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Design of a Triple-Redundant Electromechanical Brake System Control Unit for Aerospace Application

Francesco Tola

Design of a Triple-Redundant Electromechanical Brake System Control Unit for Aerospace Application.

Rel. Paolo Maggiore, Paolo Petrini, Mario Rossano. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Elettronica (Electronic Engineering), 2022

Abstract:

In the last fifteen years, the increasingly compelling performance optimization and environmental pollution containment objectives push the aerospace industry towards the concept of Hybrid Electric Powered or More Electric Aircraft. The MEA concept aims to convert today's hydraulic and pneumatic systems to more efficient and safer electric powered ones. Brake Systems represent one of the most challenging aspects of the changeover. This thesis proposes a triple-redundant fault-tolerant Electronic Control Unit design for the MAG-PoliTO-BPR Electromechanical Brake System FreME. The work describes the device, from the hardware technical requirements derived from the system level specification, through the architecture definition, to the detailed electric scheme of the Brake System Control Unit. Focus is placed on the description of internal redundancy management mechanisms to underline the compliance with safety requirements.

Relatori: Paolo Maggiore, Paolo Petrini, Mario Rossano
Anno accademico: 2022/23
Tipo di pubblicazione: Elettronica
Numero di pagine: 237
Informazioni aggiuntive: Tesi secretata. Fulltext non presente
Soggetti:
Corso di laurea: Corso di laurea magistrale in Ingegneria Elettronica (Electronic Engineering)
Classe di laurea: Nuovo ordinamento > Laurea magistrale > LM-29 - INGEGNERIA ELETTRONICA
Aziende collaboratrici: MECAER AVIATION GROUP S.p.A.
URI: http://webthesis.biblio.polito.it/id/eprint/24640
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