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Socio-Economic Objective : Air Passenger Transport
Research Topic : Flight dynamics
Australian State/Territory : NSW
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  • Active Funded Activity

    Mid-Career Industry Fellowships - Grant ID: IM230100644

    Funder
    Australian Research Council
    Funding Amount
    $889,472.00
    Summary
    Triple hybrid fuel-cell-based propulsion for long-range eVTOL operations. AMSL Aero's Vertiia is an Australian-developed electric Vertical Take Off and Landing (eVTOL) aircraft that will provide rapid response air ambulance and low-cost passenger transport for rural Australia. This project will optimise a fuel cell/battery/ultracapacitor triple hybrid system for Vertiia by combining dynamic energy source models, hardware-in-the-loop simulations, aero-propulsive flight mechanics models, and accel .... Triple hybrid fuel-cell-based propulsion for long-range eVTOL operations. AMSL Aero's Vertiia is an Australian-developed electric Vertical Take Off and Landing (eVTOL) aircraft that will provide rapid response air ambulance and low-cost passenger transport for rural Australia. This project will optimise a fuel cell/battery/ultracapacitor triple hybrid system for Vertiia by combining dynamic energy source models, hardware-in-the-loop simulations, aero-propulsive flight mechanics models, and accelerated degradation testing. The triple hybrid will extend the life of both batteries and fuel cells for eVTOL aircraft. It will allow AMSL to fast-track the improved durability needed for cost-competitive long-range eVTOL operations, giving them an up-front and industry-leading experience on hybrid systems for eVTOLs.
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    Active Funded Activity

    ARC Future Fellowships - Grant ID: FT230100519

    Funder
    Australian Research Council
    Funding Amount
    $1,118,292.00
    Summary
    Energy Source Durability for Electric Vertical TakeOff and Landing Aircraft. This project aims to address energy source durability for electric Vertical Take Off and Landing (eVTOL) aircraft by optimising a fuel cell/battery/ultracapacitor triple hybrid energy system. The project expects to generate new knowledge in the area of energy source durability using interdisciplinary approaches that combine energy source degradation models, hardware-in-the-loop simulations, aero-propulsive flight mechan .... Energy Source Durability for Electric Vertical TakeOff and Landing Aircraft. This project aims to address energy source durability for electric Vertical Take Off and Landing (eVTOL) aircraft by optimising a fuel cell/battery/ultracapacitor triple hybrid energy system. The project expects to generate new knowledge in the area of energy source durability using interdisciplinary approaches that combine energy source degradation models, hardware-in-the-loop simulations, aero-propulsive flight mechanics models, and accelerated degradation testing. This should provide significant benefits, allowing to fast-track the improved longevity needed for cost-competitive long-range rapid response air ambulance eVTOL operations.
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    Active Funded Activity

    Discovery Projects - Grant ID: DP190103307

    Funder
    Australian Research Council
    Funding Amount
    $255,000.00
    Summary
    Novel power system architecture and control for 'More Electric Aircraft'. This project aims to propose a new conceptual design of an internal aircraft electrical system and its control, which minimises the issues of traditional power systems and takes advantage of contemporary control and technology advances to minimise weight/volume and maximise reliability. The project will target a specific design, which includes consideration of novel power electronic topologies, to achieve these goals. The .... Novel power system architecture and control for 'More Electric Aircraft'. This project aims to propose a new conceptual design of an internal aircraft electrical system and its control, which minimises the issues of traditional power systems and takes advantage of contemporary control and technology advances to minimise weight/volume and maximise reliability. The project will target a specific design, which includes consideration of novel power electronic topologies, to achieve these goals. The results will be validated through simulation, experiments and field testing. It is anticipated that the ideas developed within this project will have a major impact on More Electric Aircraft technology, as well as on general interconnected energy resource systems, such as DC and AC microgrids.
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    Active Funded Activity

    Linkage Projects - Grant ID: LP180101161

    Funder
    Australian Research Council
    Funding Amount
    $194,546.00
    Summary
    Vibration-based health monitoring of aero-engine bearings . This project will develop new vibration-based techniques to greatly improve the detection and diagnosis of faults in aero engine bearings from in-flight measurements. To achieve this goal, advances will be made on source separation algorithms to extract the weak bearing signals, and signal processing techniques to extract features for diagnosing bearing fault severity and lubrication conditions, under a wide range of operating condition .... Vibration-based health monitoring of aero-engine bearings . This project will develop new vibration-based techniques to greatly improve the detection and diagnosis of faults in aero engine bearings from in-flight measurements. To achieve this goal, advances will be made on source separation algorithms to extract the weak bearing signals, and signal processing techniques to extract features for diagnosing bearing fault severity and lubrication conditions, under a wide range of operating conditions. A bearing degradation model will estimate the remaining useful life. Since rolling element bearings are among the most critical components in most machines, the results of this research will also provide massive benefits in other sectors such as mining, transportation, energy production and manufacturing.
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