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:
Feb. 18, 2020
Filed:
Jul. 26, 2016
Applicant:
Rolls-royce North American Technologies, Inc., Indianapolis, IN (US);
Inventors:
David L. Sutterfield, Greenwood, IN (US);
Bryan H. Lerg, Carmel, IN (US);
Assignee:
Rolls-Royce North American Technologies Inc., Indianapolis, IN (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/00 (2006.01); F02K 1/28 (2006.01); F02K 1/46 (2006.01); F02K 3/02 (2006.01); B64C 15/02 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
F02K 1/002 (2013.01); B64C 15/02 (2013.01); F02C 9/18 (2013.01); F02K 1/28 (2013.01); F02K 1/46 (2013.01); F02K 3/02 (2013.01); F05D 2220/323 (2013.01); F05D 2220/328 (2013.01); F05D 2220/90 (2013.01); F05D 2270/173 (2013.01);
Abstract
A gas turbine engine system is disclosed herein. The gas turbine engine system includes an engine core configured to discharge air through an exhaust nozzle along a central axis and a thrust director arranged near the exhaust nozzle and configured to redirect the discharge air by applying flow to the discharge air near the exhaust nozzle.