Electrical Machines and Power Electronics for Starter-Generators in More
Electric Aircrafts: A Technology Review
Abstract
Safety-critical power conversion systems play a major role in the
paradigm shift towards more electric aircraft (MEA) architectures. This
paper reviews the electrical machines and their power electronic systems
that are currently competing in the application of integrated
starter-generators (S/Gs) in MEA power systems. Motivated by the strict
requirements of sufficient electrical starting capability, super-high
power density and ultra-high reliability, additional considerations on
the overall system design are necessary, including the power electronic
converters (PECs) and integrated thermal designs. These aspects are
discussed not only in the light of their many benefits but also of the
challenges introduced by the continuous advancements and emerging
innovations in the power conversion technology. In achieving the MEA
goals and capitalize on all potential benefits, optimization-based
design approaches will be necessary, where the aggregation of electric
machines, PECs and the aircraft grid is considered as an integrated
system to be optimized. This review highlights the importance of these
aspects and offers a view on future perspectives and open issues.