Options of control system architectures for short-medium haul aircraft
Authors: Postnikov S.E., Trofimov A.A., Smagin D.I.
Published in issue: #12(72)/2017
DOI: 10.18698/2308-6033-2017-12-1711
Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft
One of the promising areas for the aircraft control system development is an increase in the electrification extent due to an alteration in the architecture of the control system power section. The article considers various options of the architecture of the short-medium haul aircraft control system, using drives with electric power supply, such as electrohydrostatic, combined and electromechanical steering gears. Based on go-no-go evaluation of the proposed options of the architecture of the short-medium haul aircraft control systems and subject to the requirements of the applicable aviation regulations, the most promising options were selected for the further evaluation based on a set of criteria: criteria of mass and energy perfection, dynamic performance, operating costs, etc.
References
[1] Voronovich S., Kargopoltsev V., Kutakhov V. Aviapanorama - Aviapanorama, 2009, no. 2, pp. 23-27.
[2] Volokitina E., Shalaginov V., Ovechkin O. Electronika i elektrooborudovanie transporta - Electronics and Electrical Transport, 2005, no. 5, pp. 7-9.
[3] Aviatsionnye pravila. Chast 25 (AP-23) Normy letnoy godnosti samoletov transportnoy kategorii. Razdel A-0 - "Obshchie trebovaniya letnoy godnosti samoleta pri otkazakh funktsionalnykh system [Aviation regulations. Part 25 (AP-25). The norms of transport category airplane airworthiness. Section A-0 - "General requirements for aircraft airworthiness in case of failures of functional systems"]. Moscow, MAK Publ., 2014, pp. 14-16.
[4] Certification Consideration for Highly Integrated or Complex Systems. SAEARP4754, 1996.
[5] Rukovodstvo po protsessam sertifikatsii vysokointegrirovannykh slozhnykh bortovykh system vozdushnykh sudov grazhdanskoy aviatsii R-4754 [Guidelines for the processes of certification of highly integrated complex airborne systems of civil aircraft Р4754]. Moscow, MAK Publ., 2007.
[6] Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne System and Equipment. SAEARP4761, 1996.
[7] Alekseenkov A.S. Uluchshenie dinamicheskikh svoystv i issledovanie rabochikh protsessov aviatsionnogo rulevogo gidroprivoda s kombinirovannym regulirovaniem skorosti pri uvelichenii vneshney nagruzki. Diss. ... cand. tekhn. nauk [Improvement of dynamic properties and study of working processes of the aircraft steering hydraulic gear with combined speed control at increasing external load. Cand. eng. sc. diss.]. Moscow, 2014.
[8] Ermakov S.A., Kare V.I., Mitrichenko A.N. VestnikMoskovskogo aviatsionnogo instituta - Vestnik of Moscow Aviation Institute, 2010, vol. 17, no. 3, p. 27.
[9] Lawson C.P. Fielding J.P. Actuation Technology for Flight Control System on Civil Aircraft. Cranfield University Publ., 2010.
[10] Mare J.-C. Aerospace Actuators: Needs, Reliability and Hydraulic Power Solutions. Vol. 1. Wiley-ISTE Publ., 2016.
[11] Fanliang M. Actuation System Design with Electrically Powered Actuators. MSc research thesis. Supervisor: Dr. Lawson C.P. Cranfield University. School of Engineering Publ., vol. 1, 2011.
[12] Baykov S., Bliznova T., Obolensky Yu. Nauchnyy vestnik GosNII GA - Scientific Bulletin of the State Scientific Research Institute of Civil Aviation (GosNII GA), 2013, no. 2, p. 15.