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. 17, 2026

Filed:

Jan. 31, 2025
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Brandon W. Miller, Evendale, OH (US);

Randy M. Vondrell, Evendale, OH (US);

David M. Ostdiek, Evendale, OH (US);

Craig W. Higgins, Evendale, OH (US);

Alexander Simpson, Evendale, OH (US);

Arthur W. Sibbach, Boxford, MA (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/065 (2006.01); F02C 3/06 (2006.01);
U.S. Cl.
CPC ...
F02K 3/065 (2013.01); F02C 3/06 (2013.01);
Abstract

A gas turbine engine includes a turbomachine defining an engine inlet to an inlet duct, a fan duct inlet to a fan duct, and a core inlet to a core duct; a primary fan driven by the turbomachine; a nacelle surrounding the primary fan; and a secondary fan located downstream of the primary fan within the inlet duct. The gas turbine engine is characterized by a thrust to power airflow ratio, a core bypass ratio, a blade effective acoustic length, an acoustic spacing length, and an inlet-to-nacelle ratio.


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