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:
Sep. 20, 2016

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); 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); B64C 17/10 (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

Methods and systems for controlling a magnitude of a sonic boom caused by off-design-condition operation of a supersonic aircraft at supersonic speeds are disclosed herein. The method includes, but is not limited to, monitoring, with a processor, a weight of the supersonic aircraft and a distribution of fuel onboard the supersonic aircraft. The method further includes, but is not limited to, determining, with the processor, that there is a deviation of the weight of the supersonic aircraft from a design-condition weight. The method still further includes, but is not limited to, controlling, with the processor, a redistribution of the fuel onboard the supersonic aircraft to adjust an amount of fuel stored within a wing to minimize a twist in the wing caused by the deviation. Such redistribution will reduce the magnitude of the sonic boom caused by the deviation.


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