Wear studies of copper-fly ash composite under dry sliding conditions
- 1. Faculty of Mechanical Engineering, Kalasalingam Academy of Research and Education, Krishnankoil (India)
- 2. Institute of Production Engineering, Cracow University of Technology, Cracow (Poland)
Description
Copper matrix composites with hard reinforcement offer higher strength and exhibit better wear resistance than copper with no reinforcement addition. The present study investigates about the influence of load, sliding velocity and % of reinforcement on the copper matrix. Composites were prepared with fly ash as reinforcement range from 2.5–10 wt% through the powder metallurgy technique. During the fabrication, the specimens are processed with the compaction pressure of 450 MPa, sintering temperature of 900 °C and sintering time of 90 min. The prepared specimens were tested for the dry sliding wear behaviour under the load range of 10–50 N with the steps of 10 N for the sliding velocities 1, 2 and 3 m s−1 over a distance of 2000 m. The results show that with the increase in percentage reinforcement, wear resistance increases for all the sliding velocities till 30 N load. The change in wear behaviour in higher load and sliding velocity is discussed in detail with the metallurgical examination. (paper)
Availability note (English)
Available from http://dx.doi.org/10.1088/2053-1591/ab3ffeAdditional details
Identifiers
Publishing Information
- Journal Title
- Materials Research Express (Online)
- Journal Volume
- 6
- Journal Issue
- 10
- Journal Page Range
- [11 p.]
- ISSN
- 2053-1591
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 52008565
- Subject category
- S42: ENGINEERING; S36: MATERIALS SCIENCE;
- Descriptors DEI
- COPPER; FLY ASH; MATRICES; POWDER METALLURGY; SINTERING; WEAR RESISTANCE
- Descriptors DEC
- AEROSOL WASTES; ASHES; COMBUSTION PRODUCTS; ELEMENTS; FABRICATION; MECHANICAL PROPERTIES; METALLURGY; METALS; RESIDUES; TRANSITION ELEMENTS; WASTES