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. 21, 2020

Filed:

Nov. 10, 2014
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Peter Z. Anast, Sammamish, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01); B64C 1/18 (2006.01);
U.S. Cl.
CPC ...
B64C 1/069 (2013.01); B64C 1/061 (2013.01); B64C 1/18 (2013.01);
Abstract

A fuselage portion of a vehicle (e.g., an aircraft) is disclosed. The fuselage portion comprises a frame; a floor beam attached to the frame and comprising ends; a structural stanchion comprising a first end and a second end; a first structural coupling joining the first end of the structural stanchion and the floor beam; a second structural coupling joining the second end of the structural stanchion and the frame; a non-structural stanchion comprising a third end and a fourth end; a first non-structural coupling joining the third end of the non-structural stanchion and the floor beam; and a second non-structural coupling joining the fourth end of the non-structural stanchion and the frame.


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Anast, Peter. (2020). Fuselage with structural and non-structural stanchions (U.S. Patent No. 10625844). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10625844

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