Get 20M+ Full-Text Papers For Less Than $1.50/day. Start a 14-Day Trial for You or Your Team.

Learn More →

Architecture options estimate for the near-medium-haul aircraft control system by the reliability, mass and power consumption criteria

Architecture options estimate for the near-medium-haul aircraft control system by the... Abstract Current trends in increasing fuel efficiency and improving aircrafts flight characteristics place engineers before task of reducing the weight of onboard systems and decreasing power consumption with preserving required degree of reliability. In part of aircraft control system, the main stream is the actuators usage with power supply. In this article, three architecture options of the power part of the aircraft control system with different electrification levels are considered. The considered options of the power part of the control system are estimated by three criteria: reliability, mass, power consumption. The selected criteria allow for the preliminary conclusion about the prospects one or another aircraft control system architecture. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png "Aerospace Systems" Springer Journals

Architecture options estimate for the near-medium-haul aircraft control system by the reliability, mass and power consumption criteria

Download PDF
8 pages

Loading next page...
 
/lp/springer-journals/architecture-options-estimate-for-the-near-medium-haul-aircraft-4ZXLGfCOfb
Publisher
Springer Journals
Copyright
2018 Shanghai Jiao Tong University
ISSN
2523-3947
eISSN
2523-3955
DOI
10.1007/s42401-018-0017-9
Publisher site
See Article on Publisher Site

Abstract

Abstract Current trends in increasing fuel efficiency and improving aircrafts flight characteristics place engineers before task of reducing the weight of onboard systems and decreasing power consumption with preserving required degree of reliability. In part of aircraft control system, the main stream is the actuators usage with power supply. In this article, three architecture options of the power part of the aircraft control system with different electrification levels are considered. The considered options of the power part of the control system are estimated by three criteria: reliability, mass, power consumption. The selected criteria allow for the preliminary conclusion about the prospects one or another aircraft control system architecture.

Journal

"Aerospace Systems" – Springer Journals

Published: Aug 1, 2019

Keywords: Aerospace Technology and Astronautics; Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics)

References

  • Voronovich SG, Kargopolchev VD, Kutahov VV, Aviapanorama (2009) 4, pp 14–17
    Voronovich SG, Kargopolchev VD, Kutahov VV, Aviapanorama
  • Improvement of dynamic properties and study of working processes of the aircraft steering hydraulic actuator with combined speed control with increasing external load
    Alekseenkov AS
  • Control actuation systems of civil aircraft. New developments and reliability
    SA Ermakov, VI Karev, AN Mitrichenko, AM Selivanov, RV Sukhorukov
  • Actuation technology for flight control system on civil aircraft
    Xue L
  • Aerospace actuators 1: needs, reliability and hydraulic power solutions
    J-C Maré
  • Aerospace actuators 2: signal-by-wire and power-by-wire
    J-C Maré
  • Development trends for architecture of control system’s executive section in construction of modern aircraft
    SV Baikov, TB Bliznova, YG Obolenskiy
  • Actuation system design with electrically powered actuators
    Meng F
  • Design and characterization of a dual electro-hydrostatic actuator
    McCullough KR
  • Sistemy upravleniya rulyami samoletov (Aircraft control systems), Moscow, MGTU im
    Shcumilov IS
  • Sistemy distantsionnogo upravleniya magistral’nykh samoletov (Fly-by-wire control system for long-haul aircraft)
    YF Sheluhin