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. 07, 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 17/10 (2006.01); B64C 23/00 (2006.01); B64C 30/00 (2006.01); B64D 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);
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 includes a first sensor configured to detect a first condition of the supersonic aircraft. The system further includes a pair of wings configured to move fore and aft. The system further includes a processor communicatively coupled with the sensor and operatively coupled with the pair of wings. The processor is configured to (1) receive a first information from the first sensor indicative of the first condition, (2) calculate a lift distribution of the supersonic aircraft based on the first information, (3) determine an existence of a deviation of the lift distribution from a desired lift distribution based on the flight condition, and (4) control the pair of wings to move to redistribute the lift in a manner that more closely conforms to the desired lift distribution. The magnitude of the sonic boom is reduced when the deviation is reduced.


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