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:
Mar. 29, 2022

Filed:

Jun. 03, 2020
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Nick Nolcheff, Chandler, AZ (US);

John Repp, Gilbert, AZ (US);

Bruce Reynolds, Chandler, AZ (US);

John Gunaraj, Chandler, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F01D 5/02 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F01D 5/02 (2013.01); F01D 5/30 (2013.01); F02C 7/36 (2013.01); F05D 2220/32 (2013.01); F05D 2240/24 (2013.01); F05D 2240/60 (2013.01);
Abstract

A rotor for a turbofan booster section associated with a fan section of a gas turbine engine includes a rotor blade having an airfoil extending from a root to a tip and having a leading edge and a trailing edge. The airfoil has a plurality of chord lines spaced apart in a spanwise direction. Each chord line of the plurality of chords lines is defined between the leading edge and the trailing edge and has a normalized chord value. From the hub, the normalized chord value decreases to a minimum value between about 20% to about 90% span and increases from the minimum value to the tip. The rotor includes a rotor disk coupled to the rotor blade configured to be coupled to the shaft or the fan to rotate with the shaft or the fan, respectively, at the same speed as the shaft and fan.


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