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. 03, 2019

Filed:

May. 07, 2013
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

David Lynn Dawson, Liberty Township, OH (US);

Erin Lee Lariviere, Milford, OH (US);

Brian Joseph Petersen, Mason, OH (US);

Robert Jerome Ellerhorst, Cincinnati, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/077 (2006.01); F02K 3/12 (2006.01); F02K 3/02 (2006.01); F02K 3/075 (2006.01); F02K 1/12 (2006.01); F02K 1/82 (2006.01);
U.S. Cl.
CPC ...
F02K 3/077 (2013.01); F02K 1/1292 (2013.01); F02K 1/822 (2013.01); F02K 3/025 (2013.01); F02K 3/075 (2013.01); Y02T 50/672 (2013.01); Y02T 50/675 (2013.01);
Abstract

A third stream duct producing a third air stream at reduced pressure that is exhausted through a separate nozzle that is concentric with the main or primary engine nozzle. The third stream exhaust air from the separate concentric nozzle is exhausted to a location at which pressure is ambient or sub-ambient. The location at which the third stream air is exhausted contributes to the thrust of the aircraft. The airstream from the third air duct is exhausted through an exhaust nozzle of the third duct that is positioned at the interface between the aft of the airframe and the leading edge of the engine outer flaps. This location is a low pressure region that has a recirculation zone. The exhaust of third stream air to this low pressure region substantially reduces or eliminates this recirculation zone and associated boat tail drag, thereby improving the efficiency of the engine.


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