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:
Oct. 02, 2018

Filed:

Oct. 11, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Gregory A. Kohlenberg, Kensington, CT (US);

Sean P. Zamora, Conventry, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/09 (2006.01); F02K 1/00 (2006.01); F02K 1/82 (2006.01); F02K 1/18 (2006.01); F04D 29/32 (2006.01); B64D 27/16 (2006.01); F02C 7/36 (2006.01); F04D 29/38 (2006.01); F01D 5/06 (2006.01); F01D 25/24 (2006.01); F02K 3/06 (2006.01); F04D 29/52 (2006.01); F04D 29/56 (2006.01); B64D 31/00 (2006.01); F02K 1/72 (2006.01); F02K 1/30 (2006.01); B64D 33/04 (2006.01);
U.S. Cl.
CPC ...
F02K 1/18 (2013.01); B64D 27/16 (2013.01); B64D 31/00 (2013.01); B64D 33/04 (2013.01); F01D 5/06 (2013.01); F01D 25/24 (2013.01); F02C 7/36 (2013.01); F02K 1/30 (2013.01); F02K 1/72 (2013.01); F02K 3/06 (2013.01); F04D 29/321 (2013.01); F04D 29/325 (2013.01); F04D 29/38 (2013.01); F04D 29/522 (2013.01); F04D 29/563 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2230/50 (2013.01); F05D 2240/128 (2013.01); F05D 2260/40311 (2013.01); F05D 2270/3015 (2013.01);
Abstract

A turbofan engine according to an example of the present disclosure includes, among other things, a fan section including a plurality of fan blades, the plurality of fan blades having a fixed stagger angle and a design angle of incidence, a low pressure turbine driving the plurality of fan blades through a gear train, a fan nacelle and a core nacelle extending along an engine axis of rotation, the fan nacelle at least partially surrounding the core nacelle and the plurality of fan blades, a fan bypass flow path defined between the core nacelle and the fan nacelle, the core nacelle contoured along the fan bypass flow path with respect to the engine axis of rotation, and a fan variable area nozzle in communication with a controller and with the fan bypass flow path, and defining a fan nozzle exit area between the fan nacelle and the core nacelle.


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