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:
Feb. 04, 2020

Filed:

Mar. 16, 2017
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:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F02K 3/06 (2006.01); F04D 29/38 (2006.01); F02C 3/04 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F04D 29/384 (2013.01); F01D 5/141 (2013.01); F02C 3/04 (2013.01); F02K 3/06 (2013.01); F04D 29/325 (2013.01); F04D 29/388 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2240/301 (2013.01); F05D 2240/303 (2013.01); F05D 2240/35 (2013.01); F05D 2300/603 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01);
Abstract

A gas turbine engine includes a combustion section arranged between a compressor section and a turbine section that extend in an axial direction. A fan section is arranged upstream from the compressor section. An airfoil is arranged in one of the fan section, the compressor section and the turbine section. The airfoil includes 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 leading edge that is projected onto a plane from various views and the plane is perpendicular to a viewing direction which corresponds to the various views. The plane is parallel with the axial direction in a 0° view. The various views include the 0° view which projects into an axial plane in the axial direction. A 90° view projects into a tangential plane in a tangential direction normal to the axial direction and views between the 0° and 90° views. The airfoil has a maximum leading edge projection in a 20° to° view. The radial direction is normal to the axial and tangential directions.


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