EESM Rotor Assembly With Centrifugal Oil Cooling for Heat Evacuation

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Solution Overview

Problem

Electric excited synchronous motors (EESMs) face limitations in heat evacuation due to indirect cooling systems, which restrict their performance as they replace high-power permanent magnet synchronous motors, necessitating more effective direct cooling systems.

Innovation Solution

A rotor assembly for EESMs featuring a direct oil cooling system utilizing centrifugal force to impulse cooling fluid through the rotor and end windings, with radial bores and axial channels connected to fluid guide elements that direct cooling fluid to the winding ends, allowing efficient heat dissipation without high pressure requirements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If indirect cooling systems (housing water jacket or air-cooling) are used in EESMs, then the structure is simple, but the heat evacuation capability is limited

Engineering Contradiction:
Improvecooling system structureVSAvoidheat evacuation capability
Core Design Contradiction:
Ease of manufactureVSTemperature

Solution Approach 1:

The invention extracts the cooling function from the housing and creates dedicated cooling channels within the rotor shaft and rotor core. Cooling channels are formed directly in the rotor structure, allowing cooling fluid to flow through and directly remove heat from the rotor windings and core, separating the cooling function from the structural housing function.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The invention introduces cooling fluid as an intermediary substance to transfer heat from the rotor windings and core to the external cooling system. The cooling fluid flows through channels in the rotor shaft and rotor core, absorbing heat and carrying it away, thus mediating the heat transfer process more effectively than air or housing conduction.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Temperature

If direct cooling systems are implemented to improve heat evacuation, then the cooling efficiency increases, but the system complexity increases

Engineering Contradiction:
Improvecooling efficiencyVSAvoidcooling system structure
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The invention merges the cooling system with the rotor structure by integrating cooling channels directly into the rotor shaft and rotor core. The cooling channels are formed as part of the rotor manufacturing process, combining the structural and cooling functions into a single integrated component, thereby reducing overall system complexity while achieving direct cooling.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The rotor structure serves multiple functions: it provides mechanical support for the windings, maintains magnetic circuit integrity, and simultaneously acts as a cooling fluid conduit. The rotor shaft and rotor core are designed to perform both structural and thermal management functions, reducing the need for separate cooling components.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Quantity of substance

If high pressure is used to impulse cooling fluid through the rotor, then the cooling fluid flow is improved, but the pressure requirements and system complexity increase

Engineering Contradiction:
Improvecooling fluid flowVSAvoidpressure requirements
Core Design Contradiction:
Quantity of substanceVSStress or pressure

Solution Approach 1:

The invention utilizes the dynamic rotation of the rotor to generate centrifugal force, which dynamically drives the cooling fluid through the cooling channels. As the rotor rotates, the centrifugal force automatically propels the cooling fluid from the rotor shaft through the rotor core and out through the escape openings, eliminating the need for high pressure pumps or complex pressurization systems.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The rotating rotor itself serves as the driving mechanism for the cooling fluid flow. The centrifugal force generated by the rotor's own rotation is sufficient to impulse the cooling fluid through the channels and onto the windings, making the system self-sufficient and eliminating external high-pressure sources.

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This design enhances cooling efficiency and extends the service life of EESMs by effectively distributing cooling fluid and heat across the rotor assembly, addressing the limitations of traditional cooling systems.

Implementation Method 1

A rotor assembly for an electric excited synchronous motor (EESM) can be provided with a direct oil cooling system, which uses a centrifugal force caused by a rotation of the rotor to impulse cooling fluid

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentUS20240429783A1Rotor assembly for an electric excited synchronous motor (EESM)
Publication Date: 2024.12.26 GKN AUTOMOTIVE LTD
  • US20240429783A1 patent drawing
  • US20240429783A1 patent drawing
  • US20240429783A1 patent drawing

AI summary

A rotor assembly for an electric excited synchronous motor (EESM) comprises: a rotor shaft, a rotor core with windings, a first and a second fluid guide element arranged at the ends of the rotor core, wherein the rotor shaft comprises an axial bore and a plurality of radial bores, wherein the rotor core includes a plurality of inlet openings fluidically connected to the radial bores, and axial channels extending axially to first and second outlet openings of the rotor core, wherein the first and second fluid guide elements are fluidically connected to the outlet openings of the rotor core and comprise a fluid structure configured to receive cooling fluid from the rotor core and guide same to escape openings arranged in circumferential direction between two circumferentially adjacent winding ends of the rotor.