Hostname: page-component-848d4c4894-wzw2p Total loading time: 0 Render date: 2024-05-13T02:20:09.614Z Has data issue: false hasContentIssue false
  • English
  • Français

Nondestructive Evaluation of Fatigue in Titanium Alloys

Published online by Cambridge University Press:  10 February 2011

H. Rösner ,
N. Meyendorf ,
S. Sathish  and
T.E. Matikas
H. Rösner
Affiliation:
Fraunhofer Institute Nondestructive Testing, Universität 37, 66123 Saarbrücken, Germany
N. Meyendorf
Affiliation:
Fraunhofer Institute Nondestructive Testing, Universität 37, 66123 Saarbrücken, Germany
S. Sathish
Affiliation:
Center for Materials Diagnostics, University of Dayton, Dayton OH 45469-0121
T.E. Matikas
Affiliation:
Former Director of the Center for Materials Diagnostics, University of Dayton
Get access

Abstract

Dissipated heat has been measured by thermographic technique during fatigue experiments on Ti-6AI-4V. Surface temperature of the specimen was found sensitive to the amount of fatigue damage accumulated in the material. An increased heat dissipation due to fatigue can be related to continuous change in the microstructure (increased dislocation density, stacking faults etc.) of the material. A method based on passive thermography can be proposed to monitor damage accumulation in Ti-6Al-4V due to cyclic loading.

Type
Research Article
Information
MRS Online Proceedings Library (OPL) , Volume 591 , 1999 , 73
Copyright
Copyright © Materials Research Society 2000

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

[1]Finney, J.M., “Fatigue crack growth in metallic military aircraft structures” Handbook of Fatigue Crack Propagation in Metallic Structures. Vol. 2, Elsevier Science B.V. (1994) pp. 1539–1541.Google Scholar
[2]Frouin, J., Sathish, S., Matikas, T.E., Na, J.K., “Ultrasonic linear and nonlinear behavior of fatigued Ti6AI 4V” J. Mater. Res., Vol 14, No. 4 (1999) pp 1295–1298.Google Scholar
[3]Harig, H., Middeldorf, K., Müller, K., “Überblick uiber thermometrische Untersuchungen zum Ermüdungsverhalten von Stéihlen” HTM, 41 Nr. 5 (1986) pp. 286–296.Google Scholar
[4]Luong, M.P., “Nondestructive evaluation of fatigue limit of metals using infrared thermography” Mat. Res. Soc. Symp. Proc., Vol. 503 (1998) pp. 275–280.Google Scholar
[5]Tittmann, B.R., Linebarger, R.S., “Infrared sensing ultrasonically generated thermal waves for NDE applications” Ultrasonics Symposium, 762 (1984)Google Scholar
[6]Rösner, H., Meyendorf, N., Karpen, W., Matikas, T.E., “Nondestructive Evaluation of Fatigue on Titanium Alloys with Thermography” DARPA NDE-MURI, Third Annual Report, Sept. (1999) pp. 177–188.Google Scholar
[7]Thomson, W., “On the Thermo-Elastic and Thermomagnetic Properties of Matter” Quart. J. of Pure & Appl. Math., 1 (1857) pp. 57–77.Google Scholar
[8]Hutchings, M.T., Buttle, D.J., Lotbrook, R., Dalzell, W., Scruby, C.B., “Positron annihilation for the non-destructive assessment of the early stages of damage” J. De Physik IV, Colloque Cl, Suppl. An J. De Physique III, Vol. 5, Jan. (1995) C1–111.Google Scholar
[9]Morrissey, R.J., McDowell, D.L., Nicholas, T., “Frequency and stress ratio effects in high cycle fatigue of Ti 6A1-4V” International Journal of Fatigue, 21 (1999) pp. 679–685.Google Scholar
[10]Maurer, J.L., Frouin, J., Sathish, S., Matikas, T., Eylon, D., “Internal Damage Characterization of Cyclically Loaded Ti-6A1-4V, Using TEM and Non Linear Acoustics,” Proceedings of the 9th Titanium World Conference, St. Petersburg, Russia, June 1999, In Print.Google Scholar