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:
Jan. 12, 2021

Filed:

Oct. 29, 2019
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

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

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

Joseph C. Straccia, Middletown, CT (US);

Stanley J. Balamucki, The Villages, FL (US);

Mark A. Stephens, Wethersfield, CT (US);

Kate Hudon, Superior, CO (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/54 (2006.01); F04D 29/32 (2006.01); F01D 5/14 (2006.01); F02K 3/072 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F04D 29/544 (2013.01); F01D 5/141 (2013.01); F02C 7/36 (2013.01); F02K 3/072 (2013.01); F04D 29/324 (2013.01); F05D 2220/3217 (2013.01); F05D 2240/122 (2013.01); F05D 2240/304 (2013.01); F05D 2260/40311 (2013.01); Y02T 50/60 (2013.01);
Abstract

A compressor airfoil of a turbine engine that has a geared architecture includes pressure and suction sides and extends in a radial direction from a 0% span position to a 100% span position. The airfoil has a relationship between a trailing edge angle and span position that defines a curve with a non-negative slope from 0% span to 20% span corresponding to a non-decreasing trailing edge angle.


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