System and method for composite panel finishing
AssigneeTextron Aviation Inc.
InventorsBrian Keith Jacobs, Patrick Allen Stanton
Life of this patent
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AssigneeTextron Aviation Inc.
InventorsBrian Keith Jacobs, Patrick Allen Stanton
Estimating the term…
A system and method for finishing a composite panel having undesired pores formed therethrough. A sander receives and scuffs up one or more surfaces of the composite panel and a roller receives liquid UV sealant from a source of UV sealant and rolls the UV sealant onto at least one surface of the composite panel, such that the UV sealant at least partially fills the pores. Then, a curing apparatus cures the UV sealant applied to the composite panel. The sanding, UV application, and curing steps may be performed once or numerous times depending on how many layers are needed to sufficiently smooth out surfaces of the composite panel such that the pores are no longer detectable, and the finished surfaces of the composite panel are ready for painting or other post-finishing processes/subsequent decorative applications.
1-8. (canceled)
A method of finishing a composite panel having a plurality of irregularities formed therein or therethrough, the method comprising:
A method of finishing a composite panel, the method comprising:
Dependencies are inferred from the claim text.