4.4 Article

Numerical Investigation on the Flame Characteristics and Particle Behaviors in a HVOF Spray Process Using Kerosene as Fuel

Journal

JOURNAL OF THERMAL SPRAY TECHNOLOGY
Volume 30, Issue 3, Pages 725-738

Publisher

SPRINGER
DOI: 10.1007/s11666-021-01165-3

Keywords

flame flow characteristics; HVOF; k-epsilon turbulence model; particle dynamics; WC-12Co

Funding

  1. National Natural Science Foundation of China [E050402/51105187]
  2. Project of Education Department in Liaoning Province [2017FWDF01]
  3. Opentopics of firefighting key laboratories of the ministry of public security [KF201704]
  4. Innovation Team Building Project of University of Science and Technology Liaoning [601009830-02]
  5. Natural Science Foundation Guidance Project in Liaoning Province
  6. key R&D plan science and technology support Project in Tianjin City [S20ZC771198]

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HVOF coatings with high bonding strength and good compactness improve substrate wear, corrosion, high-temperature oxidation, and fatigue properties. The flame flow characteristics and particle behaviors during the spray process have a significant impact on coating microstructure and properties. Study focused on a flow field model using kerosene as fuel, analyzing flame dynamics and particle characteristics.
HVOF coatings generally have a high bonding strength and good compactness, which improve the wear, corrosion, high-temperature oxidation, and fatigue properties of the substrate. They are widely used in automobile, home appliance, petrochemical, aerospace, and other fields. The flame flow characteristics and particle in-flight behaviors during the spray process have an essential influence on the coating microstructure and, thus, properties. This paper deals with a flow field model of a HVOF process that uses kerosene as fuel. A one-step chemical reaction model and the eddy dissipation model were used to numerically calculate the flame dynamics. The numerical simulations predicted the variation laws of flame pressure, temperature, velocity, Mach number, and combustion components. On this basis, the temperature, velocity, and trajectory of WC-12Co particles were calculated using a Lagrangian approach. The effect of the oxygen/fuel ratio on the flame flow and particles characteristics was analyzed, as well as the effect of particle diameter, shape, injection angle, and nitrogen flow rate on particle in-flight processing.

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