Helical Stator Windings for Electric Aircraft Motor Thermal Management
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Solution Overview
Problem
In electric multi-propulsion systems for eVTOL aircraft, existing designs face challenges in reducing volumetric, gravimetric, and thermal constraints, limiting efficient flight performance.
Innovation Solution
An integrated electric propulsion assembly with a stator featuring a mandrel with electrically insulating guide walls, copper windings enveloped by epoxy, and a permanent magnet array, which includes a back iron and void configuration to optimize space, weight, and thermal management.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Volume of moving object
If traditional stator designs are used, then magnetic field generation is achieved, but volumetric efficiency is reduced
Solution Approach 1:
The mandrel structure integrates multiple functions into a single component: it provides the structural framework for winding placement, incorporates electrically insulating guide walls directly into its surface, and serves as the core around which copper windings are wound. This merging of functions reduces the number of separate components needed, thereby improving volumetric efficiency while maintaining structural complexity at an acceptable level.
2Power
If more copper windings are added to increase power output, then power increases, but weight increases
Solution Approach 1:
The guide walls extend in the axial dimension of the mandrel, creating three-dimensional channels that allow copper windings to be positioned in multiple spatial layers. This dimensional approach enables more copper windings to be packed into the available volume without simply increasing the radial or circumferential dimensions, thereby increasing power output while controlling weight growth.
3Power
If copper windings are densely packed to improve power density, then power density increases, but thermal management becomes difficult
Solution Approach 1:
The guide walls create localized channels with specific geometric properties that differ from the surrounding winding areas. These channels provide dedicated thermal pathways with different thermal conductivity characteristics, allowing heat to be managed locally in high-density winding regions while maintaining overall power density. The local structural variation enables targeted thermal management without compromising power density.
4Reliability
If electrically insulating materials are added to prevent short circuits, then electrical insulation is improved, but volumetric efficiency decreases
Solution Approach 1:
The mandrel is designed as a multi-functional component that simultaneously provides structural support, winding guidance, and electrical insulation through its integrated guide walls. By making the mandrel itself electrically insulating and multi-functional, the design eliminates the need for separate insulation layers or components, thereby maintaining volumetric efficiency while ensuring adequate electrical insulation for reliability.
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 solution effectively mitigates volumetric, gravimetric, and thermal issues, enhancing the efficiency and performance of electric aircraft propulsion systems by improving structural strength, insulation, and cooling while maintaining efficient magnetic field generation.
Implementation Method 1
a plurality of copper windings wound upon the mandrel, a first cylindrical surface facing the inner cylindrical surface, the first cylindrical surface including a permanent magnet array
Data Source
AI summary
An electric propulsion assembly for an electric aircraft propulsor including an integrated stator assembly including a mandrel having an outer cylindrical surface, an inner cylindrical surface, an upper edge, and a lower edge, the mandrel includes a plurality of electrically insulating guide walls disposed on at least a portion of the outer cylindrical surface and at least a portion of the inner cylindrical surface, wherein the electrically insulating guide wall forms a path across the outer and inner cylindrical surfaces. Assembly includes a plurality of copper windings wound upon the mandrel, electrically insulating epoxy, wherein the epoxy envelops at least a portion of the plurality of copper windings, a first cylindrical surface facing the inner cylindrical surface including a permanent magnet array, a second cylindrical surface facing the outer cylindrical surface including a back iron and a void disposed between the first cylindrical surface and the second cylindrical surface.


