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. 21, 2023

Filed:

Feb. 21, 2020
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Dmitriy B. Sidelkovskiy, Ellington, CT (US);

Steven H. Zysman, Amston, CT (US);

Nathan L. Messersmith, South Windsor, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/06 (2006.01); F02K 1/09 (2006.01); F02K 1/12 (2006.01); F02K 3/075 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); F02K 1/09 (2013.01); F02K 1/1207 (2013.01); F02K 3/075 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2240/128 (2013.01); F05D 2250/323 (2013.01); F05D 2250/324 (2013.01);
Abstract

A nacelle assembly of a gas turbine engine includes an annular structure defining a central axis, and having a radially inward surface and a radially outward surface, the radially inward surface at least partially defining a bypass duct. An aft portion of the radially inward surface at least partially defines an axially extending convergent-divergent exit nozzle. A secondary nozzle flap is radially spaced from the aft portion of the radially inward surface. The secondary nozzle flap and the aft portion of the radially inward surface define a secondary bypass duct therebetween. The secondary nozzle flap is operably connected to the annular structure such that the secondary nozzle flap is selectably movable relative to the aft portion of the radially inward surface, thereby changing a cross-sectional area of a secondary bypass duct exit.


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