Integrated electric motor and thermal management system

Patent metadata

Field	Value
Publication number	US-12494699-B2
Application number	US-202117800685-A
Country	US
Kind code	B2
Filing date	Feb 19, 2021
Priority date	Feb 21, 2020
Publication date	Dec 9, 2025
Grant date	Dec 9, 2025

Abstract

A compact electric motor assembly unit includes an electric motor and an integrated thermal management system. A heat exchanger may be mounted directly to the electric motor and/or form part of the motor housing. A coolant pump may be mounted directly to the electric motor. The coolant pump may be connected either to a drive shaft of the electric motor or to a gear train disposed inside of the electric motor. In certain cases, the coolant pathways for the thermal management system are all located internal of the electric motor assembly unit.

First claim

What is claimed is:

1 . An electric motor assembly unit comprising:
a) an electric motor extending a first distance along a longitudinal axis between a first axial end and a second axial end, the electric motor including a stator assembly, a rotor assembly that rotates relative to the stator assembly, and a motor shaft operationally coupled to the rotor assembly, the motor shaft extending along the longitudinal axis of the electric motor beyond the first axial end; and b) a heat exchanger mounted to the electric motor so as to be disposed between the first and second axial ends of the electric motor and structurally supported by the electric motor, the heat exchanger including an exchanger housing and a coolant pathway routed within the exchanger housing, the exchanger housing extending radially outwardly from the electric motor so that the electric motor assembly unit has a cross-dimension that is larger than the first distance, the cross-dimension extending orthogonal to the first distance.

2 . The electric motor assembly of claim 1 , wherein the heat exchanger encircles the stator assembly about the longitudinal axis of the electric motor.

3 . The electric motor assembly of claim 1 , wherein the heat exchanger extends only a portion of a circumference of the stator assembly.

4 . The electric motor assembly of claim 1 , wherein the coolant pathway within the heat exchanger is a first coolant pathway, and wherein the first coolant pathway is fluidly coupled to a second coolant pathway within the electric motor.

5 . The electric motor assembly of claim 4 , wherein the second coolant pathway includes channels extending through a cooling jacket that surrounds the rotor assembly and the stator assembly.

6 . The electric motor assembly of claim 4 , wherein the second coolant pathway includes channels extending through portions of stator cores of the stator assembly.

7 . The electric motor assembly of claim 4 , wherein the second coolant pathway extends to a coolant pump mounted to the electric motor.

8 . The electric motor assembly of claim 7 , wherein the coolant pump is mounted to the motor shaft.

9 . The electric motor assembly of claim 7 , wherein the coolant pump is at least partially recessed into a motor housing that covers the rotor assembly.

10 . The electric motor assembly of claim 1 , further comprising an epicyclic gear train disposed within the electric motor so that the epicyclic gear train is enclosed within the stator assembly and rotor assembly, wherein the epicyclic gear train includes a sun gear, a carrier coupled to a plurality of planet gears that mesh with the sun gear, and an outer ring having inwardly-facing teeth that mesh with the planet gears, wherein at least one of the sun gear, the carrier, and the outer ring rotates in unison with the motor shaft.

11 . The electric motor assembly of claim 10 , further comprising a third coolant pathway providing coolant to the epicyclic gear train, the third coolant pathway being fluidly coupled to the coolant pathway extending through the exchanger housing.

12 . The electric motor assembly of claim 11 , further comprising a coolant pump mounted to the electric motor, the coolant pump being coupled to a first gear stage of the epicyclic gear train that rotates at a different speed from the motor shaft.

13 . The electric motor assembly of claim 12 , wherein the coolant pump is mounted to the motor shaft.

14 . The electric motor assembly of claim 1 , further comprising an electric drive disposed at an outer surface of the stator assembly, wherein the coolant pathway is fluidly coupled to a respective coolant pathway for the electric drive.

15 . An aircraft propulsion system comprising:
a) a propeller operationally coupled to a drive shaft extending along a longitudinal axis; b) an electric motor including a rotor assembly that rotates relative to a stator assembly to rotate the drive shaft; c) a heat exchanger mounted to the electric motor so that the heat exchanger extends radially outwardly from the electric motor, the heat exchanger extending along the longitudinal axis between opposite first and second axial ends; d) a flow path along which air flow generated by the propeller flows to the first axial end of the heat exchanger; and e) a nacelle surrounding a portion of the drive shaft, the nacelle being spaced from the propeller along the longitudinal axis of the drive shaft, the electric motor and the heat exchanger being located within the nacelle, wherein the flow path includes a first flow path extending into the nacelle and a second flow path extending around the nacelle, the first flow path extending to the first axial end of the heat exchanger.

16 . The aircraft propulsion system of claim 15 , wherein the electric motor is one of a plurality of electric motors applying torque to the drive shaft, each of the electric motors being aligned along the longitudinal axis and being operationally coupled to the drive shaft; and wherein the heat exchanger is one of a plurality of heat exchangers, each of the heat exchangers being mounted to a respective one of the electric motors.

17 . The aircraft propulsion system of claim 16 , wherein each of the heat exchangers extends radially outwardly from a circumferential section of the respective electric motor, wherein the heat exchangers are circumferentially staggered so that a respective first axial end of each of the heat exchangers is accessible to the flow path.

18 . The aircraft propulsion system of claim 15 , wherein the heat exchanger and the electric motor share a coolant pathway.

19 . The aircraft propulsion system of claim 15 , further comprising an epicyclic gear train disposed within the electric motor, the electric motor sharing a coolant pathway with the epicyclic gear train.

20 . An aircraft propulsion system comprising:
a) a propeller operationally coupled to a drive shaft extending along a longitudinal axis; b) an electric motor including a rotor assembly that rotates relative to a stator assembly to rotate the drive shaft, wherein the electric motor is one of a plurality of electric motors applying torque to the drive shaft, each of the electric motors being aligned along the longitudinal axis and being operationally coupled to the drive shaft; c) a heat exchanger mounted to the electric motor so that the heat exchanger extends radially outwardly from the electric motor, the heat exchanger extending along the longitudinal axis between opposite first and second axial ends, wherein the heat exchanger is one of a plurality of heat exchangers, each of the heat exchangers being mounted to a respective one of the electric motors; and d) a flow path along which air flow generated by the propeller flows to the first axial end of the heat exchanger.

21 . The aircraft propulsion system of claim 20 , wherein each of the heat exchangers extends radially outwardly from a circumferential section of the respective electric motor, wherein the heat exchangers are circumferentially staggered so that a respective first axial end of each of the heat exchangers is accessible to the flow path.

Assignees

• Eaton Intelligent Power Ltd

Inventors

• Goykhman Mikhail
• Chui Galen
• Baronian Armen

Classifications

• B64D35/08

  characterised by the transmission being driven by a plurality of power plants (for hybrid-electric power plants B64D35/022) · CPC title

• B64D35/024

  of series type · CPC title

• H02K21/24

  with magnets axially facing the armatures, e.g. hub-type cycle dynamos · CPC title

• H02K9/193

  with provision for replenishing the cooling medium; with means for preventing leakage of the cooling medium · CPC title

• H02K7/116

  with gears · CPC title