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:
Jan. 02, 2024

Filed:

May. 27, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Joseph G. Rose, Evendale, OH (US);

Atanu Saha, Bengaluru, IN;

Bhaskar Nanda Mondal, Bengaluru, IN;

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

Darek Zatorski, Evendale, OH (US);

Vaibhav Deshmukh M, Bengaluru, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01); F02C 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F02C 3/06 (2013.01); F05D 2240/52 (2013.01); F05D 2260/15 (2013.01); F05D 2260/213 (2013.01); F05D 2260/232 (2013.01); F05D 2260/605 (2013.01); F05D 2260/607 (2013.01);
Abstract

A turbine engine having a drive shaft rotatable about an axis, a multi-stage compressor, a turbine section, a thrust bearing, and a balance cavity. The thrust bearing being provided between the drive shaft and at least a portion of the multi-stage compressor section and rotationally supporting the drive shaft. During operation of the turbine engine, a first axial force is applied to the thrust bearing by the drive shaft and a second axial force is applied to the thrust bearing in an opposite direction of the first axial force by the balance cavity.


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