Effect of Ni3Al Coating on Vibration Suppression of Beams of Various Thicknesses

High cycle fatigue (HCF) caused by the vibratory stresses is the main cause of failure in many machine components, e.g. aircraft engine and gas turbine components, which has caused loss of many lives and billions of dollars. To avoid these kind of failures, vibratory stresses should be attenuated to...

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Published inKey engineering materials Vol. 875; pp. 294 - 301
Main Authors Nadeem, Shoaib, Aziz, Imran, Mehmood, Khalid, Saeed, Hasan Aftab
Format Journal Article
LanguageEnglish
Published Zurich Trans Tech Publications Ltd 04.02.2021
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Abstract High cycle fatigue (HCF) caused by the vibratory stresses is the main cause of failure in many machine components, e.g. aircraft engine and gas turbine components, which has caused loss of many lives and billions of dollars. To avoid these kind of failures, vibratory stresses should be attenuated to an acceptable level, especially at resonant frequencies. A lot of previous studies have shown that thin coatings of different materials significantly reduced these vibratory stresses by adding extra damping to the system. These include viscoelastic materials, plasma graded coatings, piezoelectric materials, and magneto-mechanical damping material coatings, but some of these had applicability and performance issues. Among these thin coatings, magneto-mechanical materials are very effective in reducing these vibratory stresses significantly.In this study, the effect of different beam structure thicknesses under same magneto-mechanical coating of 0.2mm was studied. For this purpose, Ni3Al was applied as magneto-mechanical coating. The natural frequencies, damping ratios and displacements of beams were calculated before and after applying magneto-mechanical coatings using forced response analysis and hammer tests. The results indicated a sharp change in vibration characteristics i.e. natural frequency, damping ratio and beam deflections, of all the beams used. The results showed that the magneto-mechanical coatings were more effective when applied to thin structures as compared to thick structures, because thin structures have higher strains, which enabled magneto-mechanical coatings to dissipate larger amounts of energy of applied loadings, because performance of these coatings is strain dependent.
AbstractList High cycle fatigue (HCF) caused by the vibratory stresses is the main cause of failure in many machine components, e.g. aircraft engine and gas turbine components, which has caused loss of many lives and billions of dollars. To avoid these kind of failures, vibratory stresses should be attenuated to an acceptable level, especially at resonant frequencies. A lot of previous studies have shown that thin coatings of different materials significantly reduced these vibratory stresses by adding extra damping to the system. These include viscoelastic materials, plasma graded coatings, piezoelectric materials, and magneto-mechanical damping material coatings, but some of these had applicability and performance issues. Among these thin coatings, magneto-mechanical materials are very effective in reducing these vibratory stresses significantly.In this study, the effect of different beam structure thicknesses under same magneto-mechanical coating of 0.2mm was studied. For this purpose, Ni 3 Al was applied as magneto-mechanical coating. The natural frequencies, damping ratios and displacements of beams were calculated before and after applying magneto-mechanical coatings using forced response analysis and hammer tests. The results indicated a sharp change in vibration characteristics i.e. natural frequency, damping ratio and beam deflections, of all the beams used. The results showed that the magneto-mechanical coatings were more effective when applied to thin structures as compared to thick structures, because thin structures have higher strains, which enabled magneto-mechanical coatings to dissipate larger amounts of energy of applied loadings, because performance of these coatings is strain dependent.
High cycle fatigue (HCF) caused by the vibratory stresses is the main cause of failure in many machine components, e.g. aircraft engine and gas turbine components, which has caused loss of many lives and billions of dollars. To avoid these kind of failures, vibratory stresses should be attenuated to an acceptable level, especially at resonant frequencies. A lot of previous studies have shown that thin coatings of different materials significantly reduced these vibratory stresses by adding extra damping to the system. These include viscoelastic materials, plasma graded coatings, piezoelectric materials, and magneto-mechanical damping material coatings, but some of these had applicability and performance issues. Among these thin coatings, magneto-mechanical materials are very effective in reducing these vibratory stresses significantly.In this study, the effect of different beam structure thicknesses under same magneto-mechanical coating of 0.2mm was studied. For this purpose, Ni3Al was applied as magneto-mechanical coating. The natural frequencies, damping ratios and displacements of beams were calculated before and after applying magneto-mechanical coatings using forced response analysis and hammer tests. The results indicated a sharp change in vibration characteristics i.e. natural frequency, damping ratio and beam deflections, of all the beams used. The results showed that the magneto-mechanical coatings were more effective when applied to thin structures as compared to thick structures, because thin structures have higher strains, which enabled magneto-mechanical coatings to dissipate larger amounts of energy of applied loadings, because performance of these coatings is strain dependent.
Author Aziz, Imran
Saeed, Hasan Aftab
Mehmood, Khalid
Nadeem, Shoaib
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Cites_doi 10.1016/s0925-8388(00)00938-5
10.4271/2004-01-0745
10.1115/fuelcell2017-ns
10.1115/1.4010774
10.2514/6.1997-1154
10.2514/6.1998-3863
10.1063/1.1656551
10.1063/1.1657370
10.2320/matertrans.44.1671
10.2514/3.60284
10.1016/j.jallcom.2009.01.134
10.1007/bf02725326
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Keywords Vibratory Stresses
High Cycle Fatigue
Magneto-Mechanical Material Coating
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References Yin (4139656); 44
4139662
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4072128
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– ident: 4139657
  doi: 10.1016/s0925-8388(00)00938-5
– ident: 4141239
  doi: 10.4271/2004-01-0745
– ident: 4072130
  doi: 10.1115/fuelcell2017-ns
– ident: 4139660
  doi: 10.1115/1.4010774
– ident: 4072126
  doi: 10.2514/6.1997-1154
– ident: 4072127
  doi: 10.2514/6.1998-3863
– volume: 39
  start-page: 2311
  issn: 1089-7550
  issue: 5
  ident: 4139661
  article-title: Effect of Internal Stress Distribution on Magnetomechanical Damping
  publication-title: Journal of Applied Physics
  doi: 10.1063/1.1656551
– ident: 4139662
  doi: 10.1063/1.1657370
– volume: 44
  start-page: 1671
  issn: 1347-5320
  issue: 9
  ident: 4139656
  article-title: The Damping Behavior of Ni Added Mn-Cu Damping Alloys
  publication-title: MATERIALS TRANSACTIONS
  doi: 10.2320/matertrans.44.1671
– volume: 10
  start-page: 689
  issn: 1533-3868
  issue: 11
  ident: 4139654
  article-title: Potential of Graded Coatings in Vibration Damping
  publication-title: Journal of Aircraft
  doi: 10.2514/3.60284
– ident: 4139658
  doi: 10.1016/j.jallcom.2009.01.134
– volume: 42
  start-page: 407
  issn: 1573-8973
  issue: 10
  ident: 4139659
  article-title: Effect of plasma coatings on the damping properties of structural steels
  publication-title: Metal Science and Heat Treatment
  doi: 10.1007/bf02725326
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Snippet High cycle fatigue (HCF) caused by the vibratory stresses is the main cause of failure in many machine components, e.g. aircraft engine and gas turbine...
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SubjectTerms Aircraft engines
Aircraft vibration
Coating effects
Damping ratio
Fatigue failure
Gas turbines
High cycle fatigue
Nickel aluminides
Piezoelectricity
Resonant frequencies
Strain
Thickness
Vibration analysis
Vibration control
Vibration damping
Vibratory stresses
Viscoelastic materials
Title Effect of Ni3Al Coating on Vibration Suppression of Beams of Various Thicknesses
URI https://www.scientific.net/KEM.875.294
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