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Aircraft Engine Fan Blade Design: Impact Tolerance Prediction of Partially Filled 3D Printed Aluminum, Titanium, and PEEK-Filled Waste Metal Dusts

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Resource Recovery and Recycling from Waste Metal Dust

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Abstract

Cost-cutting measures are taken to reduce acquisition and operating expenses as a result of price rivalry facing airline operators. Utilizing lightweight components can help aircrafts consume less fuel, which could help cut operational expenses. While 3D-Print Technology (3D-PT) faces a hurdle of time and material loss when parameters like infill density are set to 100% for maximum tensile strength of printed components, aircraft components created using this technology are frequently strong. As a result, heavier components are created, which raises fuel consumption. It becomes crucial to establish the ideal infill density level needed to prevent plastic deformation of components made using 3D-PT. Therefore, the intended goal can be achieved by examining the impact tolerance of a 3D printed turbine component when the infill density ranges from 20% to 85%. Another suggested study looks at how employing lightweight waste metal dust, like the copper smelter dust, affects the impact resistance of 3D printed turbine components and how that affects material costs. The proposed research will offer suggestions for the best infill density for 3D printed turbine component additive manufacturing. The ideal compositional ratio of the matrix and reinforcement for the generated composite will also be suggested.

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Authors and Affiliations

  1. Department of Mechanical and Mechatronics Engineering, Faculty of Engineering and the Built environment, Tshwane University of Technology, Pretoria, South Africa

    Shade Rouxzeta Van Der Merwe & Dawood Ahmed Desai

  2. Department of Chemical, Metallurgical and Materials Engineering, Faculty of Engineering, Tshwane University of Technology, Pretoria, South Africa

    Daniel Ogochukwu Okanigbe

  3. Pantheon Virtual Engineering Solutions, Nigel, South Africa

    Daniel Ogochukwu Okanigbe

  4. Department of Mechanical Engineering, Aerospace Systems Research Group Gate, University of KwaZulu-Natal, Durban, South Africa

    Glen Campbell Snedden

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  1. Shade Rouxzeta Van Der Merwe
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  1. Department of Chemical, Metallurgical and Materials Engineering, Faculty of Engineering and the Built EnvironmentTshwane University of Technology, Pretoria, South Africa

    Daniel Ogochukwu Okanigbe

  2. Department of Chemical, Metallurgical and Materials Engineering, Faculty of Engineering and the Built Environment Tshwane University of Technology, Pretoria, South Africa

    Abimbola Patricia Popoola

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Van Der Merwe, S.R., Okanigbe, D.O., Desai, D.A., Snedden, G.C. (2023). Aircraft Engine Fan Blade Design: Impact Tolerance Prediction of Partially Filled 3D Printed Aluminum, Titanium, and PEEK-Filled Waste Metal Dusts. In: Ogochukwu Okanigbe, D., Popoola, A.P. (eds) Resource Recovery and Recycling from Waste Metal Dust. Springer, Cham. https://doi.org/10.1007/978-3-031-22492-8_10

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