Structural element with rib-receiving member

Stock material or miscellaneous articles – Structurally defined web or sheet – Including variation in thickness

Reexamination Certificate

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Details

C428S057000, C428S053000, C428S120000, C428S119000, C428S133000, C428S137000, C428S163000, C428S167000

Reexamination Certificate

active

10154207

ABSTRACT:
A structural element for use in aerospace applications such as a structural element suitable as an aircraft component is described. The composite structure comprises: (a) a rib having a first end and a second end; (b) at least one member such as a face sheet having an inner surface and an outer surface; and (c) a rib-receiving member integral to the inner surface of the at least one member, wherein the rib-receiving member comprises at least one rib-receiving element having an opening therein for receiving the first end of the rib and at least one cover sheet having an opening therein for receiving the first end of the rib.

REFERENCES:
patent: 4177306 (1979-12-01), Schulz et al.
patent: 5273806 (1993-12-01), Lockshaw et al.
patent: 5476704 (1995-12-01), Kohler
patent: 5487930 (1996-01-01), Lockshaw et al.
patent: 5508085 (1996-04-01), Lockshaw et al.
patent: 5580622 (1996-12-01), Lockshaw et al.
patent: 5616376 (1997-04-01), Lockshaw et al.
patent: 5633053 (1997-05-01), Lockshaw et al.
patent: 5688426 (1997-11-01), Kirkwood et al.
patent: 5849393 (1998-12-01), Slattery
patent: 6374570 (2002-04-01), McKague, Jr.
patent: 6520706 (2003-02-01), McKague et al.
patent: 027107 (1986-07-01), None
patent: 0 257 148 (1988-03-01), None
patent: WO 02/16197 (2002-02-01), None
patent: WO 02/16784 (2002-02-01), None
patent: WO 03/018295 (2003-03-01), None
patent: WO 03/020496 (2003-03-01), None
“Quality Assurance for Composite Bonding” by Richard H. Bossi and Robert L. Nerenberg, Boeing Phantom works, Seattle, WA;45thInternational SAMPE Symposium,May 21-25, 2000; pp. 1787-1786.
U.S. Appl. No. 10/154,178, filed May 23, 2002, by Basil Hammi and Claude Hubert for “Structural Element With Rib-Receiving Member”.
“Composite Grid-Lock® Pre-Implementation Program” paper presented to U.S. Air Force Research Laboratory Flight Dynamics Directorate (Jan. 2001).
F-16 Horizontal Tail and Edges Sustainment dated Nov. 3, 2000.
Owens et al., “Tension Pull-off and Shear Text Methods to Characterize 3-D Textile Reinforced Bonded Composite Tee Joints,” 1999, pp. 398-409.

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