Foreign object damage tolerance and fatigue analysis of induction hardened S38C axles
- 1. State Key Laboratory of Traction Power, Southwest Jiaotong University, Chengdu 610031 (China)
- 2. School of Mechanical and Electrical Engineering, University of Electronic Science and Technology of China, Chengdu 611731 (China)
- 3. School of Materials Science and Engineering, Southwest Jiaotong University, Chengdu 610031 (China)
- 4. Center for System Reliability & Safety, University of Electronic Science and Technology of China, Chengdu 611731 (China)
- 5. Advanced Research Institute, Chengdu University, Chengdu 610106 (China)
Description
Highlights: • Impact damages under different velocities and incident angles on S38C axle specimens are fabricated. • Morphologies of artificial impact damages are explored for S38C axle. • Influences of impact velocity and incident angle on fatigue strength of S38C axle specimens are studied. • Fatigue properties of specimens with artificial defects are analyzed based on K-T diagram. Flying ballast impact damage on railway axles poses a threat to structural integrity and safety of high-speed trains. A comprehensive evaluation on the fatigue strength debit of axles with foreign object damage (FOD) is vital for their safe operation and maintenance under damage tolerance philosophy. In this study, FODs were simulated by shooting tungsten steel balls to the specimens extracted from surface induction hardened S38C axles. Specifically, tests were performed under three impact velocities, i.e. 200, 300 and 400 m/s, and five incident angles for each impact velocity. Morphologies of impact damage were observed by scanning electron microscope (SEM) as well as the cross-sections. Fatigue strength of impacted specimens were then evaluated. Results show that depth and volume of damaged zone increases with the incident angle at the velocity of 200 m/s. Fatigue strength losses of specimens impacted at velocities of 300 and 400 m/s is around 50% compared with that of smooth ones. Fatigue crack originated from the exit rim for 200 m/s glanced impacted specimens, while multiple cracks propagated from both exit rim and bottom of crater impacted at 300 and 400 m/s. Finally, fatigue strength of damaged specimens was evaluated based on the defect depth concept and Kitagawa–Takahashi (K–T) diagram.
Availability note (English)
Available from http://dx.doi.org/10.1016/j.matdes.2021.109488Additional details
Identifiers
- DOI
- 10.1016/j.matdes.2021.109488;
- PII
- S0264127521000411;
Publishing Information
- Journal Title
- Materials and Design
- Journal Volume
- 202
- Journal Page Range
- vp.
- ISSN
- 0264-1275
- CODEN
- MADSD2
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 54033175
- Subject category
- S36: MATERIALS SCIENCE; S46: INSTRUMENTATION RELATED TO NUCLEAR SCIENCE AND TECHNOLOGY;
- Descriptors DEI
- BALLASTS; COMPUTERIZED SIMULATION; CROSS SECTIONS; FORMATION DAMAGE; MAINTENANCE; MORPHOLOGY; SCANNING ELECTRON MICROSCOPY; STEELS; SURFACES; TOLERANCE; TUNGSTEN
- Descriptors DEC
- ALLOYS; CARBON ADDITIONS; ELECTRON MICROSCOPY; ELEMENTS; IRON ALLOYS; IRON BASE ALLOYS; METALS; MICROSCOPY; REFRACTORY METALS; SIMULATION; TRANSITION ELEMENT ALLOYS; TRANSITION ELEMENTS
Optional Information
- Copyright
- Copyright (c) 2021 The Author(s). Published by Elsevier Ltd.