首页> 外国专利> AIR INTAKE RING FOR TURBO MACHINE COMBUSTION CHAMBER INJECTION SYSTEM AND METHOD OF ATOMIZING FUEL IN AN INJECTION SYSTEM COMPRISING SAID AIR INTAKE RING

AIR INTAKE RING FOR TURBO MACHINE COMBUSTION CHAMBER INJECTION SYSTEM AND METHOD OF ATOMIZING FUEL IN AN INJECTION SYSTEM COMPRISING SAID AIR INTAKE RING

机译:涡轮机燃烧室喷射系统的进气环和包括所述进气环的喷射系统中的燃料雾化方法

摘要

A system for improving fuel-air mixing inside an injection system of a turbomachine combustion chamber. An air intake ring has an annular deflection wall, or venturi, having an internal profile provided with a discontinuity inducing an increase in the radius (φ) of the internal profile downstream of the discontinuity. A method of atomizing fuel includes separating fuel trickling over the internal profile of the annular deflection wall from the internal profile at the level of the discontinuity so as to form droplets within a flow of air coming from an upstream air circulation space of the air intake ring.
机译:一种用于改善涡轮机燃烧室的喷射系统内部的燃料-空气混合的系统。进气环具有环形偏转壁或文丘里管,该环形偏转壁或文丘里管具有设置有不连续性的内部轮廓,从而引起该不连续下游的内部​​轮廓的半径(φ)增大。一种使燃料雾化的方法,该方法包括在不连续的位置将滴落在环形偏转壁的内部轮廓上的燃料与内部轮廓分开,以便在来自进气环上游空气循环空间的气流中形成液滴。 。

著录项

  • 公开/公告号EP3227612B1

    专利类型

  • 公开/公告日2018-09-05

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号EP20150817462

  • 发明设计人 MERY YOANN;CAYRE ALAIN RENÉ;

    申请日2015-12-02

  • 分类号F23R3/10;F23R3/14;F23R3/28;

  • 国家 EP

  • 入库时间 2022-08-21 13:18:08

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