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. 30, 2024

Filed:

Apr. 23, 2021
Applicant:

United States of America As Represented BY the Administrator of Nasa, Washington, DC (US);

Inventors:

John C. Lin, Seaford, VA (US);

Latunia P. Melton, Yorktown, VA (US);

Mehti Koklu, Hampton, VA (US);

Marlyn Y. Andino, Newport News, VA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 9/02 (2006.01); B64C 9/16 (2006.01); B64C 9/18 (2006.01); B64C 21/04 (2023.01); B64C 13/40 (2006.01); B64D 41/00 (2006.01);
U.S. Cl.
CPC ...
B64C 13/40 (2013.01); B64C 9/02 (2013.01); B64C 9/16 (2013.01); B64C 9/18 (2013.01); B64C 21/04 (2013.01); B64D 41/00 (2013.01);
Abstract

A simple-hinged flap assembly for a winged aircraft includes a simple-hinged flap having a leading airfoil section pivotably connected to a trailing airfoil section via a hinge, and an active flow control (AFC) actuator assembly. The assembly is connected to or integrally formed with the flap and includes upstream and downstream AFC actuators arranged in respective first and second rows, and collectively configured to provide first and second outlet mass flowrates. The downstream AFC actuators emit the second outlet mass flowrate at a rate that substantially exceeds the first outlet mass flowrate, such that the first outlet mass flowrate preconditions a boundary layer around the simple-hinged flap assembly. A winged aircraft includes a pneumatic power supply, fuselage, a wing connected to the fuselage, and the simple-hinged flap assembly.


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