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:
Oct. 20, 2020

Filed:

Jul. 25, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Taryn Narrow, Glastonbury, CT (US);

Matthew E. Bintz, West Hartford, CT (US);

Lucas D. Sorensen, Middletown, CT (US);

Daniel J. Monahan, Cromwell, CT (US);

Steven D. Roberts, Moodus, CT (US);

Jordan T. Wall, Middletown, CT (US);

Yuan Dong, Glastonbury, CT (US);

Lisa I. Brilliant, Middletown, CT (US);

Andrew J. Murphy, Old Saybrook, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F04D 29/52 (2006.01); F01D 11/12 (2006.01); F01D 5/02 (2006.01); F01D 5/12 (2006.01); F01D 5/20 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F01D 5/143 (2013.01); F01D 5/025 (2013.01); F01D 5/12 (2013.01); F01D 5/20 (2013.01); F01D 11/12 (2013.01); F01D 11/122 (2013.01); F02C 3/04 (2013.01); F04D 29/526 (2013.01); F05D 2220/32 (2013.01); F05D 2240/303 (2013.01); F05D 2240/304 (2013.01); F05D 2240/307 (2013.01); F05D 2250/314 (2013.01);
Abstract

A rotor blade for a gas turbine engine includes a blade extending from a root and a contoured tip portion at a first end of the blade. The first end is opposite the root. The contoured tip portion includes a first sloped region and a second sloped region. The second sloped region is steeper than the first sloped region, relative to a platform.


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