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. 02, 2021

Filed:

Sep. 11, 2019
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

George Ryan Decker, Fort Worth, TX (US);

Steven Allen Robedeau, Jr., Keller, TX (US);

Tjepke Heeringa, Dallas, TX (US);

David Gordon Carlson, N. Richland Hills, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/26 (2006.01); B64C 3/18 (2006.01); B64C 1/00 (2006.01); B64C 29/00 (2006.01);
U.S. Cl.
CPC ...
B64C 3/26 (2013.01); B64C 3/18 (2013.01); B64C 29/0033 (2013.01); B64C 2001/0072 (2013.01);
Abstract

A wing assembly for an aircraft includes a torque box sleeve having an open end and a plurality of integral sides including leading, aft, top and bottom sides that jointlessly form a continuous surface having a generally airfoil shape. The wing assembly includes an internal support subassembly having a plurality of ribs coupled to a central spar. The internal support subassembly is formed into a single component outside the torque box sleeve and inserted into the open end of the torque box sleeve as the single component. The internal support subassembly is coupled to an interior of the torque box sleeve.


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