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. 06, 2020

Filed:

Jul. 30, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Edward J. Gallagher, West Hartford, CT (US);

Byron R. Monzon, Cromwell, CT (US);

Ling Liu, Glastonbury, CT (US);

Linda S. Li, Middlefield, CT (US);

Darryl Whitlow, Middletown, CT (US);

Barry M. Ford, Middletown, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 5/02 (2006.01); F01D 15/12 (2006.01); F02C 3/14 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F01D 5/141 (2013.01); F01D 5/02 (2013.01); F01D 15/12 (2013.01); F02C 3/04 (2013.01); F02C 3/14 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2250/71 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01);
Abstract

An airfoil for a turbine engine includes an airfoil having pressure and suction sides extending in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a curve corresponding to a relationship between a trailing edge sweep angle and a span position. The trailing edge sweep angle is in a range of 0° to 10° in a range of 10-20% span position. The trailing edge sweep angle is in a range of the trailing edge sweep angle is positive from 0% span to at least 95% span.


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