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:
Jan. 17, 2023

Filed:

May. 21, 2020
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Gregory Santini, Bothell, WA (US);

Kyle Alexander Johnson, Fall City, WA (US);

Bryan Gruner, Bellevue, WA (US);

Ross Westermeier, Seattle, WA (US);

Jan A. Kordel, Redmond, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/20 (2006.01); B64C 3/18 (2006.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
B64C 3/20 (2013.01); B64C 3/185 (2013.01); B33Y 80/00 (2014.12);
Abstract

Structural composite airfoils include a primary structural element, a secondary structural element defining the trailing edge of the structural composite airfoil, and a discrete leading edge structure defining the leading edge of the structural composite airfoil. The primary structural element includes an upper skin panel, a lower skin panel, and a middle C-channel spar that is coupled to the upper skin panel and the lower skin panel. The discrete leading edge structure is coupled to the upper leading edge end of the upper skin panel and to the lower leading edge end of the lower skin panel. The upper skin panel may include a first panel bend adjacent the discrete leading edge structure, and the lower skin panel may include a second panel bend adjacent the discrete leading edge structure.


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