...
【24h】

MILES M52

机译:英里M52

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

The M52 was essentially conventional in terms of its structure, the monocoque fuselage in particular following contemporary practice, using light alloy with a small amount of steel in stressed regions. The fuselage was a circular tube covered in a thick, stressed skin, and the cockpit was positioned well forward to ensure a good view, but did not go outside the fuselage lines. The entire cabin was jettisonable to improve the pilot's chances of survival in an emergency. Its windscreen was a moulded glass screen, and there was a vertically positioned Perspex screen behind. A single nosewheel retracted between the pilot's legs, the narrow-track main undercarriage retracted into wells in the lower fuselage sides, and 250 gallons (1,137 litres) of fuel was housed entirely in the fuselage.
机译:M52在结构上本质上是传统的,特别是遵循现代实践的单体外壳,在受力区域使用轻合金和少量钢。机身是一个圆管,上面覆盖着厚重的皮肤,座舱的位置很靠前,以确保视野良好,但没有超出机身线。整个机舱都可以抛弃,以提高飞行员在紧急情况下的生存机会。它的挡风玻璃是模压玻璃屏幕,后面是垂直放置的有机玻璃屏幕。飞行员的双腿之间缩进了一个前轮,窄轨主起落架缩进了机身下部的井中,整个机身中容纳了250加仑(1,137升)的燃油。

著录项

  • 来源
    《Aeroplane》 |2017年第10期|39-40|共2页
  • 作者

  • 作者单位
  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 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