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:
Nov. 28, 2023

Filed:

Oct. 04, 2021
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Maruthi Manohar Jupudi, Dubai, AE;

Paul Mathew, Karnataka, IN;

Jose Antonio Cuevas Alvarez, Aargau, CH;

Bouria Mohamed Faqihi, Dubai, AE;

Deoras Prabhudharwadkar, Bangalore, IN;

Murali Krishna Kalaga, Salmiya, KW;

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B01D 46/00 (2022.01); F02C 7/055 (2006.01); B01D 50/20 (2022.01); B01D 45/04 (2006.01); B01D 45/08 (2006.01); F02C 7/052 (2006.01);
U.S. Cl.
CPC ...
F02C 7/055 (2013.01); B01D 45/04 (2013.01); B01D 45/08 (2013.01); B01D 46/003 (2013.01); B01D 50/20 (2022.01); F02C 7/052 (2013.01);
Abstract

Mitigating particulate intrusion to an air intake system of a gas turbine system with intrusion protective coatings tailored to locale of operation. A particulate intrusion protective coating is applied to a surface of a component of the air intake system to mitigate ingress of particulates within the air intake system and the gas turbine system. The particulate intrusion protective coating includes one or more particulate ingress influencing properties tailored to the common attributes of the particulates associated with the locale of operation of the gas turbine engine and the air intake system. The particulate ingress influencing properties affect rebounding and coalescing characteristics of the particulates at a point of impact with the applied surface having the particulate intrusion protective coating, entraining the particulates at the point of impact and inhibiting further ingress along an inlet air flow path of the air intake system into the gas turbine engine.


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