Gross slip fretting wear of CrCn, TiAlN, Ni, and CuNiIn coatings on Ti6A4V interfaces
Identifieur interne : 007925 ( Main/Repository ); précédent : 007924; suivant : 007926Gross slip fretting wear of CrCn, TiAlN, Ni, and CuNiIn coatings on Ti6A4V interfaces
Auteurs : RBID : Pascal:07-0450488Descripteurs français
- Pascal (Inist)
- Usure petit débattement, Microdéplacement, Tribologie, Amorçage fissure, Rupture, Lubrifiant solide, Endommagement, Température ambiante, Frottement sec, Aluminium nitrure, Titane nitrure, Revêtement métallique, Métal, Aube turbine, Turbine gaz, Turboréacteur, Compresseur, Projection plasma, Essai usure, Etude expérimentale, Essai endurance, Revêtement projection.
- Wicri :
- concept : Métal.
English descriptors
- KwdEn :
- Aluminium nitride, Compressor, Crack initiation, Damaging, Dry friction, Experimental study, Fretting wear, Gas turbine, Life test, Metal, Metal coating, Microdisplacement, Plasma spraying, Room temperature, Rupture, Solid lubricant, Sprayed coatings, Titanium nitride, Tribology, Turbine blade, Turbojet, Wear test.
Abstract
Fretting is a low amplitude oscillatory wear that occurs at component interfaces and can accelerate crack initiation as well as interfacial degradation. Prevalent in Ti-alloy contacts, fretting wear often occurs at the blade/disk interfaces of fan and compressor stages in turbine engines, causing premature component failure. In many cases, plasma sprayed CuNiIn (copper-nickel-indium) coatings and solid lubricants are applied to blade roots to mitigate the fretting problem. However, the CuNiIn coatings can cause severe damage to the uncoated Ti-alloy counter parts once the solid lubricants wear out. In this study, bench level gross slip fretting wear tests were conducted at room temperature on unlubricated Ti6A14V (titanium, 6% aluminum, 4% vanadium) surfaces mated with CuNiIn and commercially pure Ni plasma sprayed surfaces. Upon analysis, it was determined that the uncoated Ti6A14V surfaces initially gall. Then the resulting adherent wear particles break up causing a transition into a third body type wear mode over time. This leads to an accumulation of wear that is similar to that of uncoated Ti6A14V mating surfaces. Additional tests were conducted after applying 2-μm thick PVD deposited TiAlN (titanium-aluminium-nitride) and CrCN (chrome-carbon-nitride) coatings to the surfaces of a second set of Ti6A14V mating pairs. When worn against the unlubricated CuNiIn and Ni coatings, the thin TiAlN and CrCN coatings wore gradually without delaminating or cracking and were able to mitigate galling and extend test life. The application of the hard coatings lead to a reduction in wear in all of the tests except with the combination of TiAlN worn against CuNiIn.
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<record><TEI><teiHeader><fileDesc><titleStmt><title xml:lang="en" level="a">Gross slip fretting wear of CrCn, TiAlN, Ni, and CuNiIn coatings on Ti6A4V interfaces</title><author><name sortKey="Hager, C H Jr" uniqKey="Hager C">C. H. Jr Hager</name><affiliation wicri:level="1"><inist:fA14 i1="01"><s1>Universal Technology Corporation, 1270 North Fairfield Road</s1><s2>Dayton, OH 45432-2600</s2><s3>USA</s3><sZ>1 aut.</sZ></inist:fA14><country>États-Unis</country><wicri:noRegion>Dayton, OH 45432-2600</wicri:noRegion></affiliation></author><author><name sortKey="Sanders, J" uniqKey="Sanders J">J. Sanders</name><affiliation wicri:level="1"><inist:fA14 i1="02"><s1>2941 Hobson Way AFRL/MLBT, Wright Patterson Air Force Base</s1><s2>OH 45433-7750</s2><s3>USA</s3><sZ>2 aut.</sZ><sZ>3 aut.</sZ><sZ>4 aut.</sZ></inist:fA14><country>États-Unis</country><placeName><region type="state">Ohio</region></placeName></affiliation></author><author><name sortKey="Sharma, S" uniqKey="Sharma S">S. Sharma</name><affiliation wicri:level="1"><inist:fA14 i1="02"><s1>2941 Hobson Way AFRL/MLBT, Wright Patterson Air Force Base</s1><s2>OH 45433-7750</s2><s3>USA</s3><sZ>2 aut.</sZ><sZ>3 aut.</sZ><sZ>4 aut.</sZ></inist:fA14><country>États-Unis</country><placeName><region type="state">Ohio</region></placeName></affiliation></author><author><name sortKey="Voevodin, A" uniqKey="Voevodin A">A. Voevodin</name><affiliation wicri:level="1"><inist:fA14 i1="02"><s1>2941 Hobson Way AFRL/MLBT, Wright Patterson Air Force Base</s1><s2>OH 45433-7750</s2><s3>USA</s3><sZ>2 aut.</sZ><sZ>3 aut.</sZ><sZ>4 aut.</sZ></inist:fA14><country>États-Unis</country><placeName><region type="state">Ohio</region></placeName></affiliation></author></titleStmt><publicationStmt><idno type="inist">07-0450488</idno><date when="2007">2007</date><idno type="stanalyst">PASCAL 07-0450488 INIST</idno><idno type="RBID">Pascal:07-0450488</idno><idno type="wicri:Area/Main/Corpus">007372</idno><idno type="wicri:Area/Main/Repository">007925</idno></publicationStmt><seriesStmt><idno type="ISSN">0043-1648</idno><title level="j" type="abbreviated">Wear</title><title level="j" type="main">Wear</title></seriesStmt></fileDesc><profileDesc><textClass><keywords scheme="KwdEn" xml:lang="en"><term>Aluminium nitride</term><term>Compressor</term><term>Crack initiation</term><term>Damaging</term><term>Dry friction</term><term>Experimental study</term><term>Fretting wear</term><term>Gas turbine</term><term>Life test</term><term>Metal</term><term>Metal coating</term><term>Microdisplacement</term><term>Plasma spraying</term><term>Room temperature</term><term>Rupture</term><term>Solid lubricant</term><term>Sprayed coatings</term><term>Titanium nitride</term><term>Tribology</term><term>Turbine blade</term><term>Turbojet</term><term>Wear test</term></keywords><keywords scheme="Pascal" xml:lang="fr"><term>Usure petit débattement</term><term>Microdéplacement</term><term>Tribologie</term><term>Amorçage fissure</term><term>Rupture</term><term>Lubrifiant solide</term><term>Endommagement</term><term>Température ambiante</term><term>Frottement sec</term><term>Aluminium nitrure</term><term>Titane nitrure</term><term>Revêtement métallique</term><term>Métal</term><term>Aube turbine</term><term>Turbine gaz</term><term>Turboréacteur</term><term>Compresseur</term><term>Projection plasma</term><term>Essai usure</term><term>Etude expérimentale</term><term>Essai endurance</term><term>Revêtement projection</term></keywords><keywords scheme="Wicri" type="concept" xml:lang="fr"><term>Métal</term></keywords></textClass></profileDesc></teiHeader><front><div type="abstract" xml:lang="en">Fretting is a low amplitude oscillatory wear that occurs at component interfaces and can accelerate crack initiation as well as interfacial degradation. Prevalent in Ti-alloy contacts, fretting wear often occurs at the blade/disk interfaces of fan and compressor stages in turbine engines, causing premature component failure. In many cases, plasma sprayed CuNiIn (copper-nickel-indium) coatings and solid lubricants are applied to blade roots to mitigate the fretting problem. However, the CuNiIn coatings can cause severe damage to the uncoated Ti-alloy counter parts once the solid lubricants wear out. In this study, bench level gross slip fretting wear tests were conducted at room temperature on unlubricated Ti6A14V (titanium, 6% aluminum, 4% vanadium) surfaces mated with CuNiIn and commercially pure Ni plasma sprayed surfaces. Upon analysis, it was determined that the uncoated Ti6A14V surfaces initially gall. Then the resulting adherent wear particles break up causing a transition into a third body type wear mode over time. This leads to an accumulation of wear that is similar to that of uncoated Ti6A14V mating surfaces. Additional tests were conducted after applying 2-μm thick PVD deposited TiAlN (titanium-aluminium-nitride) and CrCN (chrome-carbon-nitride) coatings to the surfaces of a second set of Ti6A14V mating pairs. When worn against the unlubricated CuNiIn and Ni coatings, the thin TiAlN and CrCN coatings wore gradually without delaminating or cracking and were able to mitigate galling and extend test life. The application of the hard coatings lead to a reduction in wear in all of the tests except with the combination of TiAlN worn against CuNiIn.</div></front></TEI><inist><standard h6="B"><pA><fA01 i1="01" i2="1"><s0>0043-1648</s0></fA01><fA02 i1="01"><s0>WEARAH</s0></fA02><fA03 i2="1"><s0>Wear</s0></fA03><fA05><s2>263</s2></fA05><fA06><s2>1-6</s2></fA06><fA08 i1="01" i2="1" l="ENG"><s1>Gross slip fretting wear of CrCn, TiAlN, Ni, and CuNiIn coatings on Ti6A4V interfaces</s1></fA08><fA09 i1="01" i2="1" l="ENG"><s1>16th International Conference on Wear of Materials, Montreal, Canada, 15-17 April 2007</s1></fA09><fA11 i1="01" i2="1"><s1>HAGER (C. H. JR)</s1></fA11><fA11 i1="02" i2="1"><s1>SANDERS (J.)</s1></fA11><fA11 i1="03" i2="1"><s1>SHARMA (S.)</s1></fA11><fA11 i1="04" i2="1"><s1>VOEVODIN (A.)</s1></fA11><fA12 i1="01" i2="1"><s1>LUDEMA (Kenneth C.)</s1><s9>ed.</s9></fA12><fA12 i1="02" i2="1"><s1>SHAFFER (Steven J.)</s1><s9>ed.</s9></fA12><fA14 i1="01"><s1>Universal Technology Corporation, 1270 North Fairfield Road</s1><s2>Dayton, OH 45432-2600</s2><s3>USA</s3><sZ>1 aut.</sZ></fA14><fA14 i1="02"><s1>2941 Hobson Way AFRL/MLBT, Wright Patterson Air Force Base</s1><s2>OH 45433-7750</s2><s3>USA</s3><sZ>2 aut.</sZ><sZ>3 aut.</sZ><sZ>4 aut.</sZ></fA14><fA15 i1="01"><s1>University of Michigan-Ann Arbor</s1><s3>USA</s3><sZ>1 aut.</sZ></fA15><fA15 i1="02"><s1>Battelle Memorial Institute-Columbus, Ohio</s1><s3>USA</s3><sZ>2 aut.</sZ></fA15><fA20><s1>430-443</s1></fA20><fA21><s1>2007</s1></fA21><fA23 i1="01"><s0>ENG</s0></fA23><fA43 i1="01"><s1>INIST</s1><s2>8579</s2><s5>354000162425970510</s5></fA43><fA44><s0>0000</s0><s1>© 2007 INIST-CNRS. All rights reserved.</s1></fA44><fA45><s0>15 ref.</s0></fA45><fA47 i1="01" i2="1"><s0>07-0450488</s0></fA47><fA60><s1>P</s1><s2>C</s2></fA60><fA61><s0>A</s0></fA61><fA64 i1="01" i2="1"><s0>Wear</s0></fA64><fA66 i1="01"><s0>CHE</s0></fA66><fC01 i1="01" l="ENG"><s0>Fretting is a low amplitude oscillatory wear that occurs at component interfaces and can accelerate crack initiation as well as interfacial degradation. Prevalent in Ti-alloy contacts, fretting wear often occurs at the blade/disk interfaces of fan and compressor stages in turbine engines, causing premature component failure. In many cases, plasma sprayed CuNiIn (copper-nickel-indium) coatings and solid lubricants are applied to blade roots to mitigate the fretting problem. However, the CuNiIn coatings can cause severe damage to the uncoated Ti-alloy counter parts once the solid lubricants wear out. In this study, bench level gross slip fretting wear tests were conducted at room temperature on unlubricated Ti6A14V (titanium, 6% aluminum, 4% vanadium) surfaces mated with CuNiIn and commercially pure Ni plasma sprayed surfaces. Upon analysis, it was determined that the uncoated Ti6A14V surfaces initially gall. Then the resulting adherent wear particles break up causing a transition into a third body type wear mode over time. This leads to an accumulation of wear that is similar to that of uncoated Ti6A14V mating surfaces. Additional tests were conducted after applying 2-μm thick PVD deposited TiAlN (titanium-aluminium-nitride) and CrCN (chrome-carbon-nitride) coatings to the surfaces of a second set of Ti6A14V mating pairs. When worn against the unlubricated CuNiIn and Ni coatings, the thin TiAlN and CrCN coatings wore gradually without delaminating or cracking and were able to mitigate galling and extend test life. 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