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:
Nov. 11, 2014

Filed:

Nov. 18, 2011
Applicants:

Jeffrey F. Stulc, Seattle, WA (US);

Wallace C. Chan, Seattle, WA (US);

Brian C. Clapp, Seattle, WA (US);

Neal G. Rolfes, Seattle, WA (US);

Inventors:

Jeffrey F. Stulc, Seattle, WA (US);

Wallace C. Chan, Seattle, WA (US);

Brian C. Clapp, Seattle, WA (US);

Neal G. Rolfes, Seattle, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/00 (2006.01); B64C 1/14 (2006.01); B64C 1/06 (2006.01); B64C 1/12 (2006.01);
U.S. Cl.
CPC ...
B64C 1/068 (2013.01); Y02T 50/43 (2013.01); B64C 1/069 (2013.01); B64C 1/1492 (2013.01); B64C 1/12 (2013.01); Y02T 50/433 (2013.01); B64C 2001/0072 (2013.01);
Abstract

Structures and methods for joining composite fuselage sections and other panel assemblies together. In one embodiment, a shell structure configured in accordance with the present invention includes a first panel portion positioned adjacent to a second panel portion. The first panel portion can include a first stiffener attached to a first composite skin, and the second panel portion can include a second stiffener attached to a second composite skin. The shell structure can further include a fitting extending across a first edge region of the first panel portion and a second edge region of the second panel portion. A first end portion of the fitting can be attached to the first stiffener and the first composite skin, and a second end portion of the fitting can be attached to a second stiffener and a second composite skin, to join the first panel portion to the second panel portion.


Find Patent Forward Citations

Loading…