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This study investigates the rolling contact fatigue performance of WC-NiCrBSi thermal spray coatings subjected to Hot Isostatic Pressing (HIPing) treatment. The effects of HIPing on microstructure, hardness, and bonding between splats are analyzed. The results show significant improvement in rolling contact fatigue performance after HIPing at elevated temperatures.
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Rolling Contact Fatigue of Hot Isostatic Pressed WC-NiCrBSi Thermal Spray Coatings S. Stewart Supervisor : Dr R. Ahmed
Introduction Thermal Spray Coatings are used in a number of industrial applications ranging from the automotive and aerospace industries to biomedical applications. However, in many types of industrial machinery such as gears, camshafts and rolling element bearings, surface damage generated by rolling / sliding contact limits the life of the component and hence reduces durability and product reliability. This drives the development and implementation of state of the art surface coatings which enable improved life reliability and load bearing capacity in more hostile environments. www.sulzermetco.com
AIMS AND OBJECTIVES PRESSURE VESSEL FURNACE WORK-PIECE HIP Unit Subjecting Thermal Sprayed coatings to the post treatment, Hot Isostatic Pressing (HIPing), leads to significant densification within the microstructure. The combination of high temperatures and equi-axial pressure reduces porosity and leads to the formation of a more lamellar microstructure. This preliminary study marks the first investigation in published literature in which the rolling contact fatigue performance of HIPed functional graded WC-NiCrBSi coatings are studied.
Coating fabrication process WC + Ni-7.56%Cr-3.69%Si-2.57%Fe-1.55%B-0.25% (sintered and agglomerated) WC-40%NiCrBSi (100m) HVOF Process Parameters Gun type : JP5000 Spray distance : 380 mm Barrel length : 4” Fuel gas : Kerosene Powder Carrier gas : Oxygen 440-C Bearing Steel WC-10%NiCrBSi (300m)
10 (µm) 10 (µm) 100 (µm) 100 (µm) 100 (µm) Analysis of coating microstructure Reduction in porosity and change in carbide shape indicates significant densification has occurred within the microstructure of the coating HIPed at 1200ºC. WC-40%NiCrBSi WC-10%NiCrBSi substrate As -sprayed HIP 850ºC HIP 1200ºC
Micro-hardness measurements show increased hardness values at elevated temperatures of HIPing verifying the observation of densification with the coating microstructure. Vickers Hardness (HV) WC-40%NiCrBSi WC-10%NiCrBSi Elastic Modulus results show increased values with HIPing . This indicates improved bonding between the splats after HIPing which can improve resistance of the coating to rolling contact fatigue. Elastic Modulus (GPa) ºC ºC Distance from Surface (µm)
Rolling Contact Fatigue Rig Drive shaft connected via belt to motor rotates coated disc at 4000 rpm M ωA ωs R2 RA θ A B Rp ωp D δ C β O Rc Air pressure from bellows generates required contact load between balls and disc. A modified four ball machine was used to study the rolling contact fatigue performance of the HIPed thermal spray coatings. A ceramic ball was placed below the three planetary balls to obtain the correct rolling / sliding contact kinematics.
As-Sprayed HIPed at 850ºC HIPed at 1200ºC RCF test results Significant improvement in RCF performance over as-sprayed coating Stress cycles to failure (millions) Contact stress (GPa) • A high viscosity lubricant was used to prevent asperity contact between the coating surface and the planetary balls during testing and hence maintain full film elasto-hydrodynamic lubrication. • Tests were performed using either 440-C Bearing Steel or HIPed Silicon Nitride Ceramic planetary balls.
Post test Analysis 1000 (µm) 200 (µm) as-sprayed 56µm HIP 1200ºC Under identical experimental conditions, no failure was observed on the wear track of the coating HIPed at 1200ºC after 70 million stress cycles. However, a micro-pit 56µm in depth occurred on the wear track of the as -sprayed coating after only 10 million stress cycles.
Mechanism of failure substrate coating Micro-crack initiates from pore and propagates. Depth of maximum shear stress a Planetary ball Crack leads to formation of micro-pit at surface. contact width Depth of orthogonal shearstress Micro-pit forms on wear track from sub-surface defects Debris from micro-pit forms larger failure areas on wear track Wear track forms from cyclic stresses
Conclusions • HIPing at elevated temperatures of 1200 ºC lead to significant improvement in rcf performance at low levels of contact stress. No failure occurred at 2GPa, and improvement was attributed to increased densification within the upper layer of the coating. • The post treatment HIPing was shown to increase elastic modulus and micro-hardness. At elevated temperatures of HIPing, densification occurred which was verified by an increase in micro-hardness within the upper layer of the coating. • Mechanism of failure in as-sprayed coatings was identified as delamination which initiated from sub surface defects. Acknowledgments • Dr Susan Davies at Bodycote HIP ltd / Infutec ltd • Dr T. Itsukaichi at Fujimi Inc. • Prof. S.Tobe at Agishaka Institute of Technology