journal article·2023-11

Failure analysis of a first stage turbine blade made of directionally solidified GTD111 superalloy and repaired by welding process

Zhang Zhixin, Zeng Wu, Bian Xiangde, Zhang Xiaodong

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OpenAlex topics: High Temperature Alloys and Creep · High-Temperature Coating Behaviors

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References (50)

Show source-provided references
1. Failure analysis of gas turbine rotor blades[J]10.1016/j.engfailanal.2014.06.003 ↗
2. Failure analysis of gas turbine first stage blade made of nickel-based superalloy[J]10.1016/j.csefa.2017.04.002 ↗
3. Failure of first stage gas turbine blades[J]10.1016/j.engfailanal.2003.08.010 ↗
4. Failure investigations of a first stage Ni based super alloy gas turbine blade[J]
5. Failure analysis of the 1st stage blades in gas turbine engine[J]10.1016/j.engfailanal.2013.03.017 ↗
6. Advanced Materials for Land Based Gas Turbines[J]10.1007/s12666-014-0398-3 ↗
7. Gas turbine materials selection, life management and performance improvement[J]10.1533/9780857093806.3.330 ↗
8. Insight into the sensitivities of freckles in the directional solidification of single-crystal turbine blades[J]10.1016/j.jmapro.2022.03.019 ↗
9. The subgrain structure in turbine blade roots of CMSX-4 sup-eralloy[J]10.1016/j.jcrysgro.2013.11.092 ↗
10. Direct investigation on high temperature tensile and creep behavior at different regions of directional solidified cast turbine blades[J]10.1016/j.mechmat.2019.103068 ↗
11. Some New Observations on Freckle Formation in Directionally Solidified Superalloy Components[J]10.1007/s11663-011-9608-0 ↗
12. Power industry experiences surge in welding research[J]
13. Failure mechanism of turbine guide vane and oxide composition analysis on the surface of failure vane cracks[J]10.1016/j.engfailanal.2020.104763 ↗
14. Abnormal creep property degradation in a directionally solidified superalloy DZ406 after suffering overheating[J]10.1016/j.matchar.2021.110910 ↗
15. On the fabrication of metallic single crystal turbine blades with a commentary on repair via additive manufacturing[J]
16. Evaluation of Platform Weld Repairs on F-Class, Stage 1 Buckets[C]//Turbo Expo: Power for Land, Sea, and Air
17. Repair process technology development and experience of frame 7FA+ E, Stage 1 Turbine Buckets[C]
18. A high temperature deformation mechanism map for the high performance Ni-base superalloy GTD-111[J]10.1016/S0921-5093(00)01822-0 ↗
19. On the precipitation hardening of the directionally solidified GTD-111 Ni-base superalloy: Microstructures and mechanical properties[J]10.1016/j.msea.2017.01.005 ↗
20. Microstructural and mechanical investigations on the heat treatment rejuvenation of a long-term service-exposed GTD-111 Ni-based superalloy[J]10.1016/j.msea.2022.144381 ↗
21. Microstructural evolution of NiCoCrAlY coated directionally solidified superalloy[J]10.1016/j.surfcoat.2022.128487 ↗
22. Additive Manufacturing of Nickel-Base Superalloy René N5 through Scanning Laser Epitaxy (SLE) − Material Processing, Microstructures, and Microhardness Properties[J]10.1002/adem.201600690 ↗
23. Determination of Ideal Conditions for GTD-111 Superalloy Welding Through Pre-Heating, Pre-Cold and Heat Treatment[J]10.1007/s12540-020-00779-6 ↗
24. Effect of Nd:YAG pulsed laser welding process on the liquation and strainage cracking in GTD-111 superalloy[J]10.1016/j.jmapro.2020.01.049 ↗
25. Hot Cracking of GTD-111 Nickel-Based Superalloy Welded by Pulsed Nd:YAG Laser[J]10.1007/s13632-019-00602-8 ↗
26. Mechanism of post-weld heat treatment cracking in Rene 80 nickel based superalloy[J]10.1179/026708302225001633 ↗
27. Influence of a plasma-sprayed NiCrAlY coating on the low-cycle fatigue be-haviour of a directionally solidified nickel-base superalloy[J]10.1016/S0921-5093(98)00505-X ↗
28. Influence of protective coatings on damage mechanisms and lifetime of Alloy 247 DS in thermo-mechanical fatigue tests[J]10.3184/096034013X13629345646988 ↗
29. Effect of MCrAlY coating on the low-cycle fatigue behavior of a directionally solidified nickel-base superalloy at different temperatures[J]10.1016/j.ijfatigue.2015.02.018 ↗
30. Effect of interface diffusion on low-cycle fatigue behaviors of MCrAlY coated single crystal superalloys[J]10.1016/j.ijfatigue.2020.105660 ↗
31. Evaluation, degradation and life assessment of coatings for land based combustion turbines[J]10.1179/174892306X99705 ↗
32. Thermomechanical fatigue experiment and failure analysis on a nickel-based superalloy turbine blade[J]10.1016/j.engfailanal.2019.04.023 ↗
33. A study of low cycle fatigue life and its correlation with micro-structural parameters in IN713C nickel based superalloy[J]10.1016/j.msea.2018.01.083 ↗
34. Tensile Deformation Behavior of a Directionally Solidified Superalloy at Cryogenic Temperatures[J]10.3390/cryst12070886 ↗
35. Corrosion kinetics of a directionally solidified Ni-base superalloy[J]10.1016/j.actamat.2007.01.034 ↗
36. Oxidation behavior of GTD111 Ni-based superalloy at 900°C in air[J]10.1016/j.corsci.2015.07.031 ↗
37. Low cycle fatigue of René 80 as affected by prior exposure[J]10.1007/BF02811730 ↗
38. GTD111 Alloy Material Study[J]10.1115/1.2818133 ↗
39. Control of γ′ particle size and volume fraction in the high temperature superalloy Udimet 700[J]10.1007/BF02913886 ↗
40. The Effect of Long-Term Thermal Exposure on the Microstructure and Stress Rupture Property of a Directionally Solidified Ni-Based Superalloy[J]10.1007/s11661-014-2559-8 ↗
41. Trexler M D. The relationship of microstructure to fracture and corrosion behavior of a directionally solidified superalloy[D]. ProQuest Dissertations and Theses, United States, Georgia: Georgia Institute of Technology.
42. Effect of primary and secondary precipitates on creep strength of Ni-base superalloy single crystals[J]10.1016/S0921-5093(99)00579-1 ↗
43. Microstructures and mechanical properties of DZ125 directional solidified superalloy repaired by HIP technology[J]
44. The hardness evolution of cast and the high-cycle fatigue life change of wrought Ni-base superalloys after additional heat treatment[J]10.3390/ma14237427 ↗
45. General relationship between strength and hardness[J]10.1016/j.msea.2011.08.061 ↗
46. Thermal barrier coating experience in gas turbine engines at Pratt & Whitney[J]10.1007/BF02646318 ↗
47. Interdiffusion in MCrAlY coated nickel-base superalloys[J]10.1016/j.surfcoat.2016.09.049 ↗
48. CM88Y superalloy blade metallurgical degradation in a gas turbine[J]10.1016/j.engfailanal.2023.107110 ↗
49. The mechanical properties of coatings and coated systems[J]10.1016/0921-5093(89)90826-5 ↗
50. Thermo-mechanical fatigue failure of thermal barrier coated superalloy specimen[J]10.1007/s11661-015-2996-z ↗