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. 15, 2013

Filed:

May. 10, 2012
Applicants:

Daniel N. Miller, Bainbridge Island, WA (US);

Brent N. Mccallum, Fort Worth, TX (US);

Stewart A. Jenkins, Keller, TX (US);

David M. Wells, Fort Worth, TX (US);

Inventors:

Daniel N. Miller, Bainbridge Island, WA (US);

Brent N. McCallum, Fort Worth, TX (US);

Stewart A. Jenkins, Keller, TX (US);

David M. Wells, Fort Worth, TX (US);

Assignee:

Lockheed Martin Corporation, Bethesda, MD (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 21/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

Systems to provide distributed flow control actuation to manage the behavior of a global flow field, are provided. An example of a system can include an aerodynamic structure having an outer surface, and an array of a plurality of nano-scale effectors connected to the outer surface of the aerodynamic structure to be in fluid contact with a flowing fluid when operationally flowing, to induce controlled, globally distributed disturbances at a viscous wall sublayer of a turbulent boundary layer of the flowing fluid when operationally flowing and to manipulate fluid behavior of the flowing fluid to thereby substantially reduce pressure loss associated with incipient separation of the fluid flow from portions of the aerodynamic structure.


Find Patent Forward Citations

Miller, Daniel. (2013). System for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation (U.S. Patent No. 8353482). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/8353482

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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