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:
Jul. 16, 2024

Filed:

Aug. 04, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nicholas J. Kray, Mason, OH (US);

David W. Crall, Loveland, OH (US);

Anthony L. DiPietro, Maineville, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Cincinnati, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 25/32 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 5/146 (2013.01); F02K 3/06 (2013.01); F01D 25/32 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2240/30 (2013.01);
Abstract

A fan for a turbine engine having a core air flowpath and a bypass air flowpath. The fan includes a disk, a plurality of fan blades, and a plurality of splitter blades. The disk rotates about a centerline axis. The plurality of fan blades are coupled to the disk. The plurality of splitter blades are coupled to the disk and positioned between the plurality of fan blades. The plurality of splitter blades are axially aligned on the disk at a splitter blade axial distance from an annular inlet of the core air flowpath such that the plurality of splitter blades direct debris that passes through the fan into the bypass air flowpath.


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