Abstract

In order to facilitate the rapid drainage of airport apron in the special weather (such as heavy rain and snow), the apron is usually designed to have a certain slope. However, this slope leads to a difficult problem that chocks are not easy to take out when the airplane leave airport. In order to solve this problem, a hydraulic chocks design scheme is firstly proposed. The aircraft hydraulic chock involves two systems, which are named the slider system and the rod system Taking Boeing 737-800 as an example, this paper firstly makes reasonable assumptions. And then uses a hydraulic chocks to analyze the aircraft’s stress situation. Through the calculation and analysis of the scheme, the feasibility of the scheme is verified, it also completely solve problem that chocks are not easy to take out. At the same time, the use of the hydraulic wheel block also avoids injury to personnel and waste of time.

Details

Title
Design and Calculation Analysis on a New Type of Aircraft Hydraulic Chocks
Author
Meng Kesheng 1 ; Li, Fengyu 2 ; Xia Bin 3 ; Chen Pandeng 3 ; Lin Qizhao 2 ; Chen, Chen 4 

 AnHui Civil Aviation Airport Group, Department of Maintainance Engineering, AnHui, 230086; Department of Thermal Science and Energy Engineering, University of Science and Technology of China, Hefei, China, AnHui, 230026 
 Department of Thermal Science and Energy Engineering, University of Science and Technology of China, Hefei, China, AnHui, 230026 
 AnHui Civil Aviation Airport Group, Department of Maintainance Engineering, AnHui, 230086 
 ShenZhen Branch of China Southern Airlines, Aircraft Maintenance Plant, Shenzhen, China, 518000 
Publication year
2018
Publication date
Aug 2018
Publisher
IOP Publishing
ISSN
17578981
e-ISSN
1757899X
Source type
Scholarly Journal
Language of publication
English
ProQuest document ID
2557078807
Copyright
© 2018. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.