首页> 外国专利> Ventilation of a turbomachine nacelle

Ventilation of a turbomachine nacelle

机译:涡轮机机舱的通风

摘要

A jet pump type ejector for a turbomachine, including a duct through which a secondary ventilation air flow passes, and a first end of which forms an air intake and a second end of which forms an air outlet, the two nozzles for spraying a primary air flow being mounted in the duct which defines a mixer and a diffuser downstream from the nozzle, the two nozzles being parallel and adjacent to one another, the mixer including two substantially planar longitudinal walls, bottom and top respectively, connected to one another by two side walls having a semicircular cross-section, in which the radius of curvature R2 is centered on the axis of a nozzle, the center-to-center distance of the nozzles being substantially equal to Π/2 times R2 or (Π/2)R2.
机译:用于涡轮机的喷射泵式喷射器,包括第二通风空气流通过的管道,其第一端形成进气口,第二端形成出气口,这两个喷嘴用于喷射一次空气气流安装在导管内,导管在喷嘴的下游限定了一个混合器和一个扩散器,两个喷嘴是平行的并且彼此相邻,混合器包括两个基本为平面的纵向壁,底部和顶部分别通过两侧彼此连接。具有半圆形横截面的壁,其中曲率半径R2以喷嘴的轴线为中心,喷嘴的中心距基本等于π/ 2乘以R2或(Π/ 2)R2 。

著录项

  • 公开/公告号GB2529787B

    专利类型

  • 公开/公告日2020-03-25

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号GB20150022011

  • 发明设计人 SARAH CHARTIER;JEAN-CHRISTOPHE DUFFET;

    申请日2014-06-13

  • 分类号B64D33/08;B64D29;F02C7/18;F02C9/18;

  • 国家 GB

  • 入库时间 2022-08-21 11:00:05

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