首页> 外文期刊>Russian Aeronautics >Influence of Combustion Chamber Geometry and Compression Ratio on the Main Parameters of a Diesel Aircraft Engine
【24h】

Influence of Combustion Chamber Geometry and Compression Ratio on the Main Parameters of a Diesel Aircraft Engine

机译:燃烧室几何形状和压缩比对柴油机发动机主要参数的影响

获取原文
获取原文并翻译 | 示例
           

摘要

This paper considers the problem of increasing the fuel efficiency of a diesel aircraft engine and decreasing the smokiness of its exhaust gases (EG) by means of the experimental determination of optimum compression ratio and combustion chamber dimensions. Necessity for matching of these parameters in a wide variation range of load and crankshaft speed was identified and proved.
机译:None

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