Browse Topic: Lightweighting
With new energy vehicles developing rapidly, battery safety, as an important part of the impact on the range of new energy vehicles and vehicle safety, has become the focus of attention. The battery pack protection plate is a core component to protect the battery, its performance needs not only impact resistance, but also lightweight, honeycomb sandwich structure with its excellent energy absorption characteristics and weight reduction performance by the battery pack protection plate performance research. At present, the core-to-face sheet interaction in conventional sandwich structures subjected to impact loads has not been fully elucidated, and the quantitative characterization of damage is insufficient, so this paper aims to optimize the lightweight impact-resistant structure by exploring the synergistic energy dissipation mechanism between the high-strength core material and the steel plate. The study combines theory and simulation, adopting ideal rigid-plastic film theory to establish a critical response model to predict the structural failure threshold, equivalent single-layer theory to simplify the analysis of plywood, and a stiffness matrix model to quantify the structural mechanical contribution of each layer. A two-material synergistic design framework is proposed by fully considering the material properties and adopting the corresponding intrinsic structure and failure criteria for different materials. Analysis reveals that geometric confinement is a key characteristic of the honeycomb sandwich panel’s response and a strain gradient driving mechanism at low impact resistance, and a new energy distribution paradigm is found through the analysis of the energy absorption ratio. The theoretical and simulation results are in great agreement with each other, which just has a difference of 0.7% in the peak force, 1.4% in the critical displacement error, and less than 2% in the impulse integration error. The proposed dual-material co-design framework provides a solution for electric vehicle battery protection systems that balances lightweight and impact resistance.
The present study aims to investigate the dynamic behavior of composite drive shafts operating in the supercritical rotational speed regime, with a particular focus on the mode crossing and the potential emergence of vibratory instabilities. Composite shafts offer significant advantages in terms of mass reduction and mechanical properties, making them attractive for high-performance transmission systems such as helicopter drive lines. However, their operation beyond the first critical speed raises specific challenges related to stability, damping, and sensitivity to mechanical and operational parameters. To address these issues, an experimental and analytical framework was developed to explore a wide design space involving parameters that are known or suspected to influence supercritical behavior. These parameters include unbalance levels, support characteristics, flexible coupling properties, tightening conditions of the damper, and rotational speed. Particular attention was given to the analysis of the mode crossing phenomenon in composite supercritical shafts, as well as to the identification of the most influential contributors to the vibratory response within the defined experimental perimeter. Harmonic- and subharmonic-based analyses were conducted to assess the relevance of each parameter across different frequency regimes. Overall, the results indicate that, despite the wide parametric exploration, no dynamic instability was observed in the supercritical regime, thereby demonstrating the robust vibratory behavior of composite shafts and supporting their suitability for advanced helicopter transmission applications.
An internal layout design framework for a medium-class rotorcraft fuselage is attempted to build based on the idea of the energy-based load-transfer index. Load-transfer index will quantify the way in which the flight loads are distributed among the fuselage internal structural members. The static load-transfer analysis will identify an inefficient transfer region in the baseline fuselage configuration, and the resulting layout refinement will lead to a more unified load-transfer pattern and allow an additional weight reduction in the subsequent thickness-optimization stage. For a UH-60A aircraft, the existing literature provides well-established information for an airframe layout, finite-element modeling guideline, and ground vibration test correlation.
Emerging technologies in the field of electrified propulsion systems offer a promising solution to reduce the dependence on fossil fuels and improve efficiency. However, the design of high-power density electric machines introduces new challenges, including limited passive cooling potential and the issue of the weight of electric motors. To address these challenges, this paper considers analysis and design methods for high torque-to-weight ratio axial flux motors. A magnetic equivalent circuit model coupled with a lumped parameter thermal network is developed for design space exploration and optimization. This inexpensive analytical model predicts the performance of a single-stator dual-rotor axial flux motor based on geometry, loading condition, and slot and pole pair combination. To enable comparisons against real-world data, the optimization study was demonstrated using the hover mission requirements from the Research Aircraft for eVTOL Enabling techNologies (RAVEN) vehicle to minimize the mass of the motor. In tandem with the analytical model, a higher-fidelity finite element model was also developed, and good agreement between predicted power and efficiency was demonstrated across a range of axial flux motor designs. The lightest weight design that satisfied the hover mission requirements was the 12 pole pair 27 slot (12PP 27S) configuration with a fixed weight of 9.28 kg. The analytic model undersized the output power of the electric motor by approximately 9% across a range of slot and pole pair combinations.
The wheel rim is an annular, thin-walled structure featuring complex geometry and is subjected to multiple load cases, including radial, rotary, and impact scenarios. Achieving an optimal balance between mass reduction and structural performance remains a significant challenge in modern vehicle wheel design. Aero-efficient vehicles demand lightweight backbone wheels capable of accommodating aerodynamic covers without compromising handling, steering precision, or overall performance. In this study, shape optimization is applied to an 8-spoke truck wheel with the goal of minimizing mass while enhancing lateral stiffness and ensuring that stress constraints are satisfied under all critical load cases. A three-dimensional finite element model is developed and evaluated under realistic radial, rotary, and impact loading conditions representative of industry validation tests. The optimization process fine-tuned the spoke geometry using symmetric shape domains and carefully defined perturbation vectors, while preserving styling intent, bolt pattern, and brake packaging constraints. Lateral stiffness was evaluated using a frequency-based formulation derived from modal and frequency response analyses, while grid stress responses served as robust optimization constraints. The resulting optimized wheel achieved a mass reduction of approximately 5 percent, a lateral stiffness increase of approximately 30 percent, and a 6 percent rise in the first drum-mode frequency.
Lightweighting of components has become a key challenge in the development of modern transportation systems. In the automotive and aerospace industries, the overall mass of a vehicle has a significant impact on its fuel efficiency and manufacturing cost. Therefore, the lightweight design of vehicle components is crucial in the industrial field. Topology optimization (TO) is a computational design approach aimed at achieving lightweight designs. However, most existing studies focus on simplified academic models, with limited demonstration in real-world applications. This paper presents a revised TO workflow to obtain production-ready design and a practical implementation of TO in the design of three structural components in the aerospace industry: seatback frame, seat fuselage mount, and seat spreader. The revised TO workflow incorporates the practical demands of industry, including enhanced manufacturability and cost efficiency through TO design. The resulting designs are evaluated to ensure all regulatory requirements are satisfied. Comparative results show that the designs produced by the presented TO-based design method achieve a significant weight reduction of 50% for the seatback frame. For the seat fuselage mount and seat spreader, the proposed method produced designs with a weight comparable to the baseline while satisfying stricter crashworthiness requirements. These components also ensure manufacturability, efficient fabrication cost, and compatibility with family parts. These findings demonstrate that TO can deliver production-ready solutions without compromising structural performance. The study highlights the potential of integrating TO into a revised design workflow to support performance-driven development of complex, production-ready industrial components.
Winners of the 13th edition of the Altair Enlighten Awards, presented in association with the Center for Automotive Research, were recognized during a ceremony at the CAR Management Briefing Seminars in Detroit. The awards not only acknowledged the automotive industry's best initiatives to reduce vehicle weight and meet emissions targets, but also considered other parameters such as cost reduction, part count reduction and applicability to other vehicle programs. “Starting in the 2000s, the automotive industry wasn't really that interested in optimization. Weight was an outcome of achieving performance. Seeing the rise of these digital technologies over two decades has been such a thrill,” Royston Jones, CTO of Altair Product Design and senior VP for automotive, said to kick off the event. “I'd say now we're really through the gate, particularly over the last five years where globally there's such pressure to develop products quickly. AI has really helped with technology such as optimization, so I think it's only going to accelerate, it's going to get smarter. This is such an exciting time to be in this digital space.”
Winners of the 13th edition of the Altair Enlighten Awards, presented in association with the Center for Automotive Research, were recognized during a ceremony at the CAR Management Briefing Seminars in Detroit. The awards not only acknowledged the automotive and commercial vehicle industries' best initiatives to reduce vehicle weight and meet emissions targets, but also considered other parameters such as cost reduction, part count reduction and applicability to other vehicle programs. “Starting in the 2000s, the automotive industry wasn't really that interested in optimization. Weight was an outcome of achieving performance. Seeing the rise of these digital technologies over two decades has been such a thrill,” Royston Jones, CTO of Altair Product Design and senior VP for automotive, said to kick off the event. “I'd say now we're really through the gate, particularly over the last five years where globally there's such pressure to develop products quickly. AI has really helped with technology such as optimization, so I think it's only going to accelerate, it's going to get smarter. This is such an exciting time to be in this digital space.”
Modern military aircraft represent some of the most complex electronic environments ever engineered. These platforms integrate advanced avionics, radar systems, data links, and communication networks that must function seamlessly in hostile, high-frequency environments. In these mission-critical contexts, electromagnetic interference (EMI) poses a silent but serious threat that can degrade signal integrity, cause crosstalk between systems, or even lead to mission failure. The combination of increasing data rates, higher frequencies, and more complex electromagnetic environments demands shielding solutions that can deliver superior performance while contributing to overall system weight reduction. This challenge has driven innovation toward advanced materials that maintain electrical effectiveness while dramatically reducing mass.
The paper describes a method for optimal design of a helicopter tail shaft that considers rotordynamic effects from long shaft assembly. The tail shaft transmits power from the main gearbox (MGB) to the tail rotor of the helicopter and operates at high speeds that may exceed 6000 rpm. While higher speeds allow for weight reduction, they also pose risks associated with supercritical operation, necessitating careful design optimization. The objective of the optimization is to maximize the first three transverse natural frequencies with the constraint of the safety parameter (avoidance of the resonance/critical zone) while minimizing the weight of the system. A Non-Dominated Sorting Genetic Algorithm (NSGA-II) is used to obtain the solution to this multiobjective optimization problem, which involves shaft design variables such as length, outer diameter, and wall thickness. In addition, the optimization framework also incorporates system related design variables, including the stiffness of tail shaft bearing supports, the location of bearings, and coupling characteristics, to comprehensively evaluate and enhance the system performance. A rotordynamics model utilizing Timoshenko beam finite elements is deployed to predict natural frequencies.
Fatigue design is invariably of prior concern for the automotive industry, no matter of the evolution of the mobility market: at first because carmakers must stay compliant with general structural integrity requirements for reliability, notably applicable to the chassis system, then due to the endless competition for lightweighting in order to mitigate product costs and/or enhance vehicle efficiency. In the past, this key performance was often tackled by basic reference load cases, making use of the simplest signal content, e.g. sinus functions, to practice constant amplitude loads on test rigs and for computations, respectively. Nowadays, full time series coming from proving ground measurements, or any corresponding virtual road load data computations, may be applied to feed complex vehicle computations for virtual assessment and complex test facilities for final approval, under variable amplitude loads. In between, the concept of load spectra (i.e. distribution of amplitudes with respect of their occurrences) is here highlighted as relevant and effective to manage the load/stress generation step of the fatigue design. At first, a theoretical model is called from recent papers and detailed. Moreover, it is identified on several proving ground measurements, focusing on wheel force transducer signals. Then, a discussion on the parameters values allows to shape some general trends of the model, which is in return considered trustable for any further inference. This opens the way to two main applications: damage assessment as a function of the material/process of interest, and test acceleration making use of block-type schedules.
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