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Field of Research : Aerospace Engineering
Research Topic : Memory Structures
Status : Closed
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  • Funded Activity

    Linkage - International - Grant ID: LX0348548

    Funder
    Australian Research Council
    Funding Amount
    $74,000.00
    Summary
    Structural and multidisciplinary optimization. Structural and multidisciplinary design optimization is an important subject in aeronautical, aerospace, automobile, offshore platforms and many other structures. This project aims to address design optimization of coupled structures, with a focus on electro-mechanical coupled structures. It is expected to coordinate an integrated effort to develop efficient and effective algorithms for optimum design of electro-mechanical coupled structures.
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    Funded Activity

    Discovery Projects - Grant ID: DP0666683

    Funder
    Australian Research Council
    Funding Amount
    $275,000.00
    Summary
    Shape adaptive structures with built-in compact smart material based actuators. Primary Australian aerospace manufacturers are sub-contractors and constantly compete in the global market. Their products are primarily control surfaces, e.g., Boeing 757 and 777 rudders, 737 Krueger flaps. In light of the development of the hingeless control surfaces (HCS) in the smart aircraft wing program in the USA, the economic benefits of this project are very high because (a) it will address the key technolo .... Shape adaptive structures with built-in compact smart material based actuators. Primary Australian aerospace manufacturers are sub-contractors and constantly compete in the global market. Their products are primarily control surfaces, e.g., Boeing 757 and 777 rudders, 737 Krueger flaps. In light of the development of the hingeless control surfaces (HCS) in the smart aircraft wing program in the USA, the economic benefits of this project are very high because (a) it will address the key technological issue identified in the HCS program; and (b) it will enhance Australian manufacturers¡¯ technological standing and input in the design and manufacturing of next generation HCS by providing highly trained people with world-leading niche technology.
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    Funded Activity

    Discovery Projects - Grant ID: DP0210716

    Funder
    Australian Research Council
    Funding Amount
    $279,000.00
    Summary
    Active shape control of large thin-walled structures using ferroelectric single crystals. Ferroelectric single crystals were invented 5 years ago, and they possess many superior properties compared to conventional piezoelectric materials, particularly the induced strain up to 1.5%, an order higher than conventional materials. This project aims to poineer the application of these new and powerful smart materials as actuators and sensors to shape control of smart structures. The expected outcome .... Active shape control of large thin-walled structures using ferroelectric single crystals. Ferroelectric single crystals were invented 5 years ago, and they possess many superior properties compared to conventional piezoelectric materials, particularly the induced strain up to 1.5%, an order higher than conventional materials. This project aims to poineer the application of these new and powerful smart materials as actuators and sensors to shape control of smart structures. The expected outcomes are (a) a new constitutive theory for the non-linear behaviour of ferroelectric single crystals; (b) a novel definition and formulation for the shape control problem; and (c) an innovative theoretical framework for design optimization of shape control of smart structures using ferroelectric single crystals.
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    Funded Activity

    Discovery Projects - Grant ID: DP0774596

    Funder
    Australian Research Council
    Funding Amount
    $351,942.00
    Summary
    Morphing flexible structures with lead lanthanum zirconium titanate (PLZT) based optical actuators. Lead lanthanum zirconate titanate (PLZT) materials yield mechanical strains when exposed to near ultraviolet light as a result of combined photovoltaic and converse piezoelectric effects. They offer actuation strain on par with piezoelectric materials and other advantages, such as wireless light-to-mechanical energy transfer, immunity from electrical and magnetic disturbances and fast response wi .... Morphing flexible structures with lead lanthanum zirconium titanate (PLZT) based optical actuators. Lead lanthanum zirconate titanate (PLZT) materials yield mechanical strains when exposed to near ultraviolet light as a result of combined photovoltaic and converse piezoelectric effects. They offer actuation strain on par with piezoelectric materials and other advantages, such as wireless light-to-mechanical energy transfer, immunity from electrical and magnetic disturbances and fast response with the transparent electrode design. This project aims to pioneer the application of PLZT optical actuators in morphing flexible structures leading to development of wireless smart structures technology and opt-electromechanical systems such as medical instruments.
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    Funded Activity

    Discovery Projects - Grant ID: DP0663228

    Funder
    Australian Research Council
    Funding Amount
    $290,000.00
    Summary
    A Multi-Scale Approach To Reliability And Durability Of Engineering Structures And Sensors. The Longford explosion is an example where a major failure was due to a very small defect. It is estimated to have cost Australia in excess of $1.5 Billion. The acquisition costs of aircraft mean that keeping a fleet operational for a year can produce savings of ~$100,000,000.The automotive industry is designing lighter vehicles. GM Australia has realised that ensuring the durability of these new designs .... A Multi-Scale Approach To Reliability And Durability Of Engineering Structures And Sensors. The Longford explosion is an example where a major failure was due to a very small defect. It is estimated to have cost Australia in excess of $1.5 Billion. The acquisition costs of aircraft mean that keeping a fleet operational for a year can produce savings of ~$100,000,000.The automotive industry is designing lighter vehicles. GM Australia has realised that ensuring the durability of these new designs is essential. By our participation in the GM PACE program we ensure that the developments are available to the broader Australian Industry. Indeed, to design durable MEM's structures would give Australia a commercial edge.
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    Funded Activity

    Discovery Projects - Grant ID: DP0986291

    Funder
    Australian Research Council
    Funding Amount
    $150,000.00
    Summary
    Supersonic Particle Deposition Of Metal Matrix Composite/Aluminium Alloy For Ensuring The Continued Airworthiness Of Damaged Structures. The June 2007 Report to Congress by the US Under Secretary of the Department of Defence (Acquisition, Technology and Logistics) estimated the cost of corrosion associated with US DoD systems to be between $10 billion and $20 billion annually. It further stated that the US DoD has focused its life-cycle corrosion research and development efforts on four primary .... Supersonic Particle Deposition Of Metal Matrix Composite/Aluminium Alloy For Ensuring The Continued Airworthiness Of Damaged Structures. The June 2007 Report to Congress by the US Under Secretary of the Department of Defence (Acquisition, Technology and Logistics) estimated the cost of corrosion associated with US DoD systems to be between $10 billion and $20 billion annually. It further stated that the US DoD has focused its life-cycle corrosion research and development efforts on four primary areas one of which is repair processes that restore corroded materials to an acceptable level of structural integrity and functionality. This project specifically addresses that topic and as such will have a significant impact on Australia's Defence infrastructure.
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    Funded Activity

    Linkage Projects - Grant ID: LP100100508

    Funder
    Australian Research Council
    Funding Amount
    $105,000.00
    Summary
    Improving the process modelling capability for manufacturing large composite structures used on passenger aircraft. This proposal aims to reduce manufacturing costs by developing innovative simulation tools for the production of future lightweight composite aerostructures.The development of a reliable predictive tool to simulate the cost-effective production of resin-infused composite aerostructures, will represent a significant technical advance. The successful transfer of this technology to Bo .... Improving the process modelling capability for manufacturing large composite structures used on passenger aircraft. This proposal aims to reduce manufacturing costs by developing innovative simulation tools for the production of future lightweight composite aerostructures.The development of a reliable predictive tool to simulate the cost-effective production of resin-infused composite aerostructures, will represent a significant technical advance. The successful transfer of this technology to Boeing Aerostructures Australia would give it a distinct competitive edge when bidding for participation in future international development programmes and will yield substantial economic benefits whilst further strengthening and developing local expertise. Lightweight aircraft structures will also contribute towards reducing the environmental impact of aviation.
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    Funded Activity

    Linkage Projects - Grant ID: LP0212110

    Funder
    Australian Research Council
    Funding Amount
    $177,000.00
    Summary
    Thermoforming Mechanisms for Cost-effective Manufacturing of Advanced Composite Structures. The cost barrier in thermoforming, due to the lack of understanding of shear deformation and wrinkling, has inhibited the large-scale application of fibre-reinforced composite structures in aerospace and automobile industries. This project aims to develop a cost-effective diaphragm thermoforming process through an in-depth understanding of the thermoforming mechanisms. The outcomes will include novel theo .... Thermoforming Mechanisms for Cost-effective Manufacturing of Advanced Composite Structures. The cost barrier in thermoforming, due to the lack of understanding of shear deformation and wrinkling, has inhibited the large-scale application of fibre-reinforced composite structures in aerospace and automobile industries. This project aims to develop a cost-effective diaphragm thermoforming process through an in-depth understanding of the thermoforming mechanisms. The outcomes will include novel theories for thermoforming, a standard method for material property characterization and new finite element models compatible with the most popular software available for industry. The project will form the basis for establishing the effective production window and enhance greatly the competitive edge of the Australian manufacturing industry.
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    Funded Activity

    Discovery Projects - Grant ID: DP0209504

    Funder
    Australian Research Council
    Funding Amount
    $220,186.00
    Summary
    Micro-electromechanics and finite element analysis models for adaptive structures. Adaptive structures are becoming increasingly important due to their direct improvement of structural system performance. However, electroelastic behaviour and damage mechanism, which are primary concerns for adaptive structural design, are poorly understood. This project aims at developing micro-electromechanics and finite element analysis models to investigate the electroelastic properties and detect delaminatio .... Micro-electromechanics and finite element analysis models for adaptive structures. Adaptive structures are becoming increasingly important due to their direct improvement of structural system performance. However, electroelastic behaviour and damage mechanism, which are primary concerns for adaptive structural design, are poorly understood. This project aims at developing micro-electromechanics and finite element analysis models to investigate the electroelastic properties and detect delamination for adaptive structures. It combines the fields of micro-electromechanics and composite material analysis in a computational framework to provide a useful and cost-effective tool for modelling the response of adaptive structures. It is a challenging task and will have significant impact in the adaptive structure design community.
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    Funded Activity

    Linkage Projects - Grant ID: LP150100653

    Funder
    Australian Research Council
    Funding Amount
    $330,000.00
    Summary
    Onset Theory: Pushing the design envelope for textile composite structures. This study aims to exploit an innovative physics-based approach to predict the strength of textile composites. This is particularly important in areas such as aircraft design, where drastic weight savings are needed to allow designers to remain competitive in a low-carbon future. Improved theory and design tools will remove conservatism and account for a large part of these weight savings. The new approach is the first t .... Onset Theory: Pushing the design envelope for textile composite structures. This study aims to exploit an innovative physics-based approach to predict the strength of textile composites. This is particularly important in areas such as aircraft design, where drastic weight savings are needed to allow designers to remain competitive in a low-carbon future. Improved theory and design tools will remove conservatism and account for a large part of these weight savings. The new approach is the first to be consistent at all length scales — from atoms to aeroplanes — ensuring relevance for new and evolving composite material systems. A novel understanding of crack initiation in textile laminates is intended to reduce design and certification effort for new aircraft and help to design more efficient airframes at a lower cost.
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