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:
Dec. 05, 2023

Filed:

Oct. 12, 2022
Applicant:

Government of the United States, As Represented BY the Secretary of the Air Force, Wright-Patterson AFB, OH (US);

Inventors:

Jared Neely, Troy, OH (US);

James Joo, Centerville, OH (US);

Russel Topp, Dayton, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); B64C 3/26 (2006.01); B64C 3/48 (2006.01); B64C 3/44 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B64C 3/26 (2013.01); B64C 3/48 (2013.01); F01D 5/141 (2013.01); B64C 2003/445 (2013.01); F05D 2250/90 (2013.01);
Abstract

A morphing airfoil includes a dynamic flexible skin system that is capable of carrying high level aerodynamic (or fluid) pressure loads over a structural surface. The structural surface can morph and bend in response to control inputs to change a lift force without separate movable control surfaces. A plurality of standoff mounts is attached to an inner surface of anisotropic skin. The standoff mounts include through apertures for receiving a flexible stringer. The anisotropic skin is attached to underlying structure through the flexible stringers. The flexible stringers interface with actuated position control ribs and passive compliant support ribs. A control system causes the underlying support structure to move to a desired location which in turn causes the skin to bend and/or flex without exceeding a stress threshold and thus vary the lift and drag distributions along a span of the airfoil without separate control surfaces.


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