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.
Patent No.:
Date of Patent:
Mar. 10, 2015
Filed:
Jun. 13, 2014
Applicant:
Gulfstream Aerospace Corporation, Savannah, GA (US);
Inventor:
Timothy R. Conners, Savannah, GA (US);
Assignee:
Gulfstream Aerospace Corporation, Savannah, GA (US);
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 7/08 (2006.01); F02K 99/00 (2009.01); F02B 27/00 (2006.01); B64D 33/02 (2006.01); F02K 1/34 (2006.01); B64D 29/00 (2006.01); F02K 3/02 (2006.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); B64D 33/06 (2013.01); B64D 29/00 (2013.01); F02K 3/025 (2013.01); B64D 2033/026 (2013.01); B64D 2033/0273 (2013.01);
Abstract
A supersonic nacelle design employing a bypass flow path internal to the nacelle and around the engine is disclosed herein. A set of aerodynamic vanes may be used to shape a supersonic airflow within a bypass around an engine. The vanes may be capable of compressing the supersonic airflow into a subsonic airflow, direct the subsonic airflow around the engine, and then expand the subsonic airflow into a supersonic exhaust. The vanes may shape the airflow by reducing sonic boom strength, cowl drag, and airframe interference drag.