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:
Mar. 29, 2022

Filed:

Dec. 13, 2018
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

William Tulloch, Bristol, GB;

Pat Broomfield, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/34 (2006.01); B64D 45/02 (2006.01); B64D 37/02 (2006.01); B64C 3/32 (2006.01); B64D 27/26 (2006.01); F16B 35/00 (2006.01); F16B 37/14 (2006.01); F16B 37/04 (2006.01); F16B 33/00 (2006.01); F16B 5/06 (2006.01); F16B 19/02 (2006.01);
U.S. Cl.
CPC ...
B64C 3/34 (2013.01); B64C 3/32 (2013.01); B64D 27/26 (2013.01); B64D 37/02 (2013.01); B64D 45/02 (2013.01); F16B 35/00 (2013.01); F16B 37/048 (2013.01); F16B 37/14 (2013.01); F16B 37/145 (2013.01); B64D 2027/264 (2013.01); F16B 5/0642 (2013.01); F16B 19/02 (2013.01); F16B 33/002 (2013.01); F16B 33/004 (2013.01);
Abstract

An assembly with an aircraft fuel tank is disclosed having a captive nut with an internal thread, a secondary structure, and a fastener which secures the secondary structure to the fuel tank. The fastener has a shaft which passes through the secondary structure and has an external thread coupled to the internal thread of the captive nut. The fuel tank has a fuel tank element with a hole, and the captive nut has a sleeve which is located in the hole with an interference fit between an outer surface of the sleeve and an inner surface of the wall of the hole.


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