发明名称 Fuel injection system for a combustion chamber
摘要 A fuel/air injector consists of an axial fuel injector (2), a coaxial Venturi tube (6) forming a pre-mix chamber (3), a divergent outlet (8) with a ring (9) for fixing to the tube (6), and an atomising air inlet. The atomising air inlet is equipped with a radial swirler (10) with a high level of permeability, situated in front of the Venturi tube (6) and providing a primary fuel/air mix. A second radial swirler with a series of channels (16a, 16b) is situated round the forward end of the tube with outlets in its convergent section to ensure a homogenous carburation of the fuel inside the tube. A third swirler (18a, 18b) is located round the rear end of the tube and has axial outlets which alternate in a circumferential direction with the radial outlets of the second swirler.
申请公布号 EP0828115(A1) 申请公布日期 1998.03.11
申请号 EP19970402058 申请日期 1997.09.04
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION SNECMA 发明人 ANSART, DENIS ROGER HENRI;LEPRETRE, GILLES GERARD CLAUDE;SANDELIS, DENIS JEAN MAURICE
分类号 F02C7/232;F23R3/12;F23R3/14;F23R3/28;F23R3/30;(IPC1-7):F23R3/14 主分类号 F02C7/232
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