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.

Patent No.:

US 9511845 B1

PDF
Full Text
Expired
Date of Patent:
Dec. 06, 2016

Filed:

Jan. 24, 2014
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Magdalena Boyen, Metten, DE;

Wolfgang Eilken, Hamburg, DE;

Wolfgang Schulze, Hasloh, DE;

Assignee:

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01); B29C 67/00 (2006.01); B64C 1/10 (2006.01);
U.S. Cl.
CPC ...
B64C 1/061 (2013.01); B29C 67/0051 (2013.01); B64C 1/064 (2013.01); B64C 1/069 (2013.01); B64C 1/10 (2013.01); Y10T 29/49826 (2015.01);
Abstract

An aircraft frame includes a first partial aircraft frame configured to be attached to a first aircraft fuselage segment, and a second partial aircraft frame configured to be attached to a second aircraft fuselage segment. The first and second partial aircraft frames include corresponding first and second stringer coupling sections. The first partial aircraft frame and the second partial aircraft frame are configured to be attached to each other via a first web and a second web. The first stringer coupling section is located between the first inner flange and the first outer flange and the second stringer coupling section is located between the second inner flange and the second outer flange. The first stringer coupling section includes a first wall which extends from the first web into the first section of the first partial aircraft frame, and the second stringer coupling section comprises a second wall, which extends from the second web into the second section of the second partial aircraft frame.


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Boyen, Magdalena. (2016). Aircraft frame (U.S. Patent No. 9511845). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9511845

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