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:
Jul. 28, 2015

Filed:

Oct. 13, 2010
Applicants:

Edward A. Whalen, St. Louis, MO (US);

Mark I. Goldhammer, Bellevue, WA (US);

Inventors:

Edward A. Whalen, St. Louis, MO (US);

Mark I. Goldhammer, Bellevue, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 5/06 (2006.01); B64C 9/00 (2006.01); F15D 1/00 (2006.01); B64C 21/00 (2006.01); B64C 23/00 (2006.01); B64C 23/06 (2006.01);
U.S. Cl.
CPC ...
B64C 5/06 (2013.01); B64C 21/00 (2013.01); B64C 23/005 (2013.01); B64C 23/06 (2013.01); B64C 2230/04 (2013.01); B64C 2230/16 (2013.01); Y02T 50/162 (2013.01); Y02T 50/166 (2013.01);
Abstract

Systems and methods described herein provide for the control of airflow over a vertical control surface of an aircraft to enhance the forces produced by the surface. According to one aspect of the disclosure provided herein, the vertical control surface of the aircraft is engaged by active flow control actuators that interact with the ambient airflow to alter one or more characteristics of the airflow. An actuator control system detects a flow control event, and in response, activates the active flow control actuators to alter the airflow. According to various aspects, the flow control event is associated with a separation of the airflow, which is corrected through the activation of the appropriate active flow control actuators, increasing the forces produced by the vertical control surface of the aircraft.


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