An aircraft brake assembly incorporating components which are sensitive to heat
and to contact with substances present in runway,.e.g., de-icer compositions and
cleansing liquids. The assembly includes an external member to shield the components
from the liquids. The external member may comprise a rigid or flexible, fluid-impermeable
or porous material located to receive and retain the liquids. Heat generated through
the use of the brake assembly may evaporate any liquid settled on the external
member or at least discourage any liquid from settling thereon.
