Method for manufacturing and attachment of wing fairings

Plastic and nonmetallic article shaping or treating: processes – Mechanical shaping or molding to form or reform shaped article – To produce composite – plural part or multilayered article

Reexamination Certificate

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C264S261000, C244S171700

Reexamination Certificate

active

07998392

ABSTRACT:
A method and apparatus for manufacturing and installing a fairing on an aircraft. In one advantageous embodiment, a composite fairing is installed on the aircraft. A composite sheet having a form of the composite fairing is formed. A plurality of cured composite tiles is created from the composite sheet, wherein spaces are present between the plurality of composite tiles. The plurality of composite tiles is cured to form the composite fairing. The composite fairing is attached to a surface of the aircraft. The spaces between the plurality of composite tiles are filled with a flexible filler.

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patent: 2006/0060705 (2006-03-01), Stulc et al.
patent: 2006/0083902 (2006-04-01), Jarosz et al.
patent: 1834873 (2007-09-01), None

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