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    KnowledgeBased Process Design Optimization in Blisk Manufacturing

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 011::page 111011
    Author:
    Landwehr, Markus;Ganser, Philipp;Vinogradov, Georg;Bergs, Thomas
    DOI: 10.1115/1.4055496
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The manufacturing process of bladeintegrated disks (blisks) represents one of the most challenging tasks in turbomachinery manufacturing. The requirement is to machine complex, thinwalled blade geometries with high aspect ratios made of difficulttocut materials. In addition, extremely tight tolerances are required, since the smallest deviations can lead to a reduction in efficiency of the blisk in the later use. Nowadays, the rampup phase for the manufacturing of a new blisk is time and costintensive. To find a suitable manufacturing process that meets the required tolerances of the blisk, many experimental tests with different process parameters and strategies are necessary. The used approach is often trial and error, which offers limited testing opportunities, is timeconsuming and waste of resources. Therefore, the objective of this paper is to develop a knowledgebased process design optimization in blisk manufacturing. For this purpose, this paper picks up the results from our previous work. Based on these results, an experimental validation of the two process design tasks “number of blocks” and “block transition” is conducted. As part of the validation, the results of machining tests on a demonstrator blisk made of Inconel 718 are presented and discussed.
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      KnowledgeBased Process Design Optimization in Blisk Manufacturing

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4289040
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorLandwehr, Markus;Ganser, Philipp;Vinogradov, Georg;Bergs, Thomas
    date accessioned2023-04-06T13:05:04Z
    date available2023-04-06T13:05:04Z
    date copyright9/21/2022 12:00:00 AM
    date issued2022
    identifier issn7424795
    identifier othergtp_144_11_111011.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4289040
    description abstractThe manufacturing process of bladeintegrated disks (blisks) represents one of the most challenging tasks in turbomachinery manufacturing. The requirement is to machine complex, thinwalled blade geometries with high aspect ratios made of difficulttocut materials. In addition, extremely tight tolerances are required, since the smallest deviations can lead to a reduction in efficiency of the blisk in the later use. Nowadays, the rampup phase for the manufacturing of a new blisk is time and costintensive. To find a suitable manufacturing process that meets the required tolerances of the blisk, many experimental tests with different process parameters and strategies are necessary. The used approach is often trial and error, which offers limited testing opportunities, is timeconsuming and waste of resources. Therefore, the objective of this paper is to develop a knowledgebased process design optimization in blisk manufacturing. For this purpose, this paper picks up the results from our previous work. Based on these results, an experimental validation of the two process design tasks “number of blocks” and “block transition” is conducted. As part of the validation, the results of machining tests on a demonstrator blisk made of Inconel 718 are presented and discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleKnowledgeBased Process Design Optimization in Blisk Manufacturing
    typeJournal Paper
    journal volume144
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4055496
    journal fristpage111011
    journal lastpage1110115
    page5
    treeJournal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 011
    contenttypeFulltext
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