Linkage Infrastructure, Equipment And Facilities - Grant ID: LE120100139
Funder
Australian Research Council
Funding Amount
$350,000.00
Summary
A Hot Isostatic Press (HIP) for aerospace and biomedical component processing. This facility will provide a hot isostatic press of sufficiently large capacity to maximise production efficiencies in aerospace and biomedical applications through net shape manufacturing. The facility will be able to process small components or prototypes which will behave in a manner similar to larger scale components.
Linkage Infrastructure, Equipment And Facilities - Grant ID: LE130100165
Funder
Australian Research Council
Funding Amount
$390,000.00
Summary
Thermal and mechanical simulation laboratory for light metals. The creation of a thermal and mechanical simulation laboratory for light metals will provide the critical infrastructure needed for generating new alloys and composites. This will extend Australia's competitive advantage in the design of better alloys for expanding applications in the construction, packaging, automotive and aerospace sectors.
Linkage Infrastructure, Equipment And Facilities - Grant ID: LE110100059
Funder
Australian Research Council
Funding Amount
$500,000.00
Summary
Vacuum induction furnace for casting titanium alloys. This titanium melting facility will provide a level of investment and national strategic focus necessary to sustain Australian competitive advantage in both titanium research and the global titanium market. The facility will support cutting-edge research and support the development of new titanium products.
AM of MAX Phase parts for applications in extreme environments. This project aims to develop techniques to synthesize MAX Phase compound materials in-situ using laser additive manufacturing. The project expects to increase jet engine fuel efficiency and thrust, and to fabricate longer-lasting parts for supersonic speed applications. The expected outcomes include well-developed additive manufacturing processes to make high performance engineering components with shape complexity for extreme envir ....AM of MAX Phase parts for applications in extreme environments. This project aims to develop techniques to synthesize MAX Phase compound materials in-situ using laser additive manufacturing. The project expects to increase jet engine fuel efficiency and thrust, and to fabricate longer-lasting parts for supersonic speed applications. The expected outcomes include well-developed additive manufacturing processes to make high performance engineering components with shape complexity for extreme environment applications, and new methods to increase the 3D printability of brittle materials. This should provide significant benefits to aerospace and defense industries through solving their long standing bottleneck material and processing problems. The outcomes also enhance Australia’s manufacturing capacity.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
Theoretical model that predicts the grain size of alloys inoculated with micro- and nano- particle master alloys and cast under an external field. The aim of this project is to develop a theoretical model that predicts grain size when components are cast under the influence of external fields (electromagnetic, ultrasonic, pulsed electric current and melt shearing treatments) and with the addition of nano-particle master alloys. Refining microstructures by available master alloys is reaching a li ....Theoretical model that predicts the grain size of alloys inoculated with micro- and nano- particle master alloys and cast under an external field. The aim of this project is to develop a theoretical model that predicts grain size when components are cast under the influence of external fields (electromagnetic, ultrasonic, pulsed electric current and melt shearing treatments) and with the addition of nano-particle master alloys. Refining microstructures by available master alloys is reaching a limit and this limits further improvement in mechanical properties to meet the challenge of new applications requiring, for example, high temperature properties or light weighting (for example, use of less material). The outcomes will be a new theoretical model, validated numerical models, new casting technologies and highly refined alloys with greater than 25 per cent improvement in mechanical properties. Read moreRead less