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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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