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:
Mar. 17, 2026

Filed:

Jan. 12, 2024
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventor:

Michael G. Mccaffrey, Windsor, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/04 (2006.01); B64D 33/04 (2006.01); B64D 33/08 (2006.01); F02C 7/18 (2006.01); F02K 1/08 (2006.01); F02K 1/09 (2006.01); F02K 1/36 (2006.01); F02K 1/38 (2006.01); F02K 1/78 (2006.01); F02K 1/80 (2006.01); F02K 1/82 (2006.01); F23R 3/00 (2006.01); F23R 3/06 (2006.01); B64D 33/12 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); B64D 33/04 (2013.01); B64D 33/08 (2013.01); F02C 7/18 (2013.01); F02K 1/04 (2013.01); F02K 1/08 (2013.01); F02K 1/36 (2013.01); F02K 1/386 (2013.01); F02K 1/78 (2013.01); F02K 1/80 (2013.01); F02K 1/82 (2013.01); F02K 1/822 (2013.01); F02K 1/825 (2013.01); F23R 3/06 (2013.01); B64D 33/06 (2013.01); B64D 33/12 (2013.01); F02K 1/085 (2013.01); F02K 1/09 (2013.01); F02K 1/805 (2013.01); F05D 2260/20 (2013.01); F05D 2260/601 (2013.01); F23R 2900/03044 (2013.01);
Abstract

An apparatus is provided for an aircraft engine. This apparatus includes a variable area nozzle. The variable area nozzle includes a nozzle wall, a nozzle sleeve, an actuation system and a flowpath extending axially along an axis through the variable area nozzle and radially between the nozzle wall and the nozzle sleeve. The nozzle sleeve includes a shell, a liner, a cooling cavity and an ejector. The shell extends axially along and circumferentially about the axis. The liner axially overlaps and circumscribes the shell. The cooling cavity is formed by and radially between the shell and the liner. The ejector is arranged at a downstream end of the liner along the flowpath. The ejector fluidly couples the cooling cavity to the flowpath. The actuation system is configured to move the nozzle sleeve axially along the axis relative to the nozzle wall.


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