YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • 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

    Roughness Investigations on In-Service High-Pressure Compressor Blades—Part I: An Automated Process for High-Fidelity Roughness Measurements

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 008::page 81001-1
    Author:
    Vasilopoulos, Ilias
    ,
    Rostamian, Mirco
    ,
    Voigt, Matthias
    ,
    Meyer, Marcus
    ,
    Mailach, Ronald
    DOI: 10.1115/1.4067291
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The two-part publication deals with roughness investigations on in-service high-pressure compressor (HPC) blades, both in terms of measurements and simulations. In this article (Part I), an automated process for performing detailed surface roughness measurements of the blades has been developed. Specifically, a highly accurate Alicona sensor (20x lens; capable of capturing roughness values down to 0.1μm) was combined with a pick-and-place robotic arm, and the system was trained to conduct roughness measurements on all the different rotor blades of a 10-stage HPC. First, the Alicona measuring device is validated against a NanoFocus device of similar accuracy. Then, a detailed measurement of the roughness on the suction and pressure side of Rotor 2 is demonstrated, using a 100-point grid. This process is further accelerated by using a reduced number of measuring points. The location of those points has been determined by numerical optimization that aims at minimizing the error between a radial basis function (RBF)-based approximation model and the detailed measured roughness distribution. Finally, a summary of the roughness measurements through the entire HPC is given (rotors only; before and after cleaning of the blades at an ultrasonic bath) and the article ends with a discussion of the results.
    • Download: (1.084Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Roughness Investigations on In-Service High-Pressure Compressor Blades—Part I: An Automated Process for High-Fidelity Roughness Measurements

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4306020
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorVasilopoulos, Ilias
    contributor authorRostamian, Mirco
    contributor authorVoigt, Matthias
    contributor authorMeyer, Marcus
    contributor authorMailach, Ronald
    date accessioned2025-04-21T10:21:39Z
    date available2025-04-21T10:21:39Z
    date copyright1/13/2025 12:00:00 AM
    date issued2025
    identifier issn0889-504X
    identifier otherturbo_147_8_081001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306020
    description abstractThe two-part publication deals with roughness investigations on in-service high-pressure compressor (HPC) blades, both in terms of measurements and simulations. In this article (Part I), an automated process for performing detailed surface roughness measurements of the blades has been developed. Specifically, a highly accurate Alicona sensor (20x lens; capable of capturing roughness values down to 0.1μm) was combined with a pick-and-place robotic arm, and the system was trained to conduct roughness measurements on all the different rotor blades of a 10-stage HPC. First, the Alicona measuring device is validated against a NanoFocus device of similar accuracy. Then, a detailed measurement of the roughness on the suction and pressure side of Rotor 2 is demonstrated, using a 100-point grid. This process is further accelerated by using a reduced number of measuring points. The location of those points has been determined by numerical optimization that aims at minimizing the error between a radial basis function (RBF)-based approximation model and the detailed measured roughness distribution. Finally, a summary of the roughness measurements through the entire HPC is given (rotors only; before and after cleaning of the blades at an ultrasonic bath) and the article ends with a discussion of the results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRoughness Investigations on In-Service High-Pressure Compressor Blades—Part I: An Automated Process for High-Fidelity Roughness Measurements
    typeJournal Paper
    journal volume147
    journal issue8
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4067291
    journal fristpage81001-1
    journal lastpage81001-9
    page9
    treeJournal of Turbomachinery:;2025:;volume( 147 ):;issue: 008
    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