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:
Jun. 15, 2021

Filed:

Jan. 25, 2018
Applicant:

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

Inventors:

Parmeet Singh Chhabra, Bangalore, IN;

David Raju Yamarthi, Bangalore, IN;

Navin Soni, Bangalore, IN;

Mamatha Ramakrishnaiah, Bangalore, IN;

Balamurugan Sridharan, Bangalore, IN;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02K 3/12 (2006.01); H02K 3/487 (2006.01); H02K 1/26 (2006.01); H02K 7/08 (2006.01); H02K 15/00 (2006.01); H02K 7/20 (2006.01); H02K 9/19 (2006.01); H02K 15/02 (2006.01); H02K 15/09 (2006.01); H02K 7/18 (2006.01); H02K 3/51 (2006.01); H02K 1/32 (2006.01);
U.S. Cl.
CPC ...
H02K 3/487 (2013.01); H02K 1/26 (2013.01); H02K 3/12 (2013.01); H02K 3/51 (2013.01); H02K 7/083 (2013.01); H02K 7/1823 (2013.01); H02K 7/20 (2013.01); H02K 9/19 (2013.01); H02K 15/0018 (2013.01); H02K 15/024 (2013.01); H02K 15/09 (2013.01); H02K 1/32 (2013.01);
Abstract

A rotor assembly includes a rotor core having winding slots, and one or more coils, which have slot-inserted segments included in the winding slots, and first and second end-turn segments external to the winding slots and located around opposite axial ends of the rotor core, respectively. The rotor assembly further includes a first containment band located around at least a portion of the first end-turn segments and configured to prevent the first end-turn segments from moving away from the rotor core radially, a second containment band located around at least a portion of the second end-turn segments and configured to prevent the second end-turn segments from moving away from the rotor core radially, and one or more sticks mounted in one or more of the winding slots, respectively. The first and second containment bands are retained via the sticks against moving away axially.


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