Rotor Lamination Local Alloy Tuning to Reduce Flux Leakage

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Solution Overview

Problem

Current electric machine designs for electrified vehicles face challenges in achieving high power outputs and efficiency due to magnetic flux leakage and conflicting property requirements for different regions within the rotor lamination, leading to trade-offs between mechanical strength and electromagnetic performance.

Innovation Solution

The method involves fabricating rotor laminations using additive manufacturing techniques, where different powdered metals with varying compositions are used in specific regions to optimize magnetic permeability, mechanical strength, and core loss, allowing for locally-tuned properties within the lamination plane, such as using FeSi alloys for high permeability regions and non-ferromagnetic austenite stainless steel for reduced permeability in bridge areas.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If a uniform metal alloy is used throughout the rotor lamination, then manufacturing is simple, but magnetic flux leakage occurs and electromagnetic performance is compromised

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidmagnetic flux leakage
Core Design Contradiction:
Ease of manufactureVSLoss of energy

Solution Approach 1:

The rotor lamination is divided into multiple regions with different metal alloy compositions. High permeability alloy (e.g., FeSi) is used in magnet pocket regions to enhance magnetic flux density, while low permeability alloy is used in bridge regions to reduce magnetic flux leakage. This local differentiation of material properties optimizes electromagnetic performance without compromising manufacturing feasibility through additive manufacturing processes.

Inventive Principle:
Principle #3Local quality

2Loss of energy

If high permeability metal alloy is used in bridge regions, then magnetic flux density is improved, but mechanical strength is reduced

Engineering Contradiction:
Improvemagnetic flux densityVSAvoidmechanical strength
Core Design Contradiction:
Loss of energyVSStrength

Solution Approach 1:

Different metal alloy compositions are strategically assigned to different functional regions of the rotor lamination. The bridge regions, which require high mechanical strength to withstand centrifugal forces, are made from low permeability alloy with superior mechanical properties. The magnet pocket regions, which require high magnetic permeability for optimal electromagnetic performance, are made from high permeability alloy. This spatial differentiation resolves the contradiction between magnetic performance and mechanical strength.

Inventive Principle:
Principle #3Local quality

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 approach enhances torque density and motor efficiency by strategically modifying physical properties, reducing magnetic flux leakage and increasing mechanical strength, thereby improving the overall performance of electric machines in electrified vehicles.

Implementation Method 1

with a laser, fabricating a first region of a rotor lamination layer with a first powdered metal having a first composition

Methodology Applied
Scientific EffectLaser: Laser

Implementation Method 2

fabricating a first region of a rotor lamination layer with a first powdered metal having a first composition

Methodology Applied
Scientific EffectSelective Laser Sintering: Selective Laser Sintering

Implementation Method 3

permanent magnets disposed in the magnet pockets

Methodology Applied
Scientific EffectElectromagnetic Induction: Electromagnetic Induction

Data Source

PatentUS20240258888A1Electric machine with locally-tuned properties
Publication Date: 2024.08.01 FORD GLOBAL TECH LLC
  • US20240258888A1 patent drawing
  • US20240258888A1 patent drawing
  • US20240258888A1 patent drawing

AI summary

An electric machine includes a stack of interlocked rotor core laminations, individual rotor core laminations of the interlocked rotor core laminations including a mortise extending therein and an integrally-formed tenon extending therefrom, wherein the tenons interface with the mortises to interlock adjacent rotor core laminations.