首页> 外文期刊>Journal of Minerals and Materials Characterization and Engineering >Development of Iron Based Brake Friction Material by Hot Powder Preform Forging Technique used for Medium to Heavy Duty Applications
【24h】

Development of Iron Based Brake Friction Material by Hot Powder Preform Forging Technique used for Medium to Heavy Duty Applications

机译:中型至重型应用的热粉预成型锻造技术开发铁基制动摩擦材料

获取原文
           

摘要

A promising friction material, Iron -based friction material, was prepared by powder metallurgy (PM) processing utilizing hot powder preform forging (near net-shape).The preparation of the product and its characterization are presented in this paper. These products are useful in heavy duty Military Aircraft applications such as AN-32. In order to eliminate costly environmental control systems to protect products during their high temperature processing (as is conventionally practiced employing hydrogen gas), the present investigation relies on carbon (mixed in the brake pad formulation) as reducing agent and high temperature oxidation resistant glassy coating (separately developed) applied over the product’s surface after cold compacting. After conducting an initial characterization such as hardness, density and Pin-on Disc tests, the samples were tested in sub-scale dynamometer under Rejected Take Off conditions. It was observed that the obtained density in the present investigation is higher than the reported density obtained by sintering route, and wear is on the lower side of the range as per the Aeronautical Standards. Optical metallography was used to investigate the microstructure of friction, interface and backing layer. It was observed that the distribution of ingredients in matrix was homogeneous. The results also indicate that the coefficient of friction is more stable, and wear is lower with respect to temperature rise. .
机译:通过粉末冶金(PM)工艺,利用热粉末预成型件锻造(近净形)制备了一种有前途的摩擦材料铁基摩擦材料。本文介绍了该产品的制备及其表征。这些产品可用于重型军用飞机应用,例如AN-32。为了消除用于在高温处理过程中保护产品的昂贵的环境控制系统(按照惯例,通常使用氢气进行保护),本研究依靠碳(混合在刹车片配方中)作为还原剂和耐高温氧化的玻璃涂层(单独开发)冷压后涂在产品表面上。在进行了诸如硬度,密度和销钉盘测试之类的初始表征之后,在“不合格起飞”条件下,使用小规模测力计对样品进行了测试。据观察,在本研究中获得的密度高于通过烧结路线获得的报告密度,并且按照航空标准,磨损在该范围的下侧。光学金相学用于研究摩擦,界面和衬里层的微观结构。观察到基质中成分的分布是均匀的。结果还表明,相对于温度升高,摩擦系数更稳定,磨损更低。 。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号