TY - GEN
T1 - Analysis on the flow requirement of an aircraft hydraulic energy system
AU - Wang, Hongxin
AU - Shang, Yaoxing
AU - Li, Mingyang
AU - Jiao, Zongxia
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2016/11/17
Y1 - 2016/11/17
N2 - The composition and working principle of an aircraft hydraulic energy system were introduced, the flow and pressure requirements of hydraulic users was analyzed by combining with the normal condition for each phase of flight missions, and the selection design of main components of the pump source was completed. The flow and pressure in line with supply and demand of the hydraulic system under the normal condition was analyzed, for the subsequent design and demonstration test of aircraft hydraulic energy system provides a theoretical reference.
AB - The composition and working principle of an aircraft hydraulic energy system were introduced, the flow and pressure requirements of hydraulic users was analyzed by combining with the normal condition for each phase of flight missions, and the selection design of main components of the pump source was completed. The flow and pressure in line with supply and demand of the hydraulic system under the normal condition was analyzed, for the subsequent design and demonstration test of aircraft hydraulic energy system provides a theoretical reference.
UR - https://www.scopus.com/pages/publications/85006758085
U2 - 10.1109/AUS.2016.7748166
DO - 10.1109/AUS.2016.7748166
M3 - 会议稿件
AN - SCOPUS:85006758085
T3 - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
SP - 820
EP - 824
BT - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016
Y2 - 10 October 2016 through 12 October 2016
ER -