IP Library › Granted Patent US 12,194,827
Granted Patent B2
US 12,194,827 · App. 17/859,239 · Granted Jan 14, 2025

Integrated electrified propulsion system for a vehicle

Inventors: Joel S. Hooton (Chesterfield, MI); Brian V. Castillo (Birmingham, MI); Joseph D. Kliewer (Bloomfield Hills, MI); Alan G. Holmes (Clarkston, MI)
Assignee: GM Global Technology Operations LLC
B60K1/04B60K11/04B60K17/28B60L1/003B60L53/20F16H57/021F16H57/0415B60K2001/005B60K2001/006F16H2057/02034F16H2057/02043
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Quick Facts
Patent No.
US 12,194,827
App. No.
17/859,239
Granted
Jan 14, 2025
Kind
B2
Abstract

An integrated electrified propulsion system for a vehicle includes a single electric machine, a mechanical geartrain, a rechargeable energy storage device, an integrated cooling system, and a power electronics system. The single electric machine, the mechanical geartrain, the integrated cooling system, the rechargeable energy storage device, and the power electronics system are arranged in a single housing. The single electric machine is rotatably coupled to the mechanical geartrain to transfer mechanical power therebetween.

Claims (49)

1. An integrated electrified propulsion system for a vehicle, comprising:

a single electric machine; a mechanical geartrain; a rechargeable energy storage device;

an integrated cooling system; and a power electronics system;

wherein the single electric machine, the mechanical geartrain, the integrated cooling system, the rechargeable energy storage device, and the power electronics system are arranged in a single housing;

wherein the single electric machine is rotatably coupled to the mechanical geartrain to transfer mechanical power therebetween; and

wherein the mechanical geartrain comprises a torque transmission device coupled to a plurality of power takeoff couplers via a plurality of shaft members.

2. The integrated electrified propulsion system of claim 1 :

wherein the plurality of shaft members includes a first shaft member and a second shaft member;

wherein the first and second shaft members are arranged perpendicular to a longitudinal axis of the single housing;

wherein a first of the plurality of power takeoff couplers is arranged on a first side of the single housing and is rotatably coupled to the first shaft member; and

wherein a second of the plurality of power takeoff couplers is arranged on a second side of the single housing that is opposite to the first side perpendicular to the longitudinal axis, and is rotatably coupled to the second shaft member.

3. The integrated electrified propulsion system of claim 1 :

wherein the plurality of shaft members includes a first shaft member and a second shaft member;

wherein the first and second shaft members are arranged parallel to a longitudinal axis of the single housing;

wherein a first of the plurality of power takeoff couplers is arranged on a first end of the single housing and is rotatably coupled to the first shaft member; and

wherein a second of the plurality of power takeoff couplers is arranged on a second end of the single housing that is opposite to the first end along the longitudinal axis, and is rotatably coupled to the second shaft member.

4. The integrated electrified propulsion system of claim 3 , wherein the first shaft member and the second shaft member are collinear, and are collinear with a centerline of the single housing.

5. The integrated electrified propulsion system of claim 3 , wherein the first shaft member and the second shaft member are collinear, and are laterally offset from a centerline of the single housing.

6. The integrated electrified propulsion system of claim 1 , wherein the single electric machine comprises a multi-phase rotary electric motor/generator.

7. The integrated electrified propulsion system of claim 1 , wherein the power electronics system comprises an electric power inverter, an auxiliary power module, an accessory electric motor, an electric charge manager, and a power electronics controller.

8. The integrated electrified propulsion system of claim 7 , wherein the power electronics controller is operatively connected to the electric power inverter, and wherein the electric power inverter is configured to transfer electric power between the single electric machine and the rechargeable energy storage device.

9. The integrated electrified propulsion system of claim 7 , wherein the accessory electric motor is coupled to an air-conditioning (AC) compressor.

10. The integrated electrified propulsion system of claim 1 , further comprising a high-voltage power bus, wherein the high-voltage power bus is configured to transfer electric power between the rechargeable energy storage device and the power electronics system.

11. The integrated electrified propulsion system of claim 1 , wherein the rechargeable energy storage device is disposed in a separate battery housing that is arranged within the single housing.

12. The integrated electrified propulsion system of claim 1 , wherein the integrated cooling system includes a fluidic circuit that is thermally coupled to at least one of the single electric machine, the mechanical geartrain, the rechargeable energy storage device, and the power electronics system via a plurality of fluidic heat exchange devices.

13. An electrified vehicle, comprising:

a chassis, a radiator, a driveline coupled to a drive member, a charger port, and an integrated electrified propulsion system,

wherein the integrated electrified propulsion system is assembled into the chassis;

wherein the integrated electrified propulsion system includes a single electric machine, a mechanical geartrain, a rechargeable energy storage device, an integrated cooling system, and a power electronics system, wherein the single electric machine, the mechanical geartrain, the integrated cooling system, the rechargeable energy storage device, and the power electronics system are arranged in a single housing;

wherein the single electric machine is rotatably coupled to the mechanical geartrain to transfer mechanical power therebetween;

wherein the mechanical geartrain comprises a torque transmission device coupled to a plurality of power takeoff couplers via a plurality of shaft members;

wherein the driveline is mechanically coupled to the mechanical geartrain via the plurality of power takeoff couplers;

wherein the radiator is fluidly coupled to the integrated cooling system; and

wherein the driveline and the drive member are mounted on the chassis.

14. The electrified vehicle of claim 13 , wherein the driveline is arranged in one of a front drive configuration, a rear drive configuration, an all-wheel drive configuration, a four-wheel drive configuration, a four-wheel drive configuration including a power take-off arrangement, a tracked configuration, or a propeller configuration.

15. The electrified vehicle of claim 13 , wherein the plurality of shaft members includes a first shaft member and a second shaft member; wherein the first and second shaft members are arranged parallel to a longitudinal axis of the single housing, wherein a first of the plurality of power takeoff couplers is arranged on a first end of the single housing and is rotatably coupled to the first shaft member, and wherein a second of the plurality of power takeoff couplers is arranged on a second end of the single housing that is opposite to the first end along the longitudinal axis, and is rotatably coupled to the second shaft member.

16. The electrified vehicle of claim 13 , wherein the power electronics system comprises an electric power inverter, an auxiliary power module, an accessory electric motor, an electric charge manager, and a power electronics controller.

17. The electrified vehicle of claim 16 , wherein the power electronics controller is operatively connected to the electric power inverter, and wherein the electric power inverter is configured to transfer electric power between the single electric machine and the rechargeable energy storage device.

18. An integrated electrified propulsion system for a vehicle, consisting of:

a single multi-phase rotary electric motor/generator; a mechanical geartrain; a rechargeable energy storage device; an integrated cooling system; a single housing; and a power electronics system;

wherein the single multi-phase rotary electric motor/generator, the mechanical geartrain, the integrated cooling system, the rechargeable energy storage device, and the power electronics system are arranged in the single housing;

wherein the single multi-phase rotary electric motor/generator is rotatably coupled to the mechanical geartrain to transfer mechanical power therebetween; and

wherein the mechanical geartrain comprises a torque transmission device coupled to a plurality of power takeoff couplers via a plurality of shaft members.

19. The integrated electrified propulsion system of claim 18 ,

wherein the plurality of shaft members includes a first shaft member and a second shaft member; and

wherein the first shaft member and the second shaft member are collinear, and are collinear with a centerline of the single housing.

20. The integrated electrified propulsion system of claim 18 ,

wherein the plurality of shaft members includes a first shaft member and a second shaft member; and

wherein the first shaft member and the second shaft member are collinear, and are laterally offset from a centerline of the single housing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 3, 2022
From: HOOTON, JOEL S.; CASTILLO, BRIAN V.; KLIEWER, JOSEPH D.; HOLMES, ALAN G.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 061287/0394 →
Continuity (1)
Related Publication 20240010062A1 · Jan 11, 2024
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