IP Library › Granted Patent US 12,500,473
Granted Patent B2
US 12,500,473 · App. 17/775,237 · Granted Dec 16, 2025

Axial flux motor with cooling jacket

Inventors: Mikhail Goykhman (Reseda, CA); Galen Chui (Ladera Ranch, CA); Piranavan Suntharalingam (Menomonee, WI); Robert Anson Lau (Hamilton, CA); Ehab Mohammed Mahmoud Sayed (Hamilton, CA); Alan Dorneles Callegaro (Hamilton, CA); Federico Duperly (Georgetown, CA); Mohamed Elsayed Abdallah Abdalmagid (Hamilton, CA)
Assignee: EATON INTELLIGENT POWER LIMITED
H02K5/203H02K1/141H02K1/16H02K1/27H02K5/04H02K7/003H02K9/16H02K9/193H02K16/02H02K21/24
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Quick Facts
Patent No.
US 12,500,473
App. No.
17/775,237
Granted
Dec 16, 2025
Kind
B2
Abstract

The present disclosure relates to an axial flux motor comprising a stator assembly and a rotor assembly. The axial flux motor also includes a cooling jacket including fins that extend between electromagnets of the stator assembly. The axial flux motor rotor assembly also includes an air cooling arrangement to provide air cooling to the stator assembly. The axial flux motor also includes stator cores having enlarged end plates.

Claims (39)

1 . A cooling jacket for an axial flux motor, the cooling jacket comprising:

a) a first housing part defining a circumferential internal cooling passageway through which a cooling fluid can be circulated between an inlet port and an outlet port, the first housing part having a circumferential inner wall surface and a circumferential outer wall surface, wherein the circumferential internal cooling passageway includes a plurality of internal ribs dividing the circumferential internal cooling passageway into a plurality of circumferential passageways, wherein a length of each rib extends circumferentially within the circumferential internal cooling passageway.

2 . The cooling jacket of claim 1 , wherein the plurality of internal ribs extend at an oblique angle to a longitudinal axis of the first housing part.

3 . The cooling jacket of claim 1 , wherein the plurality of internal ribs are parallel to each other along at least part of a total length of the internal ribs.

4 . The cooling jacket of claim 1 , further including an internal dividing rib within the circumferential internal cooling passageway, the internal dividing rib dividing the circumferential internal cooling passageway into an inlet end proximate the inlet port and an outlet end proximate the outlet port.

5 . The cooling jacket of claim 1 , wherein the cooling jacket is located within the axial flux motor, the axial flux motor comprising:

a) a housing assembly arranged along a housing longitudinal axis and including the first housing part;

b) a stator assembly mounted within the housing assembly and in contact with the first housing part such that a thermally conductive pathway between the circumferential internal cooling passageway and the stator assembly is formed; and

c) a rotor assembly mounted within the housing assembly, the rotor assembly being rotatable with respect to the stator assembly and including an output shaft extending out of the housing assembly.

6 . The cooling jacket of claim 5 , wherein the plurality of circumferential passageways are substantially parallel to each other.

7 . The cooling jacket of claim 6 , wherein the plurality of internal ribs extend at an oblique angle to the housing longitudinal axis.

8 . The cooling jacket of claim 6 , wherein the plurality of internal ribs are parallel to each other along at least part of a total length of the internal ribs.

9 . The cooling jacket of claim 6 , wherein the plurality of internal ribs include bend portions proximate the inlet and outlet ports to direct fluid flow from and towards the inlet and outlet ports.

10 . The cooling jacket of claim 5 , wherein the inlet and outlet ports extend through an outer circumferential wall of the first housing part.

11 . The cooling jacket of claim 5 , wherein the inlet and outlet ports extend through axial ends of an outer circumferential wall of the first housing part.

12 . The cooling jacket of claim 5 , wherein the inlet and outlet ports are aligned along a common axis that is parallel to a longitudinal axis of the first housing part.

13 . A cooling jacket for an axial flux motor, the cooling jacket comprising:

a) a first housing part defining a circumferential internal cooling passageway through which a cooling fluid can be circulated between an inlet port and an outlet port, the first housing part having a circumferential inner wall surface and a circumferential outer wall surface, wherein the circumferential internal cooling passageway includes a plurality of internal ribs dividing the circumferential internal cooling passageway into a plurality of circumferential passageways;

wherein the first housing part includes a plurality of cooling fins extending radially inward from an inner circumferential wall of the first housing part towards a longitudinal axis of the first housing part, wherein the plurality of cooling fins each define a base portion and a distal portion, the distal portion having a narrower dimension than the base portion.

14 . The cooling jacket of claim 13 , wherein the plurality of cooling fins are integrally formed with the first housing part.

15 . The cooling jacket of claim 13 , wherein the circumferential internal cooling passageway extends into the plurality of cooling fins.

16 . A cooling jacket for an axial flux motor, the cooling jacket comprising:

a) a first housing part defining a circumferential internal cooling passageway through which a cooling fluid can be circulated between an inlet port and an outlet port, the first housing part having a circumferential inner wall surface and a circumferential outer wall surface, wherein the circumferential internal cooling passageway includes a plurality of internal ribs dividing the circumferential internal cooling passageway into a plurality of circumferential passageways;

wherein the plurality of internal ribs include bend portions proximate the inlet and outlet ports to direct fluid flow from and towards the inlet and outlet ports.

17 . A cooling jacket for an axial flux motor, the cooling jacket comprising:

a) a first housing part defining a circumferential internal cooling passageway through which a cooling fluid can be circulated between an inlet port and an outlet port, the first housing part having a circumferential inner wall surface and a circumferential outer wall surface, wherein the circumferential internal cooling passageway includes a plurality of internal ribs dividing the circumferential internal cooling passageway into a plurality of circumferential passageways;

wherein the cooling jacket is located within the axial flux motor, the axial flux motor comprising:

a) a housing assembly arranged along a housing longitudinal axis and including the first housing part;

b) a stator assembly mounted within the housing assembly and in contact with the first housing part such that a thermally conductive pathway between the circumferential internal cooling passageway and the stator assembly is formed; and

c) a rotor assembly mounted within the housing assembly, the rotor assembly being rotatable with respect to the stator assembly and including an output shaft extending out of the housing assembly

wherein the first housing part includes a plurality of cooling fins extending radially inward from the circumferential inner wall surface of the first housing part towards a longitudinal axis of the first housing part and at least partially into spaces defined between stator cores of the stator assembly.

18 . The cooling jacket of claim 17 , wherein the plurality of cooling fins are integrally formed with the first housing part.

19 . The cooling jacket of claim 18 , wherein the circumferential internal cooling passageway extends into the plurality of cooling fins.

20 . A cooling jacket for an axial flux motor, the cooling jacket comprising:

a) a first housing part defining a circumferential internal cooling passageway through which a cooling fluid can be circulated between an inlet port and an outlet port, the first housing part having a circumferential inner wall surface and a circumferential outer wall surface, wherein the circumferential internal cooling passageway includes a plurality of internal ribs dividing the circumferential internal cooling passageway into a plurality of circumferential passageways;

wherein the cooling jacket is located within the axial flux motor, the axial flux motor comprising:

a) a housing assembly arranged along a housing longitudinal axis and including the first housing part;

b) a stator assembly mounted within the housing assembly and in contact with the first housing part such that a thermally conductive pathway between the circumferential internal cooling passageway and the stator assembly is formed; and

wherein the housing assembly further comprises an internal dividing rib within the circumferential internal cooling passageway, the internal dividing rib dividing the circumferential internal cooling passageway into an inlet end proximate the inlet port and an outlet end proximate the outlet port.

Assignments (7)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2025
From: LAU, ROBERT ANSON; SAYED, EHAB MOHAMMED MAHMOUD; CALLEGARO, ALAN DORNELES; DUPERLY, FEDERICO; ABDALMAGID, MOHAMED ELSAYED ABDALLAH
To: MCMASTER UNIVERSITY
Reel/Frame 070062/0555 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2025
From: CHUI, GALEN
To: EATON INTELLIGENT POWER LIMITED
Reel/Frame 070061/0962 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2025
From: GOYKHMAN, MIKHAIL
To: EATON INTELLIGENT POWER LIMITED
Reel/Frame 070062/0011 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2025
From: SUNTHARALINGAM, PIRANAVAN
To: EATON INTELLIGENT POWER LIMITED
Reel/Frame 070061/0816 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2025
From: MCMASTER UNIVERSITY
To: EATON INTELLIGENT POWER LIMITED
Reel/Frame 070062/0647 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064423/0966 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Sep 28, 2022
From: AEROJET ROCKETDYNE, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 061561/0451 →
Continuity (4)
Provisional Application 62931702 · Nov 6, 2019
Provisional Application 62931707 · Nov 6, 2019
Provisional Application 62931712 · Nov 6, 2019
Related Publication 20220393543A1 · Dec 8, 2022
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