Study on Dimension of Landing Gear Bogie for Civil Aircraft

2019 International Conference on Advanced Electronic Materials, Computers and Materials Engineering

无线电电子学;计算机科学;材料科学

Li, Zhongjian^1 ; Mu, Tengfei^1

Shanghai Aircraft Design and Research Institute, Shanghai

201210, China^1

关键词: Civil aircrafts;    Initial design;    Rapid design;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/563/4/042042/pdf
DOI  :  10.1088/1757-899X/563/4/042042

来源: IOP

【 摘 要 】

In order to study the method on rapid design of bogie dimension for aircraft landing gear, the paper firstly clarifies the dimension definitions of landing gear bogie, then proposes four kinds of constraints which have influence on determination of landing gear bogie dimension: Expanded-tire dimension limit, clearance requirement, flotation characteristics requirement and bogie accessories dimension requirement. These four kinds of constraints form an area where can be selected to define the bogie dimension during aircraft initial design phase.