The invention discloses a meridian aircraft tire cap ply structure and a meridian aircraft tire, and relates to the technical field of meridian aircraft tire design and manufacturing, the meridian aircraft tire cap ply structure comprises at least two cap ply layers which are arranged in a stacked mode, and the stacked cap ply layers are arranged between upper-layer tread rubber and lower-layer tread rubber; each cap ply is formed by winding high-strength cord fabric strips in the circumferential direction at a certain angle, and the cord fabric strips of every two adjacent cap ply layers are arranged in a crossed mode. According to the meridian aircraft tire cap ply structure and the meridian aircraft tire, the conditions of puncture resistance and high-speed resistance of the aircraft tire are met, it is guaranteed that the tread can resist puncture of foreign matter on a runway, and tread faults cannot occur under the high-speed effect.
本发明公开了一种子午线航空轮胎冠带层结构及子午线航空轮胎,涉及子午线航空轮胎设计与制造技术领域,包括至少两层层叠设置的冠带层,层叠的所述冠带层设置于上层胎面胶和下层胎面胶之间,各所述冠带层均由高强力帘布条沿与周向呈一定角度缠绕而成,相邻两层所述冠带层的所述帘布条相互交叉排列。本发明提供的子午线航空轮胎冠带层结构及子午线航空轮胎,满足航空轮胎耐刺扎、耐高速的条件,保证胎面能够抵挡跑道上异物刺扎,在高速作用下不会发生胎面故障。
Meridian aircraft tire cap ply structure and meridian aircraft tire
一种子午线航空轮胎冠带层结构及子午线航空轮胎
2022-11-22
Patent
Elektronische Ressource
Chinesisch
IPC: | B60C VEHICLE TYRES , Fahrzeugreifen |
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