Conception of combustion locomotive modernisation taking into account life cycle cost (lcc). A prototype will be built with full official certification & exploitation research, and the logistic chain of transit carriages will be redesigned.
Cost effective lifetime enhancement of forming tools will be achieved through the application of advanced materials and processing technologies, the design of dies and inserts, and the optimisation of forming technologies.
New bioactive nanostructured composite implant materials will be developed for human bone substitutes. Development is based on the plasma processing of ceramic nanopowders and chemical technology for the production of nanosized hydroxyapatite powders.
Development and elaboration of prototype production of multilayer packaging materials consisting of paper coated with new polymers from renewable resources.
Study of the technical conditions of polish inland and coastal waterways and its modernisation perspectives, economical analysis of transport conditions and needs. Development of environmentally friendly inland waterway and coastal ships.
Increasing the productivity and reducing energy consumption in the production process of thin sheet metals, while preserving the highest requirements regarding mechanical properties, for a variety of applications including the automobile industry.
Introduction of steel panels into ship structural designs to reduce manufacturing costs, increase internal space and increase the resistance of the structure, which improves safety in relation to environmentally hazardous cargo.
Flite2 is an extension of flite e!2419. 1/by completing the transfer of results from flite to aircraft manufacturers. 2/ by introducing new topics not considered in flite, but relevant to flight test analyses.
The datif study will develop a very durable concrete pavement without gaps. The structure will be used in airport roadways.
By improving the riveting technique and the fatigue life prediction codes, we will increase the operational life and the safety of the aircraft structure.