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. 21, 2022

Filed:

Sep. 02, 2020
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Jonathan Gilson, West Hartford, CT (US);

Constantine Baltas, Manchester, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/045 (2005.12); F02K 1/82 (2005.12); F02C 7/24 (2005.12); F01D 25/24 (2005.12); F02C 3/107 (2005.12);
U.S. Cl.
CPC ...
F02C 7/045 (2012.12); F01D 25/24 (2012.12); F02C 7/24 (2012.12); F02K 1/827 (2012.12); F02C 3/107 (2012.12); F05D 2240/40 (2012.12); F05D 2250/00 (2012.12); F05D 2250/283 (2012.12); F05D 2250/37 (2012.12); F05D 2260/963 (2012.12);
Abstract

A geared turbofan engine includes a first rotor, a fan, a second rotor, a gear train, a fan casing, a nacelle and a plurality of discrete acoustic liner segments. The fan is connected to the first rotor and is capable of rotation at frequencies between 200 and 6000 Hz and has a fan pressure ratio of between 1.25 and 1.60. The gear train connects the first rotor to the second rotor. The fan casing and nacelle are arranged circumferentially about a centerline and define a bypass flow duct in which the fan is disposed. The plurality of discrete acoustic liner segments with varied geometric properties are disposed along the bypass flow duct.


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