TY - GEN
T1 - Design and modeling of a novel self-powered brake system for MEA
AU - Shang, Yaoxing
AU - Liu, Xiaochao
AU - Jiao, Zongxia
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/7/2
Y1 - 2017/7/2
N2 - Traditional hydraulic braking system requires lengthy and complicated pipelines, from aircraft engine driven pump (EDP) to braking actuators, which may cause serious pipeline vibration and leakage problems. This research proposes a novel integrated self-powered braking system (ISBS) for aircrafts. The new system demands no external hydraulic source, and no complicated pipelines. It can recover the kinetic energy of the landing aircraft through a hydraulic pump geared by main wheel, and serves as hydraulic power supply for the brake actuators. The new system is expected to be more economical, reliable and safer. Another notable advantage is the failure-proof braking function under conditions of emergency such as power interruption. In this paper, the working principle of the ISBS is explained. As a conclusion, this self-powered aircraft braking system provides a new solution with a great potential in the field of more-electric aircraft.
AB - Traditional hydraulic braking system requires lengthy and complicated pipelines, from aircraft engine driven pump (EDP) to braking actuators, which may cause serious pipeline vibration and leakage problems. This research proposes a novel integrated self-powered braking system (ISBS) for aircrafts. The new system demands no external hydraulic source, and no complicated pipelines. It can recover the kinetic energy of the landing aircraft through a hydraulic pump geared by main wheel, and serves as hydraulic power supply for the brake actuators. The new system is expected to be more economical, reliable and safer. Another notable advantage is the failure-proof braking function under conditions of emergency such as power interruption. In this paper, the working principle of the ISBS is explained. As a conclusion, this self-powered aircraft braking system provides a new solution with a great potential in the field of more-electric aircraft.
KW - electro-hydraulic
KW - kinetic energy recovery
KW - more-electric aircraft
KW - new braking system
UR - https://www.scopus.com/pages/publications/85047481269
U2 - 10.1109/ICIEA.2017.8283042
DO - 10.1109/ICIEA.2017.8283042
M3 - 会议稿件
AN - SCOPUS:85047481269
T3 - Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017
SP - 1316
EP - 1320
BT - Proceedings of the 2017 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 12th IEEE Conference on Industrial Electronics and Applications, ICIEA 2017
Y2 - 18 June 2017 through 20 June 2017
ER -