Integration Design and Simulation of Hydraulic Actuated Control System of Helicopter-Reference-Cited by-同舟云学术

Integration Design and Simulation of Hydraulic Actuated Control System of Helicopter

Published:2015-07 Issue: Volume:779 Page:182-186
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Gu Feng¹,Jiang Ji Hai²,Diao Fei Meng¹,Song Yan Nan¹,Du Quan¹,Gao Lei¹,Li Yan¹,Qu Chang³

Affiliation:

1. Avic Harbin Aircraft Industry Group

2. Harbin Institute of Technology

3. Northeast Forestry University

Abstract

Hydraulic system is one of the most important parts of helicopter. Its function is to supply hydraulic power to the utilities. This paper studies an integration hydraulic system applied in helicopter flight control actuating system and simulates the system. The system has a small volume, light mass, meeting the requirements of helicopter control system actuating.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.779.182.pdf

Reference4 articles.

1. The editorial board of Aircraft Design Manual. Aircraft Design Manual. Beijing: Aviation Industry Press (2003).

2. Wang zhanlin. The high-pressure hydraulic energy system of aircraft. Beijing: Beihang University Press, (2004).

3. Zhang hongjia, Huang yi. Hydraulic transmission. Beijing: China Machine Press, (2000).

4. Li yanjun. Hydraulic drive and control of airplane. Beijing: Science Press, (2009).

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Joint optimization of mission abort and protective device selection policies for multistate systems;Risk Analysis;2022-01-15