Characterization of Droplet Flight Path and Mass Flux in Droplet-Based
Manufacturing
by
Godard Karl Abel
B.S. in Mechanical Engineering
Massachusetts Institute of Technology
1993
Submitted to the Department of Mechanical Engineering in Partial Fulfillment
of the Requirements for the Degree of
MASTER OF SCIENCE IN MECHANICAL ENGINEERING
at the
MASSACHUSETTS INSTITUTE OF TECHNOLOGY
May 1994
ABSTRACT
In this study, the droplet flight path and the mass flux in the Uniform
Droplet Spray Forming (UDS) process are characterized through numerical
simulation and experiments. In the UDS process electrically charged uniform
diameter metal droplet sprays are used to spray form deposits onto stationary
and moving substrates. A numerical simulation based on physical models
was developed to predict the droplet velocity, the droplet spray cone spreading,
the mass flux distribution in the spray, and the cross-sectional shapes
of deposits spray formed with a moving substrate.
To verify the numerical simulation results experiments were performed to
measure the droplet charging, the droplet velocity, the droplet scattering,
and the deposit cross-sectional shapes. The charging and scattering experiments
were performed with 200mm diameter Sn droplets. The velocity was measured
as a function of flight distance for 95mm and 200mm diameter Sn droplets.
The deposit cross-sections were measured for 200mm diameter Sn-40%Pb sprays
collected at a flight distance of 300mm and for 200mm diameter Sn-5%Pb
droplets at a flight distance of 480mm. The experimental results agreed
with the simulation results to within approximately 10% for the charging,
velocity, and scattering experiments. There was a larger discrepancy between
the shape of cross-sectional deposits due to variations in the process
and the impact behavior of the droplets. This numerical simulation can
be used to predict droplet flight path and mass flux for single and multiple
orifice sprays.
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