Abstract:
The subject of this thesis is the formatting, analysis and sizing of a metal construction of large dimensions
using the commercial design programme SAP2000 V15.
Specifically, this metal construction is an aircraft maintenance hangar based at Athens International
Airport ‘El. Venizelos’ in Spata, Attika. The building will be used for the maintenance and parking of
Dash-100 Bombardier aircrafts. It has been designed to accommodate up to 2 aircrafts at any one time. The
dimensions of the hangar were determined by the size of the aircrafts, taking into consideration also, the
necessary safety gaps required between them, and between the aircraft and the hangar. A bridgecrane is
installed for transporting various parts of the aircraft that need to be repaired or replaced.
The following chapters extensively describe the various components required in the design of the hangar,
the frame sections, the orientation of the beams as well as the static analysis of their functions.
The various load cases have been analysed based on the specifications outlined in Eurocode 1 and seismic
behaviour is based on the specifications in Eurocode 8.
Beginning the simulation, there is extensive reference to the functions of the programme SAP 2000, and
an initial approach to geometrical design of the hangar is described. We introduce the definition of the basic
parameters that relate to the materials, frame sections, joints and restraints that are involved in the
composition of the structure. By forming a three-dimensional model, the load cases and load combinations
are defined, while strength and seismic behaviour checks are carried out.
Finally, with the use of the program and its functions, the hangar doors are designed and their size is
determined. Their structure, resistance and functionality is tested and determined using various load
combinations – the arrows resulting from bending are calculated.
The specificity in the study of such a construction is due to the requirement of large openings and height
due to the dimensions of the aircraft, and the absence of internal columns for safe movement and parking
them. These geometric characteristics give the building a special sensitivity to wind loads, which are
verified and checked through the programme.