首页> 美国政府科技报告 >STUDY AND PRELIMINARY DESIGN OF A HIGH TEMPERATURE AIRCRAFT WHEEL, BRAKE, AND TOE ASSEMBLY
【24h】

STUDY AND PRELIMINARY DESIGN OF A HIGH TEMPERATURE AIRCRAFT WHEEL, BRAKE, AND TOE ASSEMBLY

机译:高温飞机轮,制动器和轮组件的研究与初步设计

获取原文

摘要

Design of a wheel, brake, and tire capable of operating from an ambient temperature of 800°F appears feasible. However, there are many areas which necessitate intensified study. Most prominent are mechanical tire approaches, bearings and lubricants, and hydraulic or pneumatic dynamic seals.nThe mechanical tire, and tread material, is the most revolutionary and challenging region to be conquered. Various mechanical tire approaches were herein considered. Designs utilizing spring configurations were more acutely investigated. Initial studies indicate that a mechanical tire possessing a spring configuration will involve a considerable weight penalty in comparison to the conventional wheel and casing presently being used for low temperature applications.

著录项

  • 作者

    Gilbert T. Stout;

  • 作者单位
  • 年度 1959
  • 页码 1-92
  • 总页数 92
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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