Wheat starch blast cleaning is used increasingly to remove organic coatings
from aircraft. The process was investigated to clarify aspects of the mech
anism by which a urethane topcoat and an epoxy primer are removed from alum
inum and three epoxy composites (carbon, glass, and aramid fiber). Experime
nts included an examination of the impact sites created by individual wheat
starch particles, the measurement of particle size, shape and velocity, an
d the determination of paint stripping rates. The velocity distribution of
wheat starch particles was also studied using a simplified theoretical mode
l. Paint removal rates were found to depend strongly on impact angle, mass
flow rate, particle velocity and size, and the rigidity of the substrate (c
omposite or aluminum). The urethane topcoat was found to be removed in a cu
mulative fashion by chipping. Selective stripping was possible for this coa
ting system; i.e., it was possible to remove the topcoat while leaving the
underlying primer intact. The susceptibility of composite substrates to dam
age varied with the type of fiber reinforcing, with aramid fiber being much
more sensitive than carbon fiber. (C) 1999 Published by Elsevier Science S
.A. All rights reserved.