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:
Jul. 28, 2015

Filed:

Dec. 15, 2011
Applicants:

Harinder S. Oberoi, Snohomish, WA (US);

Blair P. Nelson, Seattle, WA (US);

Alan S. Draper, Everett, WA (US);

Charles Y. HU, Newcastle, WA (US);

Randall Matthewson, Stanwood, WA (US);

Branko Sarh, Huntington Beach, CA (US);

Inventors:

Harinder S. Oberoi, Snohomish, WA (US);

Blair P. Nelson, Seattle, WA (US);

Alan S. Draper, Everett, WA (US);

Charles Y. Hu, Newcastle, WA (US);

Randall Matthewson, Stanwood, WA (US);

Branko Sarh, Huntington Beach, CA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 5/00 (2006.01);
U.S. Cl.
CPC ...
B64F 5/0009 (2013.01); B64F 5/0036 (2013.01); Y10T 29/49622 (2015.01); Y10T 29/534 (2015.01); Y10T 29/53004 (2015.01); Y10T 29/53417 (2015.01); Y10T 29/53974 (2015.01);
Abstract

A method of assembling a panelized aircraft fuselage comprises loading a keel structure on a cradle; attaching stanchions to a floor grid; positioning the floor grid and stanchions over the keel structure and attaching the stanchions to the keel structure; obtaining a full fuselage contour including locating lower panels on the floor grid while using the cradle, the floor grid, and the keel structure to support the lower panels, and locating upper panels on the lower panels; and fastening the lower panels to the keel structure and the upper panels. The fuselage is assembled upright from the keel structure without changing orientation of the fuselage.


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