ROLE OF ADDITIVE MANUFACTURING AND ADVANCED MATERIALS IN ENABLING NEXT ERA ELECTRIC MOTORS FOR AEROSPACE AND TRACTION APPLICATIONS
The rapid transformation towards more electrified propulsion systems in ground and aerospace applications has intensified the need to advance the current State-Of-The-Art (SOTA) electrical machines for improved power density, efficiency, and materials sustainability. Achieving these demanding characteristics and pushing the boundary of the SOTA require attempting new design methodologies to leverage advanced materials and innovative manufacturing techniques.
Additive Manufacturing (AM) has emerged as a promising enabler to contribute to such advancements of electrical machines in their active or passive parts. AM offers a wide range of materials with opening the design space for customized and sophisticated topologies, enabling integration of subsystems including complex direct cooling approaches and Power Electronics Unit (PEU), and reducing materials waste. However, the adoption of AM in electric machines requires a thorough understanding of its trade-off in performance, manufacturability, and build quality to best exploitation of its advantages. In addition, development in various engineering aspects is driven by materials affecting performance, sustainability, and associated technology cost.
Permanent Magnet (PM) traction electric motors have enabled improved power/torque densities with higher efficiencies and thus dominate Ground Electric Vehicles (GEVs) applications. However, the preferred type of PM (Dy-NdFeB) contains critical Rare-Earth (RE) elements that are susceptible to price volatility and sustainability concerns. Therefore, the development of new materials, especially new PM materials to reduce the reliance on critical elements is a key enabler for the continued efforts to deploy GEVs. Notable among these materials is second generation Iron Nitride (FeN) that is currently under development by Niron Magnetics with an energy product of 24-36 MGOe. FeN has attracted increasing attention for its high remanent flux density exceeding 1.3 T and RE-free composition, making it a potential candidate to replace or reduce the utilization of conventional RE-PMs.
This dissertation builds on two major U.S. Department of Energy鈥揻unded efforts that contribute to the advancement of SOTA in sustainable electric propulsion. The first, the ARPA-E ASCEND project (in collaboration with Raytheon Technologies, NREL, Florida State University, and Ampaire), aims to demonstrate a 250-225 kW class aerospace motor with an exceptionally high Specific Power (SP) above 12 kW/kg (at a system level) and efficiency exceeding 93% throughout the cruising flight condition. The proposed motor features hollow AM-ALuminum (AM-AL) windings with integrated Heat Pipes (HPs), integrated to dual AM-Condenser Chambers using PEEK aerospace grades to realize direct cooling and lightweight construction. The
contributions of this dissertation include the analysis and optimization of the motor electromagnetic design, design topology trade-off studies, and design of novel AM heat exchanger, enabling the motor to take advantage of directly integrated stator cooling through the adoption of AM. The AM-AL windings enable the tight integration to the PEU in modular approach improving overall system SP. The design in this dissertation has been optimized and evaluated in terms electromagnetic performance, effectiveness of its Thermal Management System (TMS) with CFD and thermal analyses on the novel TMS, including prototyping the proposed design with testing the full system. The motor has been fabricated with total mass of 32.4 kg including the integration of its TMS, which leads to a system SP of 7-7.7 kW/kg (225-250 kW). The motor entered the testing phase and has been tested up to 65% of its power capability. Moreover, the motor operated at 140 kW at a current density of 17.5 Arms/mm2, while testing is in progress to operate at the maximum power of 225 kW.
The second research funding effort, the DOE EERE-VTO Program, targets the development of rare-earth-free electric powertrain for GEVs through collaboration with Niron Magnetics, General Motors, NREL, and Virginia Tech. This dissertation explores blending FeN PMs and high-performance Ferrite PMs within Interior Permanent Magnet (IPM) motors operating up to 16,000 rpm and at 800V, furthering the recent industry trend of increasing speed and voltage. The contribution of this dissertation is the demonstration of the proposed design for this funding effort, addressing demagnetization concerns with FeN magnets and delivering competitive electromagnetic performance. Of note in this work is the development of very detailed electromagnetic and mechanical parametrizations for performing multi-physics optimization covering electromagnetic performance and rotor stress mechanical analysis.
By integrating these two directions, advanced manufacturing and advanced materials, advanced electric propulsion systems can be realized. The outcome highlights the use of both directions in electric machines can redefine performance limits for both aerospace and ground transportation applications, contributing to achieving global electrification goals for energy efficiency and sustainable energy conversion technologies.