The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 18, 2017

Filed:

Jan. 24, 2014
Applicant:

Spectrum Aeronautical, Llc, Carlsbad, CA (US);

Inventors:

Larry J. Ashton, Springville, UT (US);

Michael G. Allman, Spanish Fork, UT (US);

Troy L. White, Goshen, UT (US);

Benko S. Ta'ala, Elk Ridge, UT (US);

Assignee:

Spectrum Aeronautical, LLC, Carlsbad, unknown;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B29C 70/02 (2006.01); B29C 65/00 (2006.01); B29C 70/34 (2006.01); B29D 99/00 (2010.01); B29C 65/02 (2006.01); B29C 35/02 (2006.01); B29K 63/00 (2006.01); B29K 105/06 (2006.01); B29K 307/00 (2006.01);
U.S. Cl.
CPC ...
B29C 70/023 (2013.01); B29C 65/02 (2013.01); B29C 66/438 (2013.01); B29C 66/63 (2013.01); B29C 66/636 (2013.01); B29C 66/721 (2013.01); B29C 66/7212 (2013.01); B29C 66/72141 (2013.01); B29C 66/7394 (2013.01); B29C 66/919 (2013.01); B29C 66/91411 (2013.01); B29C 66/91431 (2013.01); B29C 66/929 (2013.01); B29C 66/9241 (2013.01); B29C 66/949 (2013.01); B29C 70/342 (2013.01); B29D 99/0014 (2013.01); B29C 35/02 (2013.01); B29C 66/71 (2013.01); B29K 2063/00 (2013.01); B29K 2105/06 (2013.01); B29K 2307/00 (2013.01);
Abstract

A method for manufacturing rigid panels made of a composite material requires a caul sheet having a smooth surface that is formed with a plurality of grooves. A first layer of the composite material is laid on the caul sheet, and is cut to create flaps that extend into the respective grooves. Strips of composite material are then placed along the edges of the groove to extend and overlap each other in the groove. Next, a unidirectional ply is placed along the length of the groove, and this combination is then covered with a second layer of the composite material. Together, the combination of the first and second layers, the strips and the unidirectional ply are co-cured to create a rigid panel with integral stiffening members.


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