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The IUP Journal of Mechanical Engineering
Erosion Wear Behavior Analysis of HVOF Sprayed Al-Si-Polyester Abradable Coating at High Temperature
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In the present study, erosion wear behavior of Al-Si-Polyester abradable coating at high temperature is evaluated. High Velocity Oxygen Fuel (HVOF) technique was used to spray the Al-Si-Polyester powder on the Titanium-based superalloy (Titan-15). A self-made air jet erosion testing machine was used to investigate the erosion rate of abradable coating. Erosion wear behavior of the coating was investigated at two substrate temperatures (i.e., at 350 °C and 450 °C), which shows that maximum erosion wear takes place at 450 °C substrate temperature, and as the temperature difference between substrate and air temperature increases, the erosion rate also increases. Erosion resistance of abradable coating also depends upon the hardness of the coating. As the coating becomes harder the erosion resistance becomes more. Polyester plays a very important role and increases the erosion resistance.

 
 

Surface improvement is of more concern in today’s industrial environment. The enhanced demand for higher efficiency and more productivity increases the need for more reliable and high performance components. In most of the cases, the rapid wear and eventual failure of the components subjected to damage of material are due to the environmental conditions and also high relative motion between the mating surfaces which causes cyclic stresses and high temperatures.

To avoid these types of results, a protective coating layer has been introduced to the surface of the component which acts as a barrier between the component and the aggressive environment. This method is very advantageous and is being accepted universally by the manufacturing and engineering industries. Coatings historically provide a protection against erosion and corrosion of parts, and protect the material from chemical and physical interaction with its inside and outside environment (Fauchais and Vardelle, 2012). Solid particle erosion is a dynamic process that leads to progressive loss of material from the target surface due to impingement of fast moving solid particles (Demasi, 1994). During flight, a particle carries momentum and kinetic energy, which is dissipated during impact at target surface (Oka, 1990). The function of abradable coatings is to not only allow sharp clearances but also automatically adjust clearances, i.e., to accept physical harm and thermal changes that may be found in devices. In aircraft jet engines, abradable coatings are used in the compressor and turbine sections where a minimum clearance is required between the blade tips and the casing.

 
 

Mechanical Engineering Journal, High temperature erosion, Air jet erosion testing machine, Titanium, Al-Si- Polyester coating, Taguchi.