航空轮胎结构设计一般原则  

General Principles of Structure Design of Aviation Tires

作　　者：盛保信 SHENG Baoxin(Changchun Institute of Applied Chemistry,Chinese Academy of Sciences,Changchun 130022,China)

机构地区：[1]中国科学院长春应用化学研究所,吉林长春130022

出　　处：《轮胎工业》2024年第7期394-398,共5页Tire Industry

摘　　要：对航空轮胎结构设计时需要重点关注的特殊细节和注意事项进行解读,介绍包括轮胎类型和结构形式的选择、轮胎规格的命名、额定速度和速度级、负荷能力、普通航空轮胎用于直升机、轮胎标识、轮胎规格尺寸增量的确定、充气尺寸、胀大尺寸、最小允许间隙、轮胎着合直径、轮辋尺寸和胎面花纹沟等,以期对航空轮胎的结构设计者有所助益。In this paper,the special details and precautions that needed to be focused on during the design of aviation tire structures were interpreted.The selection of tire types and structural forms,tire specification designation,rated speeds and speed levels,load capability,general aviation tires used for helicopters,tire identification,determination of tire specification size increments,pneumatic dimensions,grown dimensions,minimum clearance allowance,diameter at rim,rim dimension,tread grooves and so on were introduced,which was beneficial for structural designers of aviation tires.

关 键 词：航空轮胎 结构设计 轮辋尺寸 一般原则 

分 类 号：TQ336.1[化学工程—橡胶工业] V226.8[航空宇航科学与技术—飞行器设计]