Plastic and nonmetallic article shaping or treating: processes – Pore forming in situ – Composite article making
Reexamination Certificate
2008-07-29
2011-10-11
Del Sole, Joseph S. (Department: 1743)
Plastic and nonmetallic article shaping or treating: processes
Pore forming in situ
Composite article making
C246S045000, C246S046000, C246S046000, C246S046000, C246S219000, C156S242000, C156S245000, C156S285000, C156S381000, C156S079000
Reexamination Certificate
active
08034268
ABSTRACT:
A lightweight composite fairing bar (14) for use in fabricating a composite component (16) of an aircraft. The fairing bar (14) includes a core (18) and an elongated outer shell (20) surrounding the core (18). The outer shell (20) is comprised of a laminate material, and the core (18) is comprised of epoxy syntactic foam having a lower density than that of the laminate material. The outer shell (20) is configured for supporting the composite component (16) during the manufacture of the same.
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Albright Dennis L.
Clark Randall R.
Hackler David W.
Del Sole Joseph S.
Malekzadeh Seyed Masoud
Ostranger Chong Flaherty & Broitman P.C.
The Boeing Company
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