CPC B05D 1/02 (2013.01) [B05B 13/02 (2013.01)] | 20 Claims |
1. A method of applying a spray treatment onto a surface of an airframe of an aircraft, the method using a set of multiple modular hood units, each modular hood unit of the set including one or more enclosure walls that partially defines a combined enclosure having a shared interior volume, the method comprising:
assembling the set of multiple modular hood units to define the combined enclosure by, for each modular hood unit of the set:
interfacing one or more surfaces of an interior of a fuselage of the airframe with at least two airframe-interfacing edges of the modular hood unit to define a portion of a spray treatment region of the airframe, and
interfacing at least one inter-unit-interfacing edge of the modular hood unit with at least another inter-unit-interfacing edge of a neighboring modular hood unit of the set to form at least a portion of the combined enclosure; and
spraying a treatment fluid onto a surface of the airframe within the spray treatment region bounded by the combined enclosure.
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