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:
Feb. 04, 2020

Filed:

Aug. 22, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Michael Joseph Murphy, Windsor, CT (US);

Oleg Petrenko, Danbury, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/82 (2006.01); F01D 9/02 (2006.01); F02K 1/78 (2006.01); F01D 25/24 (2006.01); F02C 3/04 (2006.01); F02C 7/36 (2006.01); F02K 3/04 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 25/24 (2013.01); F02C 3/04 (2013.01); F02C 7/36 (2013.01); F02K 1/78 (2013.01); F02K 1/82 (2013.01); F02K 3/04 (2013.01); F05D 2220/36 (2013.01); F05D 2240/128 (2013.01); F05D 2240/24 (2013.01); F05D 2240/35 (2013.01); F05D 2260/40311 (2013.01);
Abstract

A turbofan engine includes a fan section. A core engine section drives the fan section. An outer nacelle surrounds the fan section and defines a radially outer surface of a fan duct. An inner nacelle surrounds the core engine section and defines a radially inner surface of the fan duct. A nozzle is disposed at a terminal end of the outer nacelle that defines an exit area for bypass air flow through the fan duct. The nozzle includes a convergent portion forward of a divergent portion and a turning angle for the divergent portion greater than about 12 degrees. A nacelle assembly and method are also disclosed.


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