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:
Sep. 03, 2019

Filed:

Mar. 21, 2016
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Lee Drozdenko, Bristol, CT (US);

William R. Graves, Amston, CT (US);

Michael Li, Madison, CT (US);

Maria C. Kirejczyk, Middletown, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/12 (2006.01); F04D 29/34 (2006.01); F01D 5/30 (2006.01); F04D 29/32 (2006.01); F02C 3/04 (2006.01); F02K 3/06 (2006.01); F04D 29/38 (2006.01); F01D 21/04 (2006.01);
U.S. Cl.
CPC ...
F04D 29/34 (2013.01); F01D 5/30 (2013.01); F01D 21/045 (2013.01); F02C 3/04 (2013.01); F02K 3/06 (2013.01); F04D 29/322 (2013.01); F04D 29/38 (2013.01); F01D 5/3007 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2230/10 (2013.01); F05D 2240/35 (2013.01); F05D 2250/241 (2013.01); F05D 2250/291 (2013.01); F05D 2250/294 (2013.01); F05D 2260/941 (2013.01);
Abstract

A fan blade is provided and comprises a leading edge, an attachment root extending aft of the leading edge, and a trench formed in a surface of the attachment root. An attachment root is also provided. The attachment root comprises a leading edge, a dovetail extending aft of the leading edge, and a trench formed in a surface of the dovetail. A gas turbine engine is also provided. The gas turbine engine comprises a compressor section configured to rotate about an axis, a combustor aft of the compressor section, and a turbine section aft of the compressor section and configured to rotate about the axis. A fan may be disposed forward of the turbine section and include a blade. The blade may have a trench formed in an attachment root.


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