Problems of quantitative assessment of defectiveness in granulated nickel-base superalloys
UDC
669.018.44:669.245
DOI
10.18577/2307-6046-2026-0-4-21-34
Article PDF (Russian)
(893.74 KB)
How to cite
Gerasimov D.M., Krasnov I.S., M.A. Dalin Problems of quantitative assessment of defectiveness in granulated nickel-base superalloys // Proceedings of VIAM. 2026. No. 4. DOI: 10.18577/2307-6046-2026-0-4-21-34. URL: https://test.viam.ru/en/journal/2026/4/3
Keywords
defectiveness, gas turbine engine, non-destructive testing
Abstract
The article addresses the problem of assessing the expected content of non-metallic inclusions and other defects in materials used for manufacturing rotary components of turbines and compressors for aircraft gas turbine engines. The importance of objective information on defects not detected by non-destructive testing methods for the reliable determination of the safe service life of the engine is highlighted. Various methods for collecting and processing information on the quantity and size of defects in the material are reviewed, with their advantages and disadvantages listed. The choice of research directions aimed at developing a methodology for quantitative assessment of defects in granulated alloys is reasoned.
Reference list
- Kablov E.N. Main results and directions of development of materials for advanced aviation technology. 75 years. Aviation materials. Moscow: VIAM, 2007, pp. 20–26.
- Ryzhkov P.V., Gorbovets M.A., Hodinev I.A. Determination of the parameters of the plasticity model under cyclic loading of a heat-resistant nickel alloy at elevated temperatures. Aviation materials and technologies, 2025, no. 1 (78), pp. 72–87. Available at: http://www.journal.viam.ru (accessed: September 09, 2025). DOI: 10.18577/2713-0193-2025-0-1-72-87.
- National Transportation Safety Board. Aircraft accident report. 2018. Available at: https://www.ntsb.gob (accessed: January 09, 2025).
- Domas P.A., Roth P.G. Probabilistic Life Prediction Methods. Meeting the Challenges for Practical Application: Sixth international fatigue congress. Berlin, Germany, 1996, vol. II, p. 1251.
- Airworthiness Standards for Aircraft Engines: AP-33: approved by the Resolution of the 32nd Session of the Aviation and Airspace Utilization Council. 6th ed., with amendments 1–5. Moscow: Aviaizdat, 2025, pp. 7–11.
- RC-AP-33.70-2. Methodological Materials for the Implementation of Requirements for Main Engine Components, the Service Life of Which is Established in Cycles: Advisory Circular of the Interstate Aviation Committee (AR IAC). Moscow, 2023, p. 25.
- Class action amended consolidated class action complaint for violation of the federal securities laws. United States District Court District of Connecticut. Available at: https//www.saxenawhite.com (accessed: January 09, 2025).
- Investigation result of serious incident Vietnam Airlines Uncontained Engine Failure AIRBUS A321 MSN 5306 (VN-A392) Flight VN92: Final Report. Civil Aviation Authority of Vietnam, 2020, 36 p.
- Airworthiness Directives; International Aero Engines, AG Engines. Federal Register, 2024, vol. 89, no. 15, p. 49098.
- Gorbovets M.A., Khodinev I.A., Monin S.A. Influence of average cycle stress on characteristics of low-cycle fatigue of high-temperature nickel alloy VZh175. Aviation materials and technologies, 2023, no. 1 (70), pp. 126–136. Available at: http://www.journal.viam.ru (accessed: January 09, 2025). DOI: 10.18577/2713-0193-2023-0-1-126-136.
- McClung R.C., Enright M.P., Liang W. Integration of NASA-developed lifing technology for PM alloys into DARWIN: The NASA STI. San Antonio, Texas, 2011, 74 p.
- The integrity of nickel powder metallurgy rotating critical parts for gas turbines: Certification Memorandum. European Union Aviation Safety Agency, 2017, pp. 1–11.
- Kantzos P., Bonacuse P., Telesman J. et al. The Effect of Powder Cleanliness on the Fatigue Behavior of Powder Metallurgy Ni-Disk Alloy Udimet 720. Superalloys. Multidisciplinary Digital Publishing Institute, 2004, pp. 409–417.
- Cruz-Orive L.M. Particle Size-Shape Distributions: the General Spheroid Problem I: Mathematical Model. Journal of Microscopy, 1976, vol. 107, pp. 235–253.
- Bonacuse P., Kantzos P., Telesman J. Ceramic inclusions in powder metallurgy disk alloys: characterization and modeling: NASA/CR-2002-211682. Cleveland, Ohio, 2002, 38 p.
- Cruz-Orive L.M. Particle Size-Shape Distributions: the General Spheroid Problem II: Stochastic Model and Practical Guide. Journal of Microscopy, 1977, vol. 112, pp. 153–167.
- Erasov V.S., Oreshko E.I. Fatigue tests of metal materials (review). Part 1. Main definitions, loading parameters, representation of results of tests. Aviacionnye materialy i tehnologii, 2020, no. 4 (61), pp. 59–70. DOI: 10.18577/2071-9140-2020-4-59-70.
- Erasov V.S., Oreshko E.I. Tests for fatigue of metal materials (review). Part 2. Analysis of the Basquin–Manson–Coffin equation. Methods of testing and processing of results. Aviation materials and technology, 2021, no. 1 (62), pp. 80–94. Available at: http://www.journal.viam.ru (accessed: January 09, 2025). DOI: 10.18577/2713-0193-2021-0-1-80-94.
- Chertishchev V.Yu., Dalin M.A., Boychuk A.S., Krasnov I.S. Review of statistical methods for assessing the probability of detecting defects in non-destructive testing. V mire nerazrushayushchego kontrolya, 2021, vol. 24, no. 2 (92), pp. 4–14.
- Krasnov I.S., Lozhkova D.S., Dalin M.A. Evaluation of deficiency of titanium alloy forgings for probabilistic calculation of gas turbine engine disks fracture risk. Aviation materials and technologies, 2021, no. 2 (63), pp. 115–122. Available at: https://www.journal.viam.ru (accessed: January 09, 2025). DOI: 10.18577/2713-0193-2021-0-2-115-122.
- Trunkin I.N., Artamonov M.A., Ovcharov A.V., Vasiliev A.L. Study of hafnium-containing defects in granulated nickel alloy EP741NP used for the manufacture of aircraft engines. Vestnik Samarskogo universiteta. Aerokosmicheskaya tekhnika, tekhnologii i mashinostroyenie, 2019, vol. 18, no. 2, p. 89.
- Kastner J., Plank B., Salaberger D., Sekelja J. Defect and Porosity Determination of Fibre Reinforced Polymers by X-ray Computed Tomography. 2nd International Symposium on NDT in Aerospace: Proceedings. Wels, Austria, 2010, p. 5.
