The aim of this work has been to develop a robust design methodology for the sizing of an electric powered, no-bleed, environmental control system pack for More Electric aircrafts. The results of the design have been tested through virtual verification, and a one-dimensional (1D) simulation model of the entire machine has been created. Starting from the definition of the design requirements, we have proceeded with the analytical sizing, the choice of the components, the 3D digital mock-up of the machine and with the 1D simulation of the system. Finally we have executed a fluidic and thermal analysis of the heat exchangers duct.

Development of an Environmental Control System Pack simulation model for a More Electric Aircraft / Maggiore, Paolo; DALLA VEDOVA, MATTEO DAVIDE LORENZO; Pace, Lorenzo; Tosetti, Marco; Piovano, A.. - In: INTERNATIONAL JOURNAL OF MECHANICS AND CONTROL. - ISSN 1590-8844. - STAMPA. - 15:2(2014), pp. 31-35.

Development of an Environmental Control System Pack simulation model for a More Electric Aircraft

MAGGIORE, Paolo;DALLA VEDOVA, MATTEO DAVIDE LORENZO;PACE, LORENZO;TOSETTI, MARCO;
2014

Abstract

The aim of this work has been to develop a robust design methodology for the sizing of an electric powered, no-bleed, environmental control system pack for More Electric aircrafts. The results of the design have been tested through virtual verification, and a one-dimensional (1D) simulation model of the entire machine has been created. Starting from the definition of the design requirements, we have proceeded with the analytical sizing, the choice of the components, the 3D digital mock-up of the machine and with the 1D simulation of the system. Finally we have executed a fluidic and thermal analysis of the heat exchangers duct.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11583/2584959
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