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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositorysid.inpe.br/marciana/2004/01.16.12.09
Last Update2004:03.29.03.00.00 (UTC) administrator
Metadata Repositorysid.inpe.br/marciana/2004/01.16.12.09.45
Metadata Last Update2018:06.05.01.20.48 (UTC) administrator
Secondary KeyINPE-10536-PRE/6008
Citation KeyReisPioBarNonSil:2003:InOxCr
TitleInfluence of the Oxidation in Creep of Ti-6Al-4V Alloy
FormatPapel
Year2003
Access Date2024, May 19
Secondary TypePRE CN
Number of Files1
Size310 KiB
2. Context
Author1 Reis, Danieli Aparecida Pereira
2 Piorino, F.
3 Barboza, M. J. R.
4 Nono, Maria do Carmo de Andrade
5 Silva, Carlos Roberto Marton
Resume Identifier1
2
3
4 8JMKD3MGP5W/3C9JHRC
Group1 LAS-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais, Lab. Materiais e Sensores, São José dos Campos, Brasil.
2 Centro Técnico Aeroespacial, Instituto de Aeronáutica e Espaço, São José dos Campos, Brasil.
3 Departamento de Engenharia de Materiais, Faculdade de Engenharia Química de Lorena, Lorena, Brasil.
4 danieli@las.inpe.br
Conference NameCongresso da Sociedade Brasileira de Microscopia e Microanálise, 19 (CSBMM).
Conference LocationCaxambú, 2003
Dateset. 2003
PublisherINPE
Book TitleProceedings
History (UTC)2018-06-05 01:20:48 :: administrator -> marciana :: 2003
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Keywordstitanium
oxidation
high resolution X-Ray diffraction
AbstractThe Ti-6Al-4V alloy is the most important of the titanium alloys used in engineering, combining excellent formability, weldability and a range of attractive physico-chemical properties such as good corrosion resistance and good metallurgical stability [1]. Ti-6Al-4V is currently used in aeronautic and aerospace industry mainly for applications that require resistance at high temperature such as, blades for aircraft turbines and steam turbine blades [2]. The titanium affinity by oxygen is one of main factors that limit the application of their alloys as structural materials at high temperatures. The oxidation produce a material loss through the growth of the oxide layer and the hardening by oxygen dissolution [3-4]. Notables advances have been observed in the development of titanium alloys with the objective of improving the specific high temperature strength and creep-resistance properties. However, the surface oxidation limits the use of these alloys in temperatures up to 600ºC [5]. The objective of this work was estimate the influence of the oxidation in the lifetime in creep of the Ti-6Al-4V alloy. The samples were analyzed by High Resolution X-Ray Diffraction, Scanning Electronic Microscopy (SEM), Atomic Force Microscopy (AFM) and microhardness test. The samples of Ti-6Al-4V were polished and treated during 24 hours at 600°C and observed the oxidation behavior in each case using argon, nitrogen and air atmospheres. The figure 1 shows microstructures obtained by SEM of one sample without treatment and one treated at 600°C in air atmosphere. In samples tested in argon and nitrogen atmospheres the microstructure were very similar to the sample no treated. The oxidation was more aggressive in air atmosphere, forming TiO2 film in the surface, observed by High Resolution X-Ray Diffraction and the sample color was dark gray. In argon and nitrogen atmospheres the oxidation suffered by material was not detected by High Resolution X-Ray Diffraction, just color change was observed (blue in argon and yellow in nitrogen). The oxidation layer was approximately 0,81µm and its surface roughness was approximately 22 nm in the case of highest oxidation when formed TiO2 film (figure 2). The samples microhardness was 781 HV to air atmosphere; 495 HV to nitrogen atmosphere and 393 HV to the alloy treated in argon atmosphere, showing that the oxidation brought to the microhardness increasing. Using the Ti-6Al-4V alloy produced specimens to creep test. The specimens were tested by creep at 600ºC in argon, nitrogen and air atmospheres using 250 MPa. The figure 3 shows the creep curves obtained. When the Ti-6Al-4V was treated in argon and nitrogen atmospheres the effect the oxidation is smallest and the behavior of the creep curves shows that the lifetime increases when these atmospheres were used. Also a ductility increase (final strain) observed when these protective atmospheres were applied. Occurs a decreasing of steady state creep in function of the reduction of oxidation process, showing that for the Ti-6Al-4V alloy their lifetime is strongly affected by the atmosphere that is submitted because the oxidation suffered by the material.
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/sid.inpe.br/marciana/2004/01.16.12.09
zipped data URLhttp://urlib.net/zip/sid.inpe.br/marciana/2004/01.16.12.09
Languageen
Target FileReis-CSBMM2003.pdf
User Groupadministrator
Visibilityshown
Copy HolderSID/SCD
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ESR3H2
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.55.40 1
Host Collectionsid.inpe.br/banon/2003/08.15.17.40
6. Notes
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7. Description control
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