Design and optimization of electro-hydraulic self-powered braking system

被引：0
|
作者：
Liu X. [1 ,3 ,4 ]
Jiao Z. [2 ,3 ,4 ]
Shang Y. [2 ,3 ,4 ]
Zhang H. [2 ]
Wang X. [2 ]
Li D. [2 ]
机构：
[1] Research Institute for Frontier Science, Beihang University, Beijing
[2] School of Automatic Science and Electrical Engineering, Beihang University, Beijing
[3] Ningbo Institute of Technology, Beihang University, Ningbo
[4] Science and Technology on Aircraft Control Laboratory, Beijing
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2021年 / 42卷 / 06期
关键词：
Aircraft hydraulic brake system; Energy recovery; Energy taking mechanism; On-off valve brake; Self-powered brake;
D O I：
10.7527/S1000-6893.2020.24509
中图分类号：
学科分类号：
摘要：
At present, the traditional aircraft hydraulic brake system typically uses the centralized airborne hydraulic source as the power, which is transmitted to the brake actuator through the energy pipeline. With many parts and components and complex pipeline layout, the system has many problems, such as pipeline vibration and hydraulic oil leakage, limiting the improvement of reliability and maintainability of the system. In recent years, a new principle for aircraft electro-hydraulic self-powered braking system has been proposed. The modular "self-powered device" is installed near the wheel to recover the rotational kinetic energy of wheel landing and convert it into the hydraulic energy for braking. In this paper, a special mechanism using the wave curved surface for energy taking is proposed, which breaks through the stalemate with the design of a special energy taking mechanism for the self-powered system. A fully self-powered brake system principle prototype with the features of high reliability, low energy consumption, and anti-pollution is developed. Even if the aircraft loses all power, it can still effectively brake the plane. In addition, the anti-pollution level is upgraded from NAS6 to NAS10. The Integrated Self-powered Brake System (ISBS) is demonstrated to be better than the traditional hydraulic brake in terms of reliability and maintainability. © 2021, Beihang University Aerospace Knowledge Press. All right reserved.
引用
收藏
相关论文
共 21 条
  • [1] GARCIA A, CUSIDO J, ROSERO J A, Et al., Reliable electro-mechanical actuators in aircraft, IEEE Aerospace and Electronic Systems Magazine, 23, 8, pp. 19-25, (2008)
  • [2] RODIN E Y, TUNAY I, BECK A A, Et al., Modeling and robust control design for aircraft brake hydraulics, IEEE Transactions on Control Systems Technology, 9, 2, pp. 319-329, (2001)
  • [3] FURUSHO J, SAKAGUCHI M, TAKESUE N, Et al., Development of ER brake and its application to passive force display, Journal of Intelligent Material Systems and Structures, 13, 7, (2002)
  • [4] TRENTIN A, ZANCHETTA P, WHEELER P, Et al., Power flow analysis in electro-mechanical actuators for civil aircraft, IET Electric Power Applications, 5, 1, pp. 48-58, (2011)
  • [5] ORTEGA J A, ROSERO J A, ALDABAS E, Et al., Moving towards a more electric aircraft, IEEE Aerospace and Electronic Systems Magazine, 22, 3, pp. 3-9, (2007)
  • [6] JONES R I., The more electric aircraft-assessing the benefits, Journal of Aerospace Engineering, 216, 5, pp. 259-269, (2002)
  • [7] PARK E J, STOIKOV D, FALCAO D L, Et al., A performance evaluation of an automotive magnetorheological brake design with a sliding mode controller, Mechatronics, 16, 7, pp. 405-416, (2006)
  • [8] ZHANG M, NIE H, WEI X H, Et al., Modeling and simulation of aircraft anti-skid braking and steering using co-simulation method, The International Journal for Computation and Mathematics in Electrical and Electronic Engineering, 28, 6, pp. 1471-1488, (2009)
  • [9] KARAKOC K, PARK E J, SULEMAN A, Et al., Design considerations for an automotive magnetorheological brake, Mechatronics, 18, 8, pp. 434-447, (2008)
  • [10] ALLEGRE A L, BOUSAYROL A, DELARUE P, Et al., Energy storage system with supercapacitor for an innovative subway, IEEE Transactions on Industrial Electronics, 57, 12, pp. 4001-4012, (2010)
123