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. 16, 2025

Filed:

May. 30, 2024
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Syed Khalid, Mason, OH (US);

David Marion Ostdiek, Liberty Township, OH (US);

Jeffrey S. Spruill, Hillsboro, OH (US);

Daniel Lawrence Tweedt, West Chester, OH (US);

William Joseph Solomon, Montgomery, OH (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Randy M. Vondrell, Newport, KY (US);

Kevin Edward Hinderliter, Cincinnati, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 5/145 (2013.01); F05D 2220/36 (2013.01); F05D 2250/51 (2013.01);
Abstract

A gas turbine engine is provided, comprising: a turbomachine having a compressor section, a combustion section, and a turbine section in serial flow order; and a fan section having a fan drivingly coupled to the turbomachine and an airflow surface rotatable with the fan and exposed to a fan airflow provided to and through the fan during operation of the gas turbine engine, the airflow surface defining a plurality of boundary layer openings configured to ingest a boundary layer of the fan airflow over the airflow surface during operation of the gas turbine engine.


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