Dual-Cavity Rotor Assembly for Centrifugal Coolant Flow

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Solution Overview

Problem

Contemporary dry cavity electric machines face challenges in maintaining high power density and efficiency due to limited cooling effectiveness, especially when multiple contained cooling systems are used, leading to increased thermal demands and potential heating issues.

Innovation Solution

A rotor assembly design with a dual-cavity structure and angled inner surfaces that utilize centrifugal forces to increase coolant flow velocity and pressure, optimizing coolant flow based on rotational speed to enhance cooling efficiency and reduce thermal stress.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If multiple contained cooling systems are applied in a dry cavity machine, then cooling effectiveness is improved, but power density decreases

Engineering Contradiction:
Improvecooling effectivenessVSAvoidpower density
Core Design Contradiction:
TemperatureVSPower

Solution Approach 1:

The rotor is divided into two separate cavities (inner cavity and outer cavity) with distinct cooling functions. The inner cavity houses the rotor assembly and handles internal cooling, while the outer cavity provides external cooling pathways. This segmentation allows independent optimization of cooling effectiveness without compromising power density, as each cavity serves a specific cooling purpose rather than requiring multiple overlapping cooling systems.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A set of radial openings acts as an intermediary mechanism between the inner and outer cavities, enabling coolant flow transition and thermal management. These openings allow controlled heat dissipation from the inner cavity to the outer cavity, providing effective cooling while maintaining the structural integrity and power density of the rotor assembly.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Temperature

If coolant flow velocity is increased to enhance cooling, then cooling efficiency improves, but thermal stress and leakage risks increase

Engineering Contradiction:
Improvecooling efficiencyVSAvoidthermal stress and leakage
Core Design Contradiction:
TemperatureVSObject-affected harmful factors

Solution Approach 1:

The inner surface of the rotor cap is designed with a specific angle (between 10-45 degrees) to optimize coolant flow characteristics locally. This angled surface creates a controlled flow path that increases coolant velocity for improved cooling efficiency while simultaneously managing thermal stress distribution and minimizing leakage risks through optimized flow dynamics.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The angle of the inner surface of the rotor cap is optimized to change coolant flow parameters (velocity, pressure distribution) in a controlled manner. By adjusting this geometric parameter, the system achieves enhanced cooling efficiency while maintaining acceptable thermal stress levels and leakage prevention, rather than simply increasing flow velocity without control.

Inventive Principle:
Principle #35Parameter changes

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

The design achieves improved cooling capabilities, maintaining high power density and efficiency by managing coolant flow pressure, leakage, and thermal demands across varying rotational speeds, reducing the risk of overheating and enhancing overall performance.

Implementation Method 1

A rotor assembly design with a dual-cavity structure and angled inner surfaces that utilize centrifugal forces to increase coolant flow velocity and pressure

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Implementation Method 2

The design achieves improved cooling capabilities, maintaining high power density and efficiency by managing coolant flow pressure, leakage, and thermal demands across varying rotational speeds

Methodology Applied
Scientific EffectConvection cooling: Convection

Data Source

PatentUS12525835B2Rotor assembly for an electrical machine
Publication Date: 2026.01.13 GE AVIATION SYSTEMS LLC
  • US12525835B2 patent drawing
  • US12525835B2 patent drawing
  • US12525835B2 patent drawing

AI summary

A rotor assembly for an electric machine includes a first end and a second end, the second end distal from the first end in an axial direction, a first radial wall extending between the first end and the second end and defining an inner cavity, and a second radial wall extending between the first end and the second end, the second radial wall radially-overlying the first radial wall and defining an outer cavity between the first radial wall and the second radial wall.