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. 21, 2025

Filed:

Jan. 28, 2022
Applicant:

GE Aviation Systems Llc, Grand Rapids, MI (US);

Inventors:

Balamurugan Sridharan, Bangalore, IN;

Anirban Chatterjee, Bangalore, IN;

Ami Hatim, Bangalore, IN;

Assignee:

GE AVIATION SYSTEMS LLC, Grand Rapids, MI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02K 1/32 (2006.01); H02K 1/24 (2006.01); H02K 1/26 (2006.01); H02K 3/24 (2006.01); H02K 9/19 (2006.01); H02K 19/16 (2006.01);
U.S. Cl.
CPC ...
H02K 1/32 (2013.01); H02K 1/24 (2013.01); H02K 3/24 (2013.01); H02K 9/19 (2013.01); H02K 19/16 (2013.01); H02K 1/26 (2013.01);
Abstract

A method of cooling a set of rotor winding end turns of a rotor assembly can include directing a fluid coolant flow to a coil support assembly, delivering the fluid coolant flow, by a first coolant distribution ring of the coil support assembly, radially outward toward rotor winding end turns; and delivering the fluid coolant flow, by a coil support disc of the coil support assembly, axially outward toward the rotor winding end turns. The method can further include expelling fluid coolant flow by a second coolant distribution ring radially outward toward a set of stator windings, and expelling, by the coil support disc, the fluid coolant flow axially outward toward the rotor core.


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