Author
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Miłosz Balon
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University
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University of Bielsko-Biała, Poland
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The work is comprised of a descriptive and a design part. The descriptive part comprises information regarding the designed structure and a detailed account of its constituent elements. Additionally, it provides fundamental data regarding the types of helicopters that will be utilized at the designed helipad. The design part presents the methodology used in the calculation of the landing pad structure. The calculations were performed using the Dlubal RFEM 6 program, which utilized the finite element method to create a calculation model. Following the dimensioning of the structure, a BIM model of the designed landing pad was created using the Tekla Structures software. Finally, the work also includes drawings of the structure, based on the previous calculations.