Open AccessGenerator configuration for helicopter quadruplex electric tail rotor
Author(s) -
Booker Julian D.,
North Dominic,
Yon Jason M.,
Mellor Philip H.
Publication year - 2019
Publication title -
the journal of engineering
Language(s) - English
Resource type - Journals
ISSN - 2051-3305
DOI - 10.1049/joe.2018.8233
Subject(s) - rotor (electric) , reliability (semiconductor) , computer science , automotive engineering , generator (circuit theory) , power (physics) , reliability engineering , engineering , electrical engineering , physics , quantum mechanics
With the move to more electric aircraft (MEA), a key area of investigation is the development of commercially viable systems which are reliable, efficient, low mass, and are compatible and commensurate with the power and multiplex requirements of current and future aircraft. In rotorcraft, the pace of adopting more electric systems, to replace conventional mechanical and hydraulic ones, say, is perceived as being much lower than in fixed wing aircraft. However, recently there has been growing evidence to suggest that a quadruplex electric tail rotor (ETR) is a technically viable solution. This paper shows the methodology to support the most reliable configuration of the four independent generators required to power such a quadruplex tail rotor drive, and takes account of the failure severity due to power loss in each independent channel, target reliability setting, and supporting reliability analyses. The conclusions drawn support a particular hybrid series‐parallel configuration of generators, with identification of further work related to the gearbox reliabilities which support the reliability attainment for the configuration.