Comprehensive approach to comparative efficiency evaluation of HPS for helicopters
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 30 September 2014
Abstract
Purpose
The purpose of the work is to carry out analysis of the possibilities and estimation of electric drive efficiency for rotors of helicopter propulsion systems (PS).
Design/methodology/approach
Methodology and comprehensive multidisciplinary technology for efficiency estimation of conventional and unconventional architectures PS on rotorcraft system level at preliminary design phase were developed.
Findings
Application of the approach allow to carry out analysis of hybrid (based on gas turbine and piston engines) and full electrical PS for superlight-, light- and medium-size helicopters.
Practical implications
It was shown what level of electrical technologies improvement may provide positive effect of the using of hybrid and full electrical helicopter PS of different architectures.
Originality/value
Close matching of helicopter and engine design and calculation aspects, as well as possibilities to use the external (experimental) performances of engine components, whole PS and helicopter aerodynamic performance, are the distinctive features of proposed technology and methodology.
Keywords
Citation
Zakharchenko, V. and Lukovnikov, A. (2014), "Comprehensive approach to comparative efficiency evaluation of HPS for helicopters", Aircraft Engineering and Aerospace Technology, Vol. 86 No. 6, pp. 575-583. https://doi.org/10.1108/AEAT-06-2014-0091
Publisher
:Emerald Group Publishing Limited
Copyright © 2014, Emerald Group Publishing Limited