Side rubber of aircraft tire

A technology for aviation tires and sidewall rubber, applied in special tires, tire parts, transportation and packaging, etc., can solve the problems of carcass elongation performance decline, etc., achieve good heat resistance, high tear performance, and good processing performance effect

Active Publication Date: 2019-08-23
中国化工集团曙光橡胶工业研究设计院有限公司
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0002] The sidewall part of an aviation tire is the part with the largest lateral deformation during the use of the aviation tire, such as taxiing, take-off, and landing. Under the harsh service conditions of cyclic thermal vacuum environment and radiation, vulcanized rubber will volatilize the low molecular weight in the polymer and the volatilization of softeners, anti-aging agents and other compounding agents in vacuum, especially in thermal vacuum, due to high temperature and high energy Due to the action of radiation and certain m

Method used

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  • Side rubber of aircraft tire
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Embodiment Construction

[0040] The present invention will be described in detail below with three examples of aircraft tire sidewall rubber prepared in different proportions. The ratio of raw materials in each embodiment is shown in the table below. The modified N330 carbon black in the list is a modified N330 carbon black sold by Xinjiang Junxin Chemical Co., Ltd.

[0041] .

[0042] The performance parameters of the aviation tire sidewall rubber obtained in the above embodiments are compared with the aviation tire sidewall rubber of the prior art through testing. , has the advantages of small weight loss rate in thermal vacuum environment, good heat resistance and radiation resistance, and at the same time has good flex cracking resistance, low heat generation, high elongation at break and tensile strength, brittleness Low temperature performance characteristics. See table below.

[0043]

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Abstract

The invention belongs to the field of aircraft tires and particularly relates to side rubber of an aircraft tire. The side rubber is prepared from the ingredients in parts by weight: 30-70 parts of natural glue, 20-40 parts of ethylene propylene terpolymer rubber, 10-30 parts of cis-butadiene rubber, 40-60 parts of modified carbon black N330, 1-3 parts of paraffin oil, 1-3 parts of tackifying resin, 1-4 parts of leveler, 1-2 parts of crack preventing agent, 0.1-0.5 part of antiozonant H, 1-2 parts of p-phenylenediamine type anti-aging agent, 3-8 parts of zinc oxide, 1-4 parts of stearic acid,0.1-1 part of insoluble sulfur, 1-3 parts of vulcanizer DTDM and 1-3 parts of sulfenamide type accelerator DZ. The side rubber of the aircraft tire, disclosed by the invention, can adapt to high-temperature low-temperature diurnal-cycle thermal vacuum environments and harsh working conditions such as radiation and has more excellent property performance, i.e., heat resistance, cold resistance, ozone resistance, radiation resistance, elongation at rupture and flex cracking resistance.

Description

technical field [0001] The invention belongs to the field of aviation tires, in particular to an aviation tire sidewall rubber. Background technique [0002] The sidewall part of an aviation tire is the part with the largest lateral deformation during the use of the aviation tire, such as taxiing, take-off, and landing. Under the harsh service conditions of cyclic thermal vacuum environment and radiation, vulcanized rubber will volatilize the low molecular weight in the polymer and the volatilization of softeners, anti-aging agents and other compounding agents in vacuum, especially in thermal vacuum, due to high temperature and high energy Due to the action of radiation and certain media, chemical reactions may occur in the vulcanizate. And thus produce low-molecular volatiles, these low-molecular volatiles will sublimate under the condition of high vacuum and decompression, and the sublimation and weight loss will further cause changes in the properties of the vulcanized r...

Claims

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Application Information

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IPC IPC(8): C08L7/00C08L23/16C08L9/00C08K13/06C08K3/04C08K3/22C08K5/09B60C1/00
CPCB60C1/0025C08K2003/2296C08L7/00C08L2201/08C08L2205/035C08L23/16C08L9/00C08K13/06C08K3/04C08K3/22C08K5/09
Inventor 刘蓉俞华英吴春齐傅云翠
Owner 中国化工集团曙光橡胶工业研究设计院有限公司
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