Simulation of a Series Double Cavity Buffer on the Landing Gear
Authors
Xu Zhang, Da Song, Wenxiu Shang, Lixun Zhang, Kunlun Wu, Yiwen Zhang, Qihe Zhang
Corresponding Author
Xu Zhang
Available Online January 2016.
- DOI
- 10.2991/ifeea-15.2016.19How to use a DOI?
- Keywords
- landing gear of helicopter; series double cavity buffer; simulation; analysis
- Abstract
Adopting high performance buffer is the foundation of the landing gear on the helicopter. Based on established models on Adams/Aircraft, a novel type of series double cavity buffer on the landing gear is investigated by dynamic simulation. Corresponding simulation and analysis are achieved, which is helpful for farther structure optimization. It is shown that compared with single cavity buffer, the series double cavity buffer can reduce effectively the acceleration, vertical force and tire force of the landing gear. Under the same condition, vertical force and tire force of the landing gear increase with the initial pressure increase of the high pressure grade buffer in the series double cavity buffer.
- Copyright
- © 2016, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Xu Zhang AU - Da Song AU - Wenxiu Shang AU - Lixun Zhang AU - Kunlun Wu AU - Yiwen Zhang AU - Qihe Zhang PY - 2016/01 DA - 2016/01 TI - Simulation of a Series Double Cavity Buffer on the Landing Gear BT - Proceedings of the 2015 2nd International Forum on Electrical Engineering and Automation (IFEEA 2015) PB - Atlantis Press SP - 88 EP - 91 SN - 2352-5401 UR - https://doi.org/10.2991/ifeea-15.2016.19 DO - 10.2991/ifeea-15.2016.19 ID - Zhang2016/01 ER -