journal article·2016-11

Influence of the WEDM process on the fatigue behavior of Inconel® 718

Izaro Ayesta, Borja Izquierdo, Olatz Flaño, Jose Antonio Sánchez, Joseba Albizuri, Rafael Avilés

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Abstract

Abstract The use of alternative processes for the manufacturing of aeronautical components is essential in order to fulfill the requirements that have been set by the aircraft sector. One particular solution that has been used for certain applications is that of Electrical Discharge Machining (EDM). The EDM process can machine any electrically conductive material, irrespective of its hardness or mechanical properties, and is thus a useful solution for difficult-to-machine aerospace alloys. However, due to its thermal nature, the EDM process induces metallurgical changes in the machined material, which in turn may reduce its fatigue service life. For this reason, the aerospace industry has restricted the use of EDM to the manufacturing of selected components. Nevertheless, there have recently been significant advances in the development of EDM generators that minimize thermal input toward the machined component. As a consequence, it is critical to know the extent to which these new EDM processes affect fatigue service life in aerospace alloys, in order to adequately evaluate the feasibility of using this process. Given the limited information in the literature regarding this topic, the present paper describes a study of the fatigue life of WEDM produced nickel-based Inconel® 718. In order to examine the capabilities of WEDM, fatigue specimens were manufactured using both this procedure and the grinding process (used as a reference for comparison). Surface analysis, metallographic studies, residual stresses, fractography and axial fatigue tests are described and discussed. The results showed that conducting the WEDM process with the new generation of machines has a detrimental effect at high fatigue cycles, reducing fatigue strength by approximately 10% in comparison with ground specimens. However, at low fatigue cycles, no significant differences were observed between ground and WEDM samples. These findings have implications for the potential use of the WEDM process in the manufacturing of disk turbine fir-trees.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Advanced Machining and Optimization Techniques · Metal Alloys Wear and Properties · Welding Techniques and Residual Stresses

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (48)

Show source-provided references
1. Boeing. Traffic and market outlook Boeing: traffic and market outlook 2014: p. 1–56.
2. ACARE Aviation in Europe: a vision for 2050; 2000.
3. High performance cutting of aerospace materials10.4028/www.scientific.net/AMR.498.127 ↗
4. EDMing turbopump blisks10.1108/00022660210414994 ↗
5. Optimum electrode path generation for EDM manufacturing of aerospace components10.1016/j.rcim.2015.04.003 ↗
6. Investigations on vibration-assisted EDM-machining of seal slots in high-temperature resistant materials for turbine components10.1016/j.procir.2013.03.019 ↗
7. Influence of EDM parameters on slot machining in C1023 aeronautical alloy10.1016/j.procir.2013.03.059 ↗
8. Turbomachinery component manufacture by application of electrochemical, electro-physical and photonic processes10.1016/j.cirp.2014.05.004 ↗
9. Quality assessment through in-process monitoring of wire-EDM for fir tree slot production10.1016/j.procir.2014.07.136 ↗
10. Evaluation of advanced wire-EDM capabilities for the manufacture of fir tree slots in Inconel 71810.1016/j.procir.2014.03.039 ↗
11. Modelling of process forces in broaching Inconel 71810.1016/j.procir.2013.06.125 ↗
12. Abrasive machining of advanced aerospace alloys and composites10.1016/j.cirp.2015.05.004 ↗
13. Ibrahim El-Wardany T, Smith PG, Reynolds W, Ng E, Adams KV. Abrasive waterjet machining and method to manufacture a curved rotor blade retention slot. United States Pat US008439724B2; 2013.
14. Profiled superabrasive grinding wheels for the machining of a nickel based superalloy10.1016/j.cirp.2007.05.077 ↗
15. Numerical prediction of heat affected layer in the EDM of aeronautical alloys10.1016/j.apsusc.2012.07.124 ↗
16. Microstructure at submicron scale of the white layer produced by EDM technique10.1016/j.jmatprotec.2003.11.047 ↗
17. Effect of electrical discharge machining on surface characteristics and machining damage of AISI D2 tool steel10.1016/S0921-5093(03)00272-7 ↗
18. Relationship between EDM parameters and surface crack formation10.1016/S0924-0136(03)00688-5 ↗
19. Residual stresses and white layer in electric discharge machining (EDM)10.1016/j.apsusc.2007.05.078 ↗
20. On the effect of electrodischarge machining parameters on the fatigue life of AISI D6 tool steel10.1016/S0924-0136(96)02523-X ↗
21. Influence of laser polishing on the high cycle fatigue strength of medium carbon AISI 1045 steel10.1016/j.ijfatigue.2011.06.004 ↗
22. Surface integrity characteristics in wire-EDM of Inconel 718 at different discharge energy10.1016/j.procir.2013.03.046 ↗
23. Evaluation of WEDM performance characteristics of Inconel 706 for turbine disk application10.1016/j.matdes.2015.09.036 ↗
24. Fatigue damage in aircraft structures, not wanted, but tolerated?10.1016/j.ijfatigue.2008.05.016 ↗
25. High cycle fatigue in aircraft gas turbines – an industry perspective10.1007/BF00012667 ↗
26. The effect of machining on the surface integrity and fatigue life10.1016/j.ijfatigue.2008.01.005 ↗
27. Influence of pulse sequence and edge material effect on fatigue life of Al2024-T351 specimens treated by laser shock processing10.1016/j.ijfatigue.2014.09.015 ↗
28. Through thickness property variations in friction stir welded AA6061 joint fatigued in very high cycle fatigue regime10.1016/j.ijfatigue.2015.08.013 ↗
29. Effect of electric discharge machining on the fatigue life of Inconel 71810.1016/0142-1123(88)90040-0 ↗
30. Improving the fatigue life of electro-discharge-machined SDK11 tool steel via the suppression of surface cracks10.1016/j.ijfatigue.2008.07.013 ↗
31. Role of electro-discharge machining on the fatigue performance of 15-5PH stainless steel component10.1016/j.engfailanal.2010.02.005 ↗
32. Effects of finishing processes on the fatigue life improvements of electro-machined surfaces of tool steel10.1007/s00170-010-2751-y ↗
33. Improvement of fatigue life of electrical discharge machined AISI D2 tool steel by TiN coating10.1016/S0921-5093(01)01268-0 ↗
34. Fracture and fatigue behavior of electrical-discharge machined cemented carbides10.1016/j.ijrmhm.2005.04.007 ↗
35. Workpiece surface roughness and integrity after WEDM of Ti–6Al–4V and Inconel 718 using minimum damage generator technology10.1016/j.cirp.2008.03.054 ↗
36. WEDM of aerospace alloys using “Clean Cut”generator technology
37. Comparison of grinding and wire EDM concerning fatigue strength and surface integrity of machined Ti6Al4V components10.1016/j.proeng.2011.11.099 ↗
38. Degradation of titanium 6Al–4V fatigue strength due to electrical discharge machining10.1016/j.ijfatigue.2014.02.018 ↗
39. The effect of wire electrical discharge machining on the fatigue life of Ti-6Al-2Sn-4Zr-6Mo aerospace alloy10.1016/j.procir.2013.03.043 ↗
40. Fatigue response of Udimet 720 following minimum damage wire electrical discharge machining10.1016/j.matdes.2012.06.003 ↗
41. Results of surface integrity and fatigue study of wire-EDM compared to broaching and grinding for demanding jet engine components made of Inconel 71810.1016/j.procir.2014.04.057 ↗
42. The exponential law of endurance tests
43. Universality behind Basquin’s law of Fatigue10.1103/PhysRevLett.100.094301 ↗
44. Marin · 1962
45. Mean stress effect correction using constant stress ratio S-N curves10.1016/j.ijfatigue.2013.02.019 ↗
46. High-cycle fatigue of Ni-base superalloy Inconel 713LC10.1016/j.ijfatigue.2009.02.042 ↗
47. Influence of low-plasticity ball burnishing on the high cycle fatigue strength of medium carbon AISI 1045 steel10.1016/j.ijfatigue.2013.06.024 ↗
48. Influence of laser polishing in an inert atmosphere on the high cycle fatigue strength of AISI 1045 steel10.1016/j.ijfatigue.2014.06.004 ↗