Discovery Early Career Researcher Award - Grant ID: DE120102906
Funder
Australian Research Council
Funding Amount
$375,000.00
Summary
Topology optimisation for advanced engineered nanostructures. Advanced technological innovation requires extraordinary material properties, which can be generated directly from engineered nanostructures by manipulating surface plasmon resonances. The project will develop a new computational method for nanostructural design and expect to benefit aerospace, biomedical, optical and energy engineering fields.
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. Read moreRead less
Optimised flush repairs for dissimilar composite material systems. The outcome of this research project will overcome a major technological challenge when designing repairs for dissimilar composite material systems, which are being utilised at an increasing pace in a multitude of industries. This new technological capability will help to improve the competitiveness of the Australian aerospace industry.
Optimisation of self-healing repair systems in aerospace composite structures. Design and manufacture of composite structures for civilian and military aircraft is a multi-billion dollar export business for Boeing Aerostructures Australia and other Australian aerospace companies. To remain globally competitive, Australian industry must develop new expertise for next-generation composite aerostructures that are lighter, cheaper, more damage tolerant and easily repaired. Autonomic self-healing of ....Optimisation of self-healing repair systems in aerospace composite structures. Design and manufacture of composite structures for civilian and military aircraft is a multi-billion dollar export business for Boeing Aerostructures Australia and other Australian aerospace companies. To remain globally competitive, Australian industry must develop new expertise for next-generation composite aerostructures that are lighter, cheaper, more damage tolerant and easily repaired. Autonomic self-healing of composites is an innovative repair technology with many future potential applications for damaged aerostructures. This project will develop analytical tools and data to enable the Australian aerospace industry to take advantage of the economic benefits offered by self-healing repair systems in aircraft composite structures.Read moreRead less
Efficient and Robust Bi-directional Evolutionary Structural Optimisation Method for Large-scale Three-dimensional Topological Design. Structural optimisation is a process of searching for the best shape and topology of an engineering structure which will consume the least amount of material or energy. This project aims to further investigate the Bi-directional Structural Optimisation (BESO) method which has recently been proposed by the applicant's team. New algorithms will be developed to subst ....Efficient and Robust Bi-directional Evolutionary Structural Optimisation Method for Large-scale Three-dimensional Topological Design. Structural optimisation is a process of searching for the best shape and topology of an engineering structure which will consume the least amount of material or energy. This project aims to further investigate the Bi-directional Structural Optimisation (BESO) method which has recently been proposed by the applicant's team. New algorithms will be developed to substantially improve the efficiency and robustness of the BESO method. The expected outcome of the project is a simple and effective optimisation technique that can be used for the conceptual design of a wide range of engineering structures.Read moreRead less
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.Read moreRead less
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.Read moreRead less
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.Read moreRead less
Novel quantitative sizing of inaccessible and hard-to-inspect defects to address the challenges posed by innovations in airframe design. Modern unitised aircraft structures cannot be reliably inspected using traditional techniques. This project will develop new techniques to quantify defects required for this innovation in aircraft component design. This research will improve the through-life support of future metallic and composite aircraft structures and improve air safety.