact on Wheel Temperatures

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 005::page 51009-1
    Author:
    Weihard, Stefan
    ,
    Willeke, Tobias
    ,
    Božek, Lukáš
    ,
    Hort, Vladimír
    ,
    Münch, Stefan
    ,
    Spengler, Sebastian
    ,
    Winter, Thomas
    DOI: 10.1115/1.4066733
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High power density, low fuel consumption, and a compact design with competitive total costs of ownership are key requirements for internal combustion engines for conventional fuels and carbon-free or carbon-neutral future fuels. These requirements influence the development targets of charging systems and call for single-stage charging systems with increased charge air pressures. However, high compressor pressure ratios of the turbocharger lead to challenging material temperatures in aluminum alloy wheels. Consequently, creep becomes the fundamental lifetime-limiting damage mechanism for these wheels. In order to meet customer requirements regarding total costs of ownership, the lifetime is of major importance for the development of aluminum compressor wheels for turbochargers with pressure ratios beyond 6. This paper focuses on a high-pressure compressor (HPC) design with a water-cooling system for a new turbocharger generation. The development of its components and their validation based on numerically predicted and measured compressor wheel temperatures are discussed. After introducing the need for high-pressure ratios and the accompanying lifetime challenges, the paper presents the design strategy and methods of the development process. Finally, the paper summarizes the achievements obtained by this procedure. Detailed and rarely before documented temperature measurements from the rotating compressor wheel are published. As will be shown, the temperature measurements confirm the predictions from the predevelopment phase. A comparison of the temperature measurements from the recently developed compressor wheel with measurements carried out for a state-of-the-art wheel reveals the technological improvements achieved by this new generation of high-pressure compressor wheels.
    • Download: (2.530Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Cooling System of a High-Pressure Centrifugal Compressor: Development and Impact on Wheel Temperatures

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4306098
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorWeihard, Stefan
    contributor authorWilleke, Tobias
    contributor authorBožek, Lukáš
    contributor authorHort, Vladimír
    contributor authorMünch, Stefan
    contributor authorSpengler, Sebastian
    contributor authorWinter, Thomas
    date accessioned2025-04-21T10:23:42Z
    date available2025-04-21T10:23:42Z
    date copyright11/14/2024 12:00:00 AM
    date issued2024
    identifier issn0742-4795
    identifier othergtp_147_05_051009.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306098
    description abstractHigh power density, low fuel consumption, and a compact design with competitive total costs of ownership are key requirements for internal combustion engines for conventional fuels and carbon-free or carbon-neutral future fuels. These requirements influence the development targets of charging systems and call for single-stage charging systems with increased charge air pressures. However, high compressor pressure ratios of the turbocharger lead to challenging material temperatures in aluminum alloy wheels. Consequently, creep becomes the fundamental lifetime-limiting damage mechanism for these wheels. In order to meet customer requirements regarding total costs of ownership, the lifetime is of major importance for the development of aluminum compressor wheels for turbochargers with pressure ratios beyond 6. This paper focuses on a high-pressure compressor (HPC) design with a water-cooling system for a new turbocharger generation. The development of its components and their validation based on numerically predicted and measured compressor wheel temperatures are discussed. After introducing the need for high-pressure ratios and the accompanying lifetime challenges, the paper presents the design strategy and methods of the development process. Finally, the paper summarizes the achievements obtained by this procedure. Detailed and rarely before documented temperature measurements from the rotating compressor wheel are published. As will be shown, the temperature measurements confirm the predictions from the predevelopment phase. A comparison of the temperature measurements from the recently developed compressor wheel with measurements carried out for a state-of-the-art wheel reveals the technological improvements achieved by this new generation of high-pressure compressor wheels.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCooling System of a High-Pressure Centrifugal Compressor: Development and Impact on Wheel Temperatures
    typeJournal Paper
    journal volume147
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4066733
    journal fristpage51009-1
    journal lastpage51009-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 005
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian