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:
Jan. 17, 2023

Filed:

Aug. 20, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Anthony R. Bifulco, Ellington, CT (US);

David A. Topol, West Hartford, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); F01D 25/24 (2006.01); F01D 9/06 (2006.01);
U.S. Cl.
CPC ...
F01D 25/28 (2013.01); F01D 9/06 (2013.01); F01D 25/24 (2013.01); F05D 2240/14 (2013.01); F05D 2250/191 (2013.01); F05D 2260/30 (2013.01); F05D 2260/606 (2013.01); F05D 2260/96 (2013.01);
Abstract

A gear reduction reduces a speed of a fan rotor relative to a speed of a fan drive turbine. A fan case surrounds the fan rotor. A core engine has a compressor section and includes a low pressure compressor. The fan rotor delivers air into a bypass duct defined between the fan case and the core engine. A rigid connection between the fan case and the core engine includes a plurality of aft connecting members rigidly connected to the fan case, and to the core engine. A plurality of fan exit guide vanes are rigidly connected to the fan case, with the fan exit guide vanes including structural fan exit guide vanes which are rigidly connected to the core engine, and non-structural fan exit guide vanes, and the non-structural fan exit guide vanes being provided with an acoustic feature to reduce noise.


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