Reduced-Order Modeling of Bladed Disks Considering Small Mistuning of the Disk Sectors
A model order reduction method based on the component mode synthesis for mistuned bladed disks is introduced, with one component for the disk and one component for each blade. The interface between the components at the blade roots is reduced using the wave-based substructuring (WBS) method, which e...
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Veröffentlicht in: | Journal of engineering for gas turbines and power 2019-05, Vol.141 (5) |
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container_title | Journal of engineering for gas turbines and power |
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creator | Schwerdt, Lukas Willeke, Sebastian Scheidt, Lars Panning-von Wallaschek, Jörg |
description | A model order reduction method based on the component mode synthesis for mistuned bladed disks is introduced, with one component for the disk and one component for each blade. The interface between the components at the blade roots is reduced using the wave-based substructuring (WBS) method, which employs tuned system modes. These system modes are calculated first, and used subsequently during the reduction of the individual components, which eliminates the need to build a partially reduced intermediate model with dense matrices. For the disk, a cyclic Craig–Bampton (CB) reduction is applied. The deviations of the stiffness and mass matrices of individual disk sectors are then projected into the cyclic basis of interior and interface modes of the disk substructure. Thereby, it is possible to model small disk mistuning in addition to large mistuning of the blades. |
doi_str_mv | 10.1115/1.4041071 |
format | Article |
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The interface between the components at the blade roots is reduced using the wave-based substructuring (WBS) method, which employs tuned system modes. These system modes are calculated first, and used subsequently during the reduction of the individual components, which eliminates the need to build a partially reduced intermediate model with dense matrices. For the disk, a cyclic Craig–Bampton (CB) reduction is applied. The deviations of the stiffness and mass matrices of individual disk sectors are then projected into the cyclic basis of interior and interface modes of the disk substructure. Thereby, it is possible to model small disk mistuning in addition to large mistuning of the blades.</description><identifier>ISSN: 0742-4795</identifier><identifier>EISSN: 1528-8919</identifier><identifier>DOI: 10.1115/1.4041071</identifier><language>eng</language><publisher>ASME</publisher><subject>Gas Turbines: Structures and Dynamics</subject><ispartof>Journal of engineering for gas turbines and power, 2019-05, Vol.141 (5)</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a249t-a796e3c86bd0811b33fa6157f7e1840f125a922cb53592a49213761d1ff8f7403</citedby><cites>FETCH-LOGICAL-a249t-a796e3c86bd0811b33fa6157f7e1840f125a922cb53592a49213761d1ff8f7403</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904,38499</link.rule.ids></links><search><creatorcontrib>Schwerdt, Lukas</creatorcontrib><creatorcontrib>Willeke, Sebastian</creatorcontrib><creatorcontrib>Scheidt, Lars Panning-von</creatorcontrib><creatorcontrib>Wallaschek, Jörg</creatorcontrib><title>Reduced-Order Modeling of Bladed Disks Considering Small Mistuning of the Disk Sectors</title><title>Journal of engineering for gas turbines and power</title><addtitle>J. Eng. Gas Turbines Power</addtitle><description>A model order reduction method based on the component mode synthesis for mistuned bladed disks is introduced, with one component for the disk and one component for each blade. The interface between the components at the blade roots is reduced using the wave-based substructuring (WBS) method, which employs tuned system modes. These system modes are calculated first, and used subsequently during the reduction of the individual components, which eliminates the need to build a partially reduced intermediate model with dense matrices. For the disk, a cyclic Craig–Bampton (CB) reduction is applied. The deviations of the stiffness and mass matrices of individual disk sectors are then projected into the cyclic basis of interior and interface modes of the disk substructure. Thereby, it is possible to model small disk mistuning in addition to large mistuning of the blades.</description><subject>Gas Turbines: Structures and Dynamics</subject><issn>0742-4795</issn><issn>1528-8919</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNot0LtPwzAQBnALgUQoDMwsXhlSfH7E8QjhKbWqRIHVcmIbUvJAdjLw35PSTDfcT9-dPoQugSwBQNzAkhMORMIRSkDQPM0VqGOUEMlpyqUSp-gsxh0hwBiXCfp4dXasnE03wbqA1711Td194t7ju8ZYZ_F9Hb8jLvou1pPY77ataRq8ruMwdrMdvtw_xFtXDX2I5-jEmya6i3ku0Pvjw1vxnK42Ty_F7So1lKshNVJljlV5VlqSA5SMeZOBkF46yDnxQIVRlFalYEJRwxUFJjOw4H3uJSdsga4PuVXoYwzO659Qtyb8aiB6X4gGPRcy2auDNbF1etePoZte0yybLlH2ByJ6Wis</recordid><startdate>20190501</startdate><enddate>20190501</enddate><creator>Schwerdt, Lukas</creator><creator>Willeke, Sebastian</creator><creator>Scheidt, Lars Panning-von</creator><creator>Wallaschek, Jörg</creator><general>ASME</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20190501</creationdate><title>Reduced-Order Modeling of Bladed Disks Considering Small Mistuning of the Disk Sectors</title><author>Schwerdt, Lukas ; Willeke, Sebastian ; Scheidt, Lars Panning-von ; Wallaschek, Jörg</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a249t-a796e3c86bd0811b33fa6157f7e1840f125a922cb53592a49213761d1ff8f7403</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Gas Turbines: Structures and Dynamics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Schwerdt, Lukas</creatorcontrib><creatorcontrib>Willeke, Sebastian</creatorcontrib><creatorcontrib>Scheidt, Lars Panning-von</creatorcontrib><creatorcontrib>Wallaschek, Jörg</creatorcontrib><collection>CrossRef</collection><jtitle>Journal of engineering for gas turbines and power</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Schwerdt, Lukas</au><au>Willeke, Sebastian</au><au>Scheidt, Lars Panning-von</au><au>Wallaschek, Jörg</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Reduced-Order Modeling of Bladed Disks Considering Small Mistuning of the Disk Sectors</atitle><jtitle>Journal of engineering for gas turbines and power</jtitle><stitle>J. Eng. Gas Turbines Power</stitle><date>2019-05-01</date><risdate>2019</risdate><volume>141</volume><issue>5</issue><issn>0742-4795</issn><eissn>1528-8919</eissn><abstract>A model order reduction method based on the component mode synthesis for mistuned bladed disks is introduced, with one component for the disk and one component for each blade. The interface between the components at the blade roots is reduced using the wave-based substructuring (WBS) method, which employs tuned system modes. These system modes are calculated first, and used subsequently during the reduction of the individual components, which eliminates the need to build a partially reduced intermediate model with dense matrices. For the disk, a cyclic Craig–Bampton (CB) reduction is applied. The deviations of the stiffness and mass matrices of individual disk sectors are then projected into the cyclic basis of interior and interface modes of the disk substructure. Thereby, it is possible to model small disk mistuning in addition to large mistuning of the blades.</abstract><pub>ASME</pub><doi>10.1115/1.4041071</doi></addata></record> |
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subjects | Gas Turbines: Structures and Dynamics |
title | Reduced-Order Modeling of Bladed Disks Considering Small Mistuning of the Disk Sectors |
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