Woven preform for structural joints

Textiles: weaving – Fabrics – Drier felts

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C139S38300A, C139SDIG001, C442S205000

Reexamination Certificate

active

06874543

ABSTRACT:
A preform for structural joints has a three-dimensional weave architecture with fill fibers woven to provide layer-to-layer interlocking of layers of warp fiber as well as interlocking of fibers within each layer. At least two legs extend from a base, the base and legs each having at least two layers of warp fibers. The legs are connected at a symmetrical, distributed-column intersection, with an odd number of columns of warp fibers being located being the legs. The outer ends of the base and legs preferably have tapers formed from terminating layers of warp fibers in a stepped pattern. Tracer fibers that include a colored strand and an x-ray opaque strand are woven into the preform at selected locations as a warp fiber. The tracer fibers allow for identification of a selected location or a selected portion of the preform through visual inspection or by x-ray image.

REFERENCES:
patent: 4063684 (1977-12-01), O'Brian et al.
patent: 4376710 (1983-03-01), Gardos et al.
patent: 4379798 (1983-04-01), Palmer et al.
patent: 4669523 (1987-06-01), Sabatie et al.
patent: 4671470 (1987-06-01), Jonas
patent: 4717302 (1988-01-01), Adams et al.
patent: 4778637 (1988-10-01), Adams et al.
patent: 4782864 (1988-11-01), Abildskov
patent: 4786548 (1988-11-01), Place, Jr.
patent: 4902326 (1990-02-01), Jarmon
patent: 4922968 (1990-05-01), Bottger et al.
patent: 5026595 (1991-06-01), Crawford, Jr. et al.
patent: 5042565 (1991-08-01), Yuen et al.
patent: 5085252 (1992-02-01), Mohamed et al.
patent: 5108830 (1992-04-01), Osaka et al.
patent: 5137058 (1992-08-01), Anahara et al.
patent: 5184706 (1993-02-01), Christensen
patent: 5236020 (1993-08-01), Sakatani et al.
patent: 5263516 (1993-11-01), van Schuylenburch
patent: 5270094 (1993-12-01), Anahara et al.
patent: 5334414 (1994-08-01), Edie et al.
patent: 5343897 (1994-09-01), Sakatani et al.
patent: 5348056 (1994-09-01), Tsuzuki
patent: 5397595 (1995-03-01), Carroll et al.
patent: 5399418 (1995-03-01), Hartmanns et al.
patent: 5451448 (1995-09-01), Sawko et al.
patent: 5465760 (1995-11-01), Mohamed et al.
patent: 5487941 (1996-01-01), Pepin
patent: 5540260 (1996-07-01), Mood
patent: 5540877 (1996-07-01), Repetto et al.
patent: 5616175 (1997-04-01), Walsh
patent: 5651474 (1997-07-01), Callaghan et al.
patent: 5657795 (1997-08-01), Sawko et al.
patent: 5720339 (1998-02-01), Glass et al.
patent: 5759620 (1998-06-01), Wilson et al.
patent: 5767023 (1998-06-01), Berger et al.
patent: 5783279 (1998-07-01), Edgson et al.
patent: 5785094 (1998-07-01), Yoshida
patent: 5804277 (1998-09-01), Ashbee
patent: 5833802 (1998-11-01), Yasui et al.
patent: 5840221 (1998-11-01), Lau et al.
patent: 5952075 (1999-09-01), Clarke et al.
patent: 5962135 (1999-10-01), Walker et al.
patent: 5981022 (1999-11-01), Min et al.
patent: 6003563 (1999-12-01), Uchida et al.
patent: 6010652 (2000-01-01), Yoshida
patent: 6013226 (2000-01-01), Steel et al.
patent: 6019138 (2000-02-01), Malck et al.
patent: 6124015 (2000-09-01), Baker et al.
patent: 6129122 (2000-10-01), Bilisik
patent: 6207598 (2001-03-01), Lee et al.
patent: 6228453 (2001-05-01), Fareed et al.
patent: 6338367 (2002-01-01), Khokar
patent: 6470916 (2002-10-01), Uchida et al.
patent: 6555488 (2003-04-01), Qiu et al.
patent: 6712099 (2004-03-01), Schmidt et al.
patent: 6742547 (2004-06-01), Bryn et al.
Owens et al.;Tension Pull-off and Shear Test Methods to Characterize 3-D Textile Reinforced Bonded Composite Tee-Joints0 ; published 2000; Composite Structures, Theory and Practice, Editors: Peter Grant and Carl Q. Roosseau.
Sheahan et al.;Primary Sandwich Structure, A Unitized Approach; copyright 2000 by Lockheed Martin; published by the American Institute of Aeronautics and Astronauts, Inc.; pp. 1-8.
Sheahan et al.;Robust Composite Sandwich Structures; copyright 1998 by Lockheed Martin; published by the American Institute of Aeronautics and Astronauts, Inc.; pp. 1-12.
Bersuch et al.;Affordable Composite Structure for Next Generation Fighters; copyright 1998 by Lockheed Martin, published by Society for the Advancement of Material and Process Engineering; pp. 1-11.
Wanthal et al.;Interlaminar Reinforced Composites Development for Improved Damage Tolerance; copyright 2000 by the Boeing Company, Lockheed Martin; Northrop Grunman; Society for the Advancement of Material and Process Engineering; 15 pages.
Bersuch et al.;3-D Composites in Primary Aircraft Structure Joints; published Jan. 1997 AGARD Bolted/onded Joints in Polymeric Composites; pp. 16-1—16-10.
Sheahan et al;Affordable 3-D Intergrated Composite Structures; copyright 2000 by Lockheed Martin; published by the Universal Technology Corporation; 20 pages.
Steven Clark;A Comparison of Braiding, Knitting and Weaving Technologies, Engineered Textile Preforms for RTM; Oct. 28-Nov. 1, 1997, pp. 15-23.
Wilson et al.;<<SPARC>>5 Axis, 3-D Woven, Low Crimp Preforms; Bombardier Aerospace, Short Brothers pplc, May 31-Jun. 4, 1998, pp. 102-113.
Hans Walter Kipp;Narrow Fabric Weaving; 1989, pp. 221-227.
Citations from Engineering Index; EIX (including abstracts).
Sketches of BRM Products.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Woven preform for structural joints does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Woven preform for structural joints, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Woven preform for structural joints will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3420580

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.