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:
Jan. 23, 2024

Filed:

Nov. 09, 2021
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Gregory A. Cass, Seattle, WA (US);

Ian E. Schroeder, Seattle, WA (US);

Khanh M. Pham, Tukwila, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/18 (2006.01); B32B 3/08 (2006.01); B32B 5/26 (2006.01); B32B 5/10 (2006.01); B29C 65/00 (2006.01); B32B 38/00 (2006.01); B32B 3/10 (2006.01); B32B 38/10 (2006.01);
U.S. Cl.
CPC ...
B64C 3/182 (2013.01); B29C 66/0326 (2013.01); B32B 3/085 (2013.01); B32B 5/10 (2013.01); B32B 5/26 (2013.01); B32B 38/0004 (2013.01); B32B 38/10 (2013.01); B32B 2038/0076 (2013.01); B32B 2260/023 (2013.01); B32B 2605/18 (2013.01);
Abstract

Provided are stiffened stringer panels with integrated shim structures. An example composite panel comprises a skin member having an inner surface, and a stringer positioned on the inner surface. The stringer comprises a first flange portion and a second flange portion with the first flange portion and the second flange portion contacting the inner surface. The composite panel further comprises an integrated shim positioned on the first flange portion. The integrated shim may comprise a sacrificial material configured to be trimmed to the desired geometry. The sacrificial material may comprise a glass fiber reinforced plastic fabric pre-impregnated with resin. The integrated shim may be configured to interface with internal support structures of a wing assembly. The integrated shim may be configured to be machined to fit dimensions and measurements corresponding to the internal support structures of the wing assembly.


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