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:
Dec. 29, 2020

Filed:

Nov. 07, 2018
Applicant:

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

Inventors:

Nick Nolcheff, Chandler, AZ (US);

John Repp, Gilbert, AZ (US);

John A. Gunaraj, Chandler, AZ (US);

Yoseph Gebre-Giorgis, Phoenix, AZ (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/10 (2006.01); B23P 15/04 (2006.01); F01D 5/16 (2006.01);
U.S. Cl.
CPC ...
F01D 5/10 (2013.01); B23P 15/04 (2013.01); F01D 5/16 (2013.01); B23P 2700/01 (2013.01); B23P 2700/50 (2013.01); F05D 2260/961 (2013.01);
Abstract

A rotor includes a plurality of airfoils and each airfoil has a span that extends from 0% at a root to 100% at a tip, a chord that extends from 0% at a leading edge to 100% at a trailing edge and a pressure side opposite a suction side. The pressure side of each airfoil has a pressure side surface shape and the suction side of each airfoil has a suction side surface shape based on an operating state of the rotor. Each airfoil has the same suction side surface shape between 10% and 90% of the chord and between 80% and 100% of the span at a first state. At least one first airfoil has a different suction side surface shape between 10% and 90% of the chord and between 80% and 100% of the span than at least one second airfoil at a static state of the rotor.


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