The invention provides an autonomous heat balance aircraft tire and a preparation method thereof, and belongs to the technical field of aircraft tires. The invention provides an autonomous heat balance aircraft tire which comprises a rubber matrix and a fiber skeleton arranged in the rubber matrix, and the fiber skeleton and the rubber matrix are doped with heat conduction filler. The fiber skeleton and the rubber matrix are doped with the heat-conducting filler, so that a heat-conducting passage can be constructed in the obtained autonomous heat balance aircraft tire, and the temperature of the aircraft tire under a dynamic working condition can be effectively reduced, so that the structure of the aircraft tire is effectively improved, the service life of the aircraft tire is prolonged, and the flight safety is ensured.
本发明提供了一种自主热平衡航空轮胎及其制备方法,属于航空轮胎技术领域。本发明提供了一种自主热平衡航空轮胎,包括橡胶基体与设置在所述橡胶基体中的纤维骨架,所述纤维骨架和橡胶基体中掺杂有导热填料。本发明在纤维骨架和橡胶基体中掺杂导热填料,能够在所得自主热平衡航空轮胎中构建导热通路,进而能够有效降低航空轮胎在动态工况下的温度,从而有效改善航空轮胎的结构,延长航空轮胎的使用寿命,保证飞行安全。
Autonomous heat balance aircraft tire and preparation method thereof
一种自主热平衡航空轮胎及其制备方法
27.08.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B60C VEHICLE TYRES , Fahrzeugreifen / C08L COMPOSITIONS OF MACROMOLECULAR COMPOUNDS , Massen auf Basis makromolekularer Verbindungen / C08K Verwendung von anorganischen oder nichtmakromolekularen organischen Stoffen als Zusatzstoffe , USE OF INORGANIC OR NON-MACROMOLECULAR ORGANIC SUBSTANCES AS COMPOUNDING INGREDIENTS |
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