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:
Aug. 25, 2026

Filed:

Mar. 27, 2024
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Ramesh Balla, Bengaluru, IN;

Bhaskar Nanda Mondal, Bangalore, IN;

Thomas O. Moniz, Mason, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/06 (2006.01); F02C 7/06 (2006.01);
U.S. Cl.
CPC ...
F02C 3/06 (2013.01); F02C 7/06 (2013.01);
Abstract

Structures for achieving high bypass ratio in gas turbine engines are described. A gas turbine engine includes a compressor section, a combustion section, a turbine section, and an exhaust section. The compressor section includes a first booster, a second booster, and a blisk including an inclined web and offset bore. An angle of inclination relative to a vertical plane is between 5° and 55°. The vertical plane is perpendicular to an axial direction that is parallel to a longitudinal centerline defined by the gas turbine engine. The turbine section includes a first turbine and a second turbine.


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