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:
Feb. 28, 2017

Filed:

Feb. 10, 2014
Applicant:

Gulfstream Aerospace Corporation, Savannah, GA (US);

Inventor:

Donald Freund, Savannah, GA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 23/00 (2006.01); B64C 30/00 (2006.01); B64C 37/00 (2006.01); B64C 3/38 (2006.01); B64C 3/42 (2006.01); B64C 9/00 (2006.01); B64C 3/18 (2006.01); B64C 3/20 (2006.01); B64C 17/10 (2006.01); B64D 37/00 (2006.01);
U.S. Cl.
CPC ...
B64C 23/00 (2013.01); B64C 3/185 (2013.01); B64C 3/20 (2013.01); B64C 3/38 (2013.01); B64C 3/42 (2013.01); B64C 9/00 (2013.01); B64C 17/10 (2013.01); B64C 30/00 (2013.01); B64D 37/00 (2013.01); Y02T 50/145 (2013.01); Y02T 50/44 (2013.01);
Abstract

A system for controlling a magnitude of a sonic boom caused by off-design operation of a supersonic aircraft includes a sensor configured to detect a condition of the supersonic aircraft. The system further includes a control surface that is mounted to a wing of the supersonic aircraft. The system still further includes a processor communicatively coupled to the sensor and operatively coupled with the control surface. The processor is configured to (1) receive information from the sensor indicative of the condition of the supersonic aircraft, (2) determine that there is a deviation between a lift distribution and a design-condition lift distribution based on the information, and (3) control the control surface to move in a manner that reduces the deviation. The magnitude of the sonic boom is reduced when the deviation is reduced.


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