Fully suspended, five-axis, three-magnetic-bearing dynamic spin rig with forced excitation
A significant advancement in the dynamic spin rig (DSR), i.e., the five-axis, three-magnetic-bearing DSR, is used to perform vibration tests of turbomachinery blades and components under rotating and non-rotating conditions in a vacuum. The rig has three magnetic bearings as its critical components:...
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Veröffentlicht in: | Experimental mechanics 2005-06, Vol.45 (3), p.226-237 |
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creator | MORRISON, C. R PROVENZA, A KURKOV, A MONTAGUE, G DUFFY, K MEHMED, O JOHNSON, D JANSEN, R |
description | A significant advancement in the dynamic spin rig (DSR), i.e., the five-axis, three-magnetic-bearing DSR, is used to perform vibration tests of turbomachinery blades and components under rotating and non-rotating conditions in a vacuum. The rig has three magnetic bearings as its critical components: two heteropolar radial active magnetic bearings and a magnetic thrust bearing. The bearing configuration allows full vertical rotor magnetic suspension along with a feedforward control feature, which enables the excitation of various modes of vibration in the bladed disk test articles. The theoretical, mechanical, electrical, and electronic aspects of the rig are discussed. Also presented are the forced-excitation results of a fully levitated, rotating and non-rotating, unbladed rotor and a fully levitated, rotating and non-rotating, bladed rotor in which a pair of blades were arranged 180 deg apart from each other. These tests include the 'bounce' mode excitation of the rotor in which the rotor was excited at the blade natural frequency of 144 Hz. The rotor natural mode frequency of 355 Hz was discerned from the plot of acceleration versus frequency. For non-rotating blades, a blade-tip excitation amplitude of approximately 100 g A was achieved at the first-bending critical ({approximately equal to}144 Hz) and at the first-torsional and second-bending blade modes. A blade-tip displacement of 1.778X10m (70 mils) was achieved at the first-bending critical by exciting the blades at a forced-excitation phase angle of 90 deg relative to the vertical plane containing the blades while simultaneously rotating the shaft at 3000 rpm. |
doi_str_mv | 10.1007/BF02427946 |
format | Article |
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R ; PROVENZA, A ; KURKOV, A ; MONTAGUE, G ; DUFFY, K ; MEHMED, O ; JOHNSON, D ; JANSEN, R</creator><creatorcontrib>MORRISON, C. R ; PROVENZA, A ; KURKOV, A ; MONTAGUE, G ; DUFFY, K ; MEHMED, O ; JOHNSON, D ; JANSEN, R</creatorcontrib><description>A significant advancement in the dynamic spin rig (DSR), i.e., the five-axis, three-magnetic-bearing DSR, is used to perform vibration tests of turbomachinery blades and components under rotating and non-rotating conditions in a vacuum. The rig has three magnetic bearings as its critical components: two heteropolar radial active magnetic bearings and a magnetic thrust bearing. The bearing configuration allows full vertical rotor magnetic suspension along with a feedforward control feature, which enables the excitation of various modes of vibration in the bladed disk test articles. The theoretical, mechanical, electrical, and electronic aspects of the rig are discussed. Also presented are the forced-excitation results of a fully levitated, rotating and non-rotating, unbladed rotor and a fully levitated, rotating and non-rotating, bladed rotor in which a pair of blades were arranged 180 deg apart from each other. These tests include the 'bounce' mode excitation of the rotor in which the rotor was excited at the blade natural frequency of 144 Hz. The rotor natural mode frequency of 355 Hz was discerned from the plot of acceleration versus frequency. For non-rotating blades, a blade-tip excitation amplitude of approximately 100 g A was achieved at the first-bending critical ({approximately equal to}144 Hz) and at the first-torsional and second-bending blade modes. A blade-tip displacement of 1.778X10m (70 mils) was achieved at the first-bending critical by exciting the blades at a forced-excitation phase angle of 90 deg relative to the vertical plane containing the blades while simultaneously rotating the shaft at 3000 rpm.</description><identifier>ISSN: 0014-4851</identifier><identifier>EISSN: 1741-2765</identifier><identifier>DOI: 10.1007/BF02427946</identifier><identifier>CODEN: EXMCAZ</identifier><language>eng</language><publisher>Heidelberg: Springer</publisher><subject>Applied sciences ; Bearings, bushings, rolling bearings ; Drives ; Equipment and supplies ; Exact sciences and technology ; Fundamental areas of phenomenology (including applications) ; Measurement and testing methods ; Mechanical engineering. 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R</creatorcontrib><creatorcontrib>PROVENZA, A</creatorcontrib><creatorcontrib>KURKOV, A</creatorcontrib><creatorcontrib>MONTAGUE, G</creatorcontrib><creatorcontrib>DUFFY, K</creatorcontrib><creatorcontrib>MEHMED, O</creatorcontrib><creatorcontrib>JOHNSON, D</creatorcontrib><creatorcontrib>JANSEN, R</creatorcontrib><title>Fully suspended, five-axis, three-magnetic-bearing dynamic spin rig with forced excitation</title><title>Experimental mechanics</title><description>A significant advancement in the dynamic spin rig (DSR), i.e., the five-axis, three-magnetic-bearing DSR, is used to perform vibration tests of turbomachinery blades and components under rotating and non-rotating conditions in a vacuum. The rig has three magnetic bearings as its critical components: two heteropolar radial active magnetic bearings and a magnetic thrust bearing. The bearing configuration allows full vertical rotor magnetic suspension along with a feedforward control feature, which enables the excitation of various modes of vibration in the bladed disk test articles. The theoretical, mechanical, electrical, and electronic aspects of the rig are discussed. Also presented are the forced-excitation results of a fully levitated, rotating and non-rotating, unbladed rotor and a fully levitated, rotating and non-rotating, bladed rotor in which a pair of blades were arranged 180 deg apart from each other. These tests include the 'bounce' mode excitation of the rotor in which the rotor was excited at the blade natural frequency of 144 Hz. The rotor natural mode frequency of 355 Hz was discerned from the plot of acceleration versus frequency. For non-rotating blades, a blade-tip excitation amplitude of approximately 100 g A was achieved at the first-bending critical ({approximately equal to}144 Hz) and at the first-torsional and second-bending blade modes. A blade-tip displacement of 1.778X10m (70 mils) was achieved at the first-bending critical by exciting the blades at a forced-excitation phase angle of 90 deg relative to the vertical plane containing the blades while simultaneously rotating the shaft at 3000 rpm.</description><subject>Applied sciences</subject><subject>Bearings, bushings, rolling bearings</subject><subject>Drives</subject><subject>Equipment and supplies</subject><subject>Exact sciences and technology</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Measurement and testing methods</subject><subject>Mechanical engineering. Machine design</subject><subject>Physics</subject><subject>Rotors</subject><subject>Shafts, couplings, clutches, brakes</subject><subject>Solid mechanics</subject><subject>Structural and continuum mechanics</subject><subject>Technology application</subject><subject>Vibration tests</subject><subject>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</subject><issn>0014-4851</issn><issn>1741-2765</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2005</creationdate><recordtype>article</recordtype><recordid>eNptkUFLAzEQhYMoWKsXf0FA9CCuJtlssjlqsSoIXvTiZZlNZmtkm63JVtt_75YKIsjADAzfG97wCDnm7JIzpq9upkxIoY1UO2TEteSZ0KrYJSPGuMxkWfB9cpDSOxvgXIsReZ0u23ZN0zItMDh0F7Txn5jByqcL2r9FxGwOs4C9t1mNEH2YUbcOMPeWpoUPNPoZ_fL9G226aNFRXFnfQ--7cEj2GmgTHv3MMXmZ3j5P7rPHp7uHyfVjZkVp-kxY19S5QMuVKpHnkiGqGkBDbYQ0hZU4NC7BOlMKobAAB47VyFkpC2byMTnb3l3E7mOJqa_mPllsWwjYLVMlTMmUyPUAnmzBGbRY-dB0fQS7gatrLjnLtSnEQF3-Qw3lcHi6C9j4Yf9HcL4V2NilFLGpFtHPIa4rzqpNKtVvKgN8-mMWkoW2iRCsT78KpY3Kuc6_Aelwivo</recordid><startdate>20050601</startdate><enddate>20050601</enddate><creator>MORRISON, C. 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R ; PROVENZA, A ; KURKOV, A ; MONTAGUE, G ; DUFFY, K ; MEHMED, O ; JOHNSON, D ; JANSEN, R</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c289t-2cdfb32ec1668e1340ee6baa7ab92495c4e95c14acd98226e5adad0be10845093</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2005</creationdate><topic>Applied sciences</topic><topic>Bearings, bushings, rolling bearings</topic><topic>Drives</topic><topic>Equipment and supplies</topic><topic>Exact sciences and technology</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Measurement and testing methods</topic><topic>Mechanical engineering. Machine design</topic><topic>Physics</topic><topic>Rotors</topic><topic>Shafts, couplings, clutches, brakes</topic><topic>Solid mechanics</topic><topic>Structural and continuum mechanics</topic><topic>Technology application</topic><topic>Vibration tests</topic><topic>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>MORRISON, C. R</creatorcontrib><creatorcontrib>PROVENZA, A</creatorcontrib><creatorcontrib>KURKOV, A</creatorcontrib><creatorcontrib>MONTAGUE, G</creatorcontrib><creatorcontrib>DUFFY, K</creatorcontrib><creatorcontrib>MEHMED, O</creatorcontrib><creatorcontrib>JOHNSON, D</creatorcontrib><creatorcontrib>JANSEN, R</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Experimental mechanics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>MORRISON, C. R</au><au>PROVENZA, A</au><au>KURKOV, A</au><au>MONTAGUE, G</au><au>DUFFY, K</au><au>MEHMED, O</au><au>JOHNSON, D</au><au>JANSEN, R</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Fully suspended, five-axis, three-magnetic-bearing dynamic spin rig with forced excitation</atitle><jtitle>Experimental mechanics</jtitle><date>2005-06-01</date><risdate>2005</risdate><volume>45</volume><issue>3</issue><spage>226</spage><epage>237</epage><pages>226-237</pages><issn>0014-4851</issn><eissn>1741-2765</eissn><coden>EXMCAZ</coden><abstract>A significant advancement in the dynamic spin rig (DSR), i.e., the five-axis, three-magnetic-bearing DSR, is used to perform vibration tests of turbomachinery blades and components under rotating and non-rotating conditions in a vacuum. The rig has three magnetic bearings as its critical components: two heteropolar radial active magnetic bearings and a magnetic thrust bearing. The bearing configuration allows full vertical rotor magnetic suspension along with a feedforward control feature, which enables the excitation of various modes of vibration in the bladed disk test articles. The theoretical, mechanical, electrical, and electronic aspects of the rig are discussed. Also presented are the forced-excitation results of a fully levitated, rotating and non-rotating, unbladed rotor and a fully levitated, rotating and non-rotating, bladed rotor in which a pair of blades were arranged 180 deg apart from each other. These tests include the 'bounce' mode excitation of the rotor in which the rotor was excited at the blade natural frequency of 144 Hz. The rotor natural mode frequency of 355 Hz was discerned from the plot of acceleration versus frequency. For non-rotating blades, a blade-tip excitation amplitude of approximately 100 g A was achieved at the first-bending critical ({approximately equal to}144 Hz) and at the first-torsional and second-bending blade modes. A blade-tip displacement of 1.778X10m (70 mils) was achieved at the first-bending critical by exciting the blades at a forced-excitation phase angle of 90 deg relative to the vertical plane containing the blades while simultaneously rotating the shaft at 3000 rpm.</abstract><cop>Heidelberg</cop><pub>Springer</pub><doi>10.1007/BF02427946</doi><tpages>12</tpages></addata></record> |
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subjects | Applied sciences Bearings, bushings, rolling bearings Drives Equipment and supplies Exact sciences and technology Fundamental areas of phenomenology (including applications) Measurement and testing methods Mechanical engineering. Machine design Physics Rotors Shafts, couplings, clutches, brakes Solid mechanics Structural and continuum mechanics Technology application Vibration tests Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...) |
title | Fully suspended, five-axis, three-magnetic-bearing dynamic spin rig with forced excitation |
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