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:
Dec. 19, 2017

Filed:

Mar. 13, 2014
Applicant:

Rolls-royce North American Technologies, Inc., Indianapolis, IN (US);

Inventors:

Kenneth M. Pesyna, Carmel, IN (US);

Anthony F. Pierluissi, Indianapolis, IN (US);

Bryan H. Lerg, Carmel, IN (US);

Justin N. Moore, Indianapolis, IN (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/077 (2006.01); F02K 1/12 (2006.01); F02K 1/15 (2006.01); F02K 3/075 (2006.01); F02K 3/115 (2006.01); F02K 1/80 (2006.01);
U.S. Cl.
CPC ...
F02K 1/1223 (2013.01); F02K 1/1207 (2013.01); F02K 1/1238 (2013.01); F02K 1/15 (2013.01); F02K 1/80 (2013.01); F02K 3/075 (2013.01); F02K 3/077 (2013.01); F02K 3/115 (2013.01); F05D 2250/411 (2013.01); F05D 2260/50 (2013.01); F05D 2260/56 (2013.01); F05D 2270/051 (2013.01); F05D 2270/66 (2013.01); Y02T 50/671 (2013.01);
Abstract

An exhaust nozzle for a gas turbine engine may include a plurality of flap trains in the exhaust stream of the gas turbine engine. The flap trains are operable to selectively control three separate flow paths of gas that traverse the engine. A first stream of is the core airflow. The second stream of air is peeled off of the first stream to form a low pressure fan bypass air stream. The third stream of air traverses along the engine casing and is passed over a flap assembly to aid in cooling. The flaps are operable converge/diverge to control the multiple streams of air.


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