An Artificial Inclusion Seeding Methodology for Fatigue Design of Aerospace Ti Castings

인공개재물 이식법을 통한 항공기용 티타늄 주물의 피로설계

  • Paul, L. Ret (Air Force Research Lab, Wright-Patterson Air Force Base) ;
  • Park, Yong-Kuk (Catholic University of Daegu) ;
  • Kim, Jin-Gon (Air Force Research Lab, Wright-Patterson Air Force Base)
  • Published : 2006.08.20

Abstract

Presence of inclusions in Ti castings imparts detrimental effects on the mechanical performance of castings. However, actual inclusions do not occur very frequently and they are difficult to locate. As a result, acquirement of specimens for mechanical tests and thus in-depth research of the adverse influence of inclusions are challenging. To address this problem, artificial inclusion seeding methodology is developed to emulate actual inclusions in Ti investment castings. Firstly, to validate that this new methodology does not result in inherent mechanical property degradation, Ti specimens with machined, backfilled and HIPed holes are produced and compared to control (unaltered), cast Ti material. Fatigue test results indicate that this 'machine-and-HIP methodology without seeding' does not result in any fundamental mechanical property alteration, which would bias ensuing comparative results. Secondly, based on this result, validation of the artificially seeded inclusions being equivalent to 'as cast' inclusions is performed by comparing their fatigue behaviors. Test specimens created by the novel artificial inclusion seeding methodology are equivalent to Ti casting specimens containing actual cast-in inclusions, and an adverse effect of inclusions in investment castings is confirmed.

Keywords

References

  1. Z.W. Li, et. al.: Scripta mater. 48 (2003) 1649 https://doi.org/10.1016/S1359-6462(03)00133-7
  2. L.L. Soffa: Metals Engineering Quarterly, 8 (1968) 28-32
  3. W.J. Barice: Journal of Aircraft, 'Large Structural Titanium Castings,' 19 (1982) 687-691 https://doi.org/10.2514/3.57450
  4. R.R. Boyer, W.F. Spurr, and J.M. Edwards: 17th National SAMPE Technical Conference, 'Current and Potential Usage of Titanium Castings for Airframe Applications,' (1985) 624-634
  5. C. Shamblen and G. Hunter: 'Titanium based alloys clean melt process development,' Proceedings of the 1989 Vacuum Metallurgy Conference on the Melting and Processing of Specialty Materials, Pittsburgh, PA, (1989) 6
  6. M. Gigliotti, R. Gilmore and L. Percocchi, 'Microstructure and Sound Velocity of Ti-N-O Synthetic Inclusions in Ti-6AI4V', Metallurgical and Materials Transactions A, Vol. 25A, (1994) 2321
  7. Military Handbook: 'General Guidelines for Aircraft Structural Integrity Program(ASIP), MIL-HDBK-1530A,' (2002)
  8. National Transportation Safety Board (NTSB): 'Accident Report No: PB90-910406 NTSB/AAR 90-06,' (1990). 71
  9. J.D. Cotton, L.P. Clark and T.R. Reinhart: American Institute of Aeronautics and Astronautics 'Inclusions in Ti-6AI-4V Investment Castings,' AIAA-2000-1464 (2000) 5-8
  10. Y.Park, P. Ret and J. Kim: Journal of the Korean Foundrymen's Society, 'A study on the effect of inclusions on the fatigue life of titanium investment castings,' 26 (2006) 16-24
  11. Society of Automotive Engineers: 'Aerospace Materials Specification 4962,' (1998) 4
  12. Military Handbook: 'General Guidelines for Aircraft Structural Integrity Program,' MIL-HDBK-1530A (2002) 24
  13. Air Force Research Lab., WPAFB: 'Materials and Manufacturing Directorate, Mechanical Data,' (2001)
  14. D. C. Montgomery, G. C. Runger, and N. F. Hubele: 'Engineering Statistics', 3rd ed., Wiley, (2004) 211