首页> 外国专利> PERFORMANCE IMPROVEMENT STRUCTURE OF A LARGE-CAPACITY AIR COMPRESSOR WITH A SLIT BROWING ON SUCTION DUCT

PERFORMANCE IMPROVEMENT STRUCTURE OF A LARGE-CAPACITY AIR COMPRESSOR WITH A SLIT BROWING ON SUCTION DUCT

机译:抽气管道上带凹痕的大容量空气压缩机的性能改进结构

摘要

It relates to the performance improvement structure of a large-capacity air compressor that applies a slit blowing to the suction passage, In a large-capacity air compressor that supplies air sucked through the suction duct to the impeller of the compression unit, a slit is formed around the outer periphery of the suction duct and high-pressure air is supplied to the slit to generate low-speed flow within the boundary layer of the suction duct. Through technology configuration that activates the area up to the speed of the outer area of the boundary It is possible to greatly improve the compression efficiency of a large-capacity air compressor by activating the low-speed flow area inside the boundary layer permanently occurring upstream of the compression unit without a separate additional device for activating the boundary layer flow or a risk of failure.
机译:本发明涉及对吸入通道施加狭缝吹气的大容量空气压缩机的性能改进结构,在将通过吸入管道吸入的空气供应到压缩单元的叶轮的大容量空气压缩机中,狭缝为围绕吸入管的外周形成的高压空气被提供给狭缝,以在吸入管的边界层内产生低速流动。通过激活达到边界外部区域速度的区域的技术配置,可以通过激活永久存在于边界上游的边界层内部的低速流动区域,来大大提高大容量空气压缩机的压缩效率。压缩单元没有单独的附加装置来激活边界层流动或发生故障的风险。

著录项

  • 公开/公告号KR102150374B1

    专利类型

  • 公开/公告日2020-09-01

    原文格式PDF

  • 申请/专利权人 DAEJOO MACHINERY CO. LTD.;

    申请/专利号KR20190104848

  • 发明设计人 김희동;이재형;

    申请日2019-08-27

  • 分类号F04D29/68;F04D17/12;F15D1/06;

  • 国家 KR

  • 入库时间 2022-08-21 11:03:54

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

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