Influence of hydrogen on metals behavior. 1 - Mechanical behavior of Ti 6 pc Al 6 pc V 2 pc Sn titanium alloy versus hydrogen: influence of heat treatment and of oxygen content
Description
The mechanical behavior of Ti 6 pc Al 6 pc V Sn alloy during dynamic testing has been investigated versus hydrogen and oxygen content. The hydrogen susceptibility depends only slightly on its microstructure, acicular or equi-axed: it depends much more on conditions of hydrogen contamination and on the thermal history afterward. When the alloy has been stabilized by annealing in α - β and provided hydrogen absorption does not induce phase transformations, hydrogen sensitivity is relatively low: brittleness occurs suddenly but at a high concentration threshold (2000 ppm H), which coincides with hydrogen saturation of β phase. When the alloy includes unstabilized phases, its response to hydrogen changes whether it has been finally annealed or not, in the 300 - 500 C temperature area, prone to ω phase formation. In the absence of such an annealing, a reduction in ductility only occurs at high concentrations (> 1500 ppm H). In the other and, after annealing at 400 C, alloy hardening and a ductility decrease start even at the lowest hydrogen amounts: then hydrogen susceptibility is very high. Low oxygen concentration (up to 2000 ppm) do not sensibly affect the good hydrogen tolerance of this alloy. Beyond 2500 ppm, oxygen, while improving tensile strength, yet severely decreases ductility.
Abstract (French)
Le comportement mecanique de l'alliage TA6-V6-E2 lors d'un essai dynamique a ete etudie en fonction de la teneur en hydrogene et en oxygene. La sensibilite vis-a-vis de l'hydrogene ne depend que tres faiblement de sa structure migrographique, aciculaire ou equiaxe; elle depend bien plus des conditions de contamination par l'hydrogene et de son histoire thermique apres contamination. Lorsque l'alliage a ete stabilise par un recuit dans le domaine biphase, et a condition que l'absorption d'hydrogene n'entraine pas de modification structurale, la sensibilite vis-a-vis de l'hydrogene est relativement faible: la fragilite apparait brutalement mais pour un seuil de concentration eleve (2000 ppm H) qui coincide avec la saturation de la phases β en hydrogene. Lorsque l'alliage comporte des domaines non stabilises, sa reponse vis-a-vis de l'hydrogene depend de l'existence ou non d'un recuit final dans la zone de temperature 300-500 C, propice a la formation de phase ω. En l'absence d'un tel recuit, une diminution de la capacite de deformation ne se manifeste que pour des teneurs elevees (> 1500 ppm H). Par contre, si un recuit a 400 C a ete effectue, on observe un durcissement de l'alliage et une baisse de ductilite des les plus faibles teneurs en hydrogene: la sensibilite de l'alliage vis-a-vis de l'hydrogene est alors tres grande. De faibles quantites d'oxygene (jusqu'a 2000 ppm) n'affecte pas de facon sensible le bon comportement de cet alliage vis-a-vis de l'hydrogene. Au-dela de 2500 ppm, tout en ameliorant la resistance mecanique, l'oxygene diminue cependant fortement la capacite de deformation. (auteur)Files
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Additional details
Additional titles
- Original title (French)
- Influence de l'hydrogene sur le comportement des metaux. 1 - comportement mecanique de l'alliage de titane T A6 V6 E2 vis-a-vis de l'hydrogene: influence du traitement thermique et de la teneur en oxygene
Identifiers
Publishing Information
- Imprint Pagination
- 108 p.
- Report number
- CEA-R--4472
INIS
- Country of Publication
- France
- Country of Input or Organization
- France
- INIS RN
- 45026082
- Subject category
- S36: MATERIALS SCIENCE;
- Resource subtype / Literary indicator
- Thesis
- Descriptors DEI
- CHEMICAL COMPOSITION; HARDENING; HEAT TREATMENTS; HYDROGEN; HYDROGEN EMBRITTLEMENT; MECHANICAL PROPERTIES; METALLURGICAL EFFECTS; OXYGEN; TEMPERATURE DEPENDENCE; TITANIUM ALLOYS
- Descriptors DEC
- ALLOYS; ELEMENTS; EMBRITTLEMENT; NONMETALS; TRANSITION ELEMENT ALLOYS
Optional Information
- Notes
- 85 refs.; Available from the INIS Liaison Officer for France, see the 'INIS contacts' section of the INIS website for current contact and E-mail addresses: http://www.iaea.org/inis/contacts/