Studies on Elevated Temperature Tribological Behavior of Fly Ash Based Plasma Spray Coatings
Date
2018
Authors
Mathapati, Mahantayya
Journal Title
Journal ISSN
Volume Title
Publisher
National Institute of Technology Karnataka, Surathkal
Abstract
Material behavior at elevated temperature is becoming an increasing technological
importance. Components working at higher temperatures like in land based gas and
steam turbines, power generation boiler tubes, hot sections of aero engine, propulsion
bearings, materials processing and internal combustion engines are subjected to
surface friction, wear, oxidation and hot corrosion conditions. Service conditions of
such components in elevated temperature environments may compromise their
mechanical properties resulting in the reduced life cycle. Components working in
such adverse conditions demand suitable surface modification techniques like thermal
spray coatings that are widely adopted in similar situations.
Plasma spray coating processes belong to the family of thermal spraying techniques
and are widely used in many industries to protect the components against erosion,
oxidation and wear. Thermal energy is utilized in this process to deposit a wide
variety of materials including finely divided metallic and non-metallic materials.
Higher temperatures utilized in these processes enable the use of coating materials
with very high melting points like ceramics, cermets, and refractory alloys. The
present work explores the possibility of using fly ash based plasma spray coatings for
high temperature applications. The proposed coatings are investigated for their
resistance to erosion, oxidation and wear under laboratory conditions.
Commercially available Cr3C2-25NiCr, NiCrAlY, WC-Co, fly ash cenospheres,
MoS2, CaF2 and CaSO4 are used as coating feedstock in the present investigation. Six
types of coatings namely Cr3C2-NiCr/Cenosphere, NiCrAlY/WC-Co/Cenosphere,
Cr3C2-NiCr/Cenosphere/MoS2/CaF2, Cr3C2-NiCr/Cenosphere/MoS2/CaSO4,
NiCrAlY/WC-Co /Cenosphere/MoS2/CaF2 and NiCrAlY/WC-Co
/Cenosphere/MoS2/CaSO4 are deposited on MDN 321 steel substrate (Midhani
Grade). Coatings are characterized using Scanning Electron Microscope (SEM),
Energy Dispersive Spectroscopy (EDS) and X-ray diffraction (XRD). Further,
microstructure and mechanical properties (microhardness, adhesion strength, erosion,
oxidation, and wear) have been characterized to evaluate their potential for hightemperature application. For the chosen spray parameters, seemingly dense laminar
structured coatings (six types as mentioned earlier) with a thickness in the range of
350-400 m having porosity lower than 5 % has been achieved.
Erosion behavior of MDN 321 steel, Cr3C2-NiCr/Cenosphere, and NiCrAlY/WCCo/Cenosphere coatings are investigated at elevated temperatures using solid particle
erosion test (ASTM G76-13) set up at 200, 400, 600 °C with 30 and 90° impact
angles using alumina erodent. Erosion resistance of both the coatings is observed to
be higher than the substrate for the test temperatures chosen and noted to be more
prominent at lower impact angle and higher temperature. Both the coatings
exhibited a brittle mode of material removal through brittle cracking and
chipping. NiCrAlY/WC-Co/Cenosphere coating reported better erosion resistance as
compared to Cr3C2-NiCr/Cenosphere coating which may be attributed to plastic
deformation of the NiCrAlY matrix due to the ductility of the matrix and hard WC-Co
reinforcement to resist the matrix plow thereby reduces the erosion loss.
Cyclic oxidation behavior of MDN 321 steel, Cr3C2-NiCr/Cenosphere and
NiCrAlY/WC-Co/Cenosphere coatings are further carried out at 600 °C for 20 cycles.
Each cycle consisted of heating at 600 °C for 1 hour, followed by 20 minutes of
cooling in air. The thermogravimetric technique is used to approximate the kinetics of
oxidation of substrate and coatings. Both the coatings reported lower weight gain as
compared to the substrate. NiCrAlY/WC-Co/Cenosphere coating registered less
weight gain as compared to Cr3C2-NiCr/Cenosphere coating which is attributed to the
excellent oxidation resistance of NiCrAlY and formation of CoWO4 along with NiO
and Cr2O3 oxides on the coating surface.
Influence of solid lubricants on Cr3C2-NiCr/Cenosphere and NiCrAlY/WCCo/Cenosphere coatings is dealt next for tribological response. Dry sliding wear
behavior of MDN 321 steel, Cr3C2-NiCr/Cenosphere/MoS2/CaF2, Cr3C2-
NiCr/Cenosphere/MoS2/CaSO4, NiCrAlY/WC-Co/Cenosphere/MoS2/CaF2 and
NiCrAlY/WC-Co/Cenosphere/MoS2/CaSO4 is carried out using high temperature pin
on disc tribometer as outlined in ASTM G99-05 standard. All the four coatingsdisplayed a lower coefficient of friction and wear rate in comparison with the
substrate. Excellent wear resistance of the coatings is attributed to the solid lubricants
effect. Based on the wear rate data, the relative wear resistance of the coatings under
dry sliding conditions is arranged in the following sequence:
(Cr3C2-NiCr/Cenosphere/MoS2/CaSO4) > (Cr3C2-NiCr/Cenosphere/MoS2/CaF2) >
(NiCrAlY/WC-Co/Cenosphere/MoS2/CaSO4) > (NiCrAlY/WC-Co/Cenosphere/MoS2/CaF2)
Higher wear resistance of Cr3C2-NiCr/Cenosphere/solid lubricant coatings is
attributed to the high hardness of Cr3C2-NiCr which is incorporated in the coatings.
Developed coatings in the present study exhibit higher temperature resistance to
erosion, oxidation and wear as compared to MDN321 steel making them suitable for
components subjected to elevated temperature service conditions.
Description
Keywords
Department of Mechanical Engineering, Plasma spray, Fly ash cenosphere, Solid lubricants, Erosion, Oxidation, Wear, Elevated temperature