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:
Feb. 09, 2021

Filed:

Jan. 14, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Steven Paul Walker, Arlington, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/26 (2006.01); B64F 5/10 (2017.01); F16B 5/02 (2006.01); B64C 3/34 (2006.01); B64C 3/18 (2006.01); F16B 33/00 (2006.01);
U.S. Cl.
CPC ...
B64F 5/10 (2017.01); B64C 3/187 (2013.01); B64C 3/26 (2013.01); B64C 3/34 (2013.01); F16B 5/02 (2013.01); F16B 33/004 (2013.01);
Abstract

Metallic fittings for coupling composite ribs to skin panels of aircraft wings are described. An example metallic fitting includes a through hole configured to receive a fastener. The fastener is configured to couple the metallic fitting to a composite rib of an aircraft wing. The example metallic fitting further includes a bore configured to receive a bolt. The example metallic fitting further includes a cavity intersecting the bore. The cavity has an access opening. The example metallic fitting further includes a barrel nut located within the cavity. The barrel nut is configured to threadably engage the bolt to couple the metallic fitting to a skin panel of the aircraft wing. The example metallic fitting further includes a seal located within the cavity. The seal is configured to close the access opening.


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