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:
Apr. 13, 2021

Filed:

Oct. 22, 2018
Applicants:

Troy S Prince, West Hartford, CT (US);

Richard Kolacinski, Merrimack, NH (US);

Mehul Patel, Chandler, AZ (US);

Inventors:

Troy S Prince, West Hartford, CT (US);

Richard Kolacinski, Merrimack, NH (US);

Mehul Patel, Chandler, AZ (US);

Assignee:

Orbital Research Inc., Cleveland, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 5/12 (2006.01); F42B 15/01 (2006.01); B64C 23/06 (2006.01); F42B 10/64 (2006.01); G05D 1/00 (2006.01); F41G 7/00 (2006.01); B64C 21/00 (2006.01); G05D 1/08 (2006.01); F42B 10/62 (2006.01); F42B 10/02 (2006.01); F42B 10/14 (2006.01); F42B 10/60 (2006.01); F42B 10/00 (2006.01);
U.S. Cl.
CPC ...
B64C 5/12 (2013.01); B64C 21/00 (2013.01); B64C 23/06 (2013.01); F41G 7/00 (2013.01); F42B 10/02 (2013.01); F42B 10/14 (2013.01); F42B 10/60 (2013.01); F42B 10/62 (2013.01); F42B 10/64 (2013.01); F42B 15/01 (2013.01); G05D 1/0088 (2013.01); G05D 1/0816 (2013.01);
Abstract

The present invention relates to a missile or aircraft with a hierarchical, modular, closed-loop flow control system and more particularly to aircraft or missile with a flow control system for enhanced aerodynamic control, maneuverability and stabilization. The present invention further relates to flow control system involving different elements including flow sensors, active flow control device or activatable flow effectors and logic devices with closed loop control architecture. The active flow control device or activatable flow effectors of these various embodiments are adapted to be activated, controlled, and deactivated based on signals from the sensors to achieve a desired stabilization or maneuverability effect. The logic devices are embedded with a hierarchical control structure allowing for rapid, real-time control at the flow surface.


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