Rotor Shaft Heat Sink Insert for Motor Cooling Flow Control

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Solution Overview

Problem

Existing electric motor designs face challenges in effectively cooling the rotor shaft, which can lead to overheating and reduced efficiency.

Innovation Solution

Incorporating a heat sink insert into the rotor shaft with a first flow passage and multiple second flow passages, along with optional flow interruption grooves, to enhance coolant circulation and heat dissipation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a simple hollow rotor shaft design is used, then the device complexity is reduced, but the cooling efficiency deteriorates leading to overheating

Engineering Contradiction:
Improverotor shaft structureVSAvoidcooling efficiency
Core Design Contradiction:
Device complexityVSTemperature

Solution Approach 1:

The rotor shaft is segmented into multiple functional zones with different cooling mechanisms: a central first flow passage for primary coolant flow, multiple radial second flow passages for secondary cooling, and flow interruption grooves for flow distribution. This segmentation allows each zone to address specific cooling needs, improving overall thermal management without excessive complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the rotor shaft are equipped with tailored cooling features: the first flow passage provides axial cooling at the core, while second flow passages provide radial cooling at the periphery. Flow interruption grooves create localized turbulence zones that enhance heat transfer where needed. This local differentiation optimizes cooling efficiency for each thermal hotspot.

Inventive Principle:
Principle #3Local quality

2Temperature

If coolant flow is increased to improve cooling efficiency, then temperature control improves, but fluid flow patterns become laminar reducing heat transfer

Engineering Contradiction:
Improvetemperature controlVSAvoidheat transfer efficiency
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

Flow interruption grooves are strategically placed to create controlled turbulence and flow disruption in the coolant streams. This mechanical disturbance breaks up laminar flow patterns, enhancing convective heat transfer coefficients. The grooves act as passive turbulence generators that maintain effective heat transfer without requiring additional energy input or complex active control systems.

Inventive Principle:
Principle #18Mechanical vibration

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

Improves cooling efficiency by breaking up laminar flow and increasing heat transfer, thereby maintaining motor performance and reducing the risk of overheating.

Implementation Method 1

a coolant fluid is pumped into the inlet end of the feed tube as the hollow shaft rotates. Fluid that exits the outlet end of the feed tube flows between the feed tube and the inside circumferential surface of the hollow shaft

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 2

The support member causes the coolant fluid to flow circumferentially about the feed tube as the coolant fluid travels in an axial direction back toward the inlet end of the feed tube

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 3

The flow interruption groove is formed through the outer insert surface and intersects at least a portion of the second flow passages... breaking up laminar flow and increasing heat transfer

Methodology Applied
Scientific EffectTurbulence: Turbulence

Data Source

PatentUS12355308B2Electric drive module having motor with heat sink insert in rotor shaft
Publication Date: 2025.07.08 AMERICAN AXLE & MANUFACTURING INC
  • US12355308B2 patent drawing
  • US12355308B2 patent drawing
  • US12355308B2 patent drawing

AI summary

A motor drive system has a rotor assembly that is rotatable about an axis and includes a hollow shaft, a tube, and one or more fin sets. The tube is received in the shaft and defines a first passage. The fin sets are disposed about the tube and are engaged to the shaft. Each fin set defines a plurality of circumferentially spaced apart fins that are coupled to the shaft and the tube. The first passage is configured to discharge fluid communicated therethrough into a return chamber that is formed in the rotor assembly. A plurality of second passages are formed between the shaft and fins and are in fluid communication with the return chamber.