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:
Nov. 29, 2022

Filed:

May. 27, 2020
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Joseph H. Campana, Mill Creek, WA (US);

William H. Pearson, Redmond, WA (US);

Charles R. Coates, Renton, WA (US);

Kevin P. Ryder, Kirkland, WA (US);

Peter J. Newnham, Mukilteo, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/26 (2006.01); B64C 5/06 (2006.01); B64F 5/10 (2017.01); B64C 7/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/26 (2013.01); B64C 5/06 (2013.01); B64C 7/00 (2013.01); B64F 5/10 (2017.01);
Abstract

An aircraft has a vertical stabilizer having a multi-spar box and a base rib assembly secured to the multi-spar box. The base rib assembly has a pair of middle longitudinal lugs between a front and rear of the base rib assembly, a pair of front lateral lugs along the front of the base rib assembly, and a pair of rear lateral lugs along the rear of the base rib assembly. There are no lateral lugs between the pairs of middle lugs. A pair of middle clevises extend through corresponding apertures in an outer skin of the fuselage and are secured to one of the plurality of frame members and a plurality of retaining members are inserted through mounting holes in each middle longitudinal lug and mounting holes in each middle clevis to secure the vertical stabilizer to the aircraft fuselage.


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