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US 2006/0231065 A1Published application
Fuel injector for an internal combustion engine
AssigneeMagneti Marelli Motopropulsion France SAS
InventorMichael Pontoppidan
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AssigneeMagneti Marelli Motopropulsion France SAS
InventorMichael Pontoppidan
Estimating the term…
A fuel injector comprising a head which has a free outer face and a main orifice designed to spray a fuel jet in a main direction and a secondary orifice designed to spray a fuel jet in a secondary direction, the main and secondary orifices opening into the outer face and communicating directly with a common injection chamber which is selectively placed in communication with a supply chamber. The secondary direction forms an angle α between 10° and 80°, with the main direction so that the secondary jet intercepts the main jet in a burst zone which starts at a distance d of between 1 and 15 mm, and the flow rate of the secondary jet is between 80% and 100% of the flow rate of the main jet. The invention also relates to a spark ignition engine and to a method of manufacturing the injector.
1/ A fuel injector for spraying fuel into a combustion chamber of a spark ignition engine, comprising a head which has a free outer face and which is provided with at least one main orifice designed to spray a fuel jet in a main direction and at least one secondary orifice designed to spray a fuel jet in a secondary direction, said main and secondary orifices opening into said outer face and communicating directly with a common injection chamber which is selectively placed in communication with a supply chamber, wherein said secondary direction forms an angle α between 10° and 80°, preferably between 15° and 45°, and more preferably equal to approximately 25°, with said main direction so that said secondary jet intercepts said main jet in a burst zone which starts at a distance d, measured in said main direction from said outer face of said head, of between 1 and 15 mm, preferably between 1 and 5 mm, and wherein said flow rate of said secondary jet is between 80% and 100% of said flow rate of said main jet.
2/ The injector according to claim 1, wherein said outer face of said head comprises at least one portion having an outwardly oriented concavity into which opens a main orifice and at least one secondary orifice.
3/ The injector according to claim 2, wherein said main orifice and said secondary orifice open out perpendicularly to said outer face of said head.
4/ The injector according to claim 1, wherein said head is provided with at least two secondary orifices which are uniformly distributed around said main orifice.
5/ The injector according to claim 4, wherein said secondary orifices have secondary spray directions designed so that said secondary jets intercept said main jet at said same longitudinal position of said main direction.
6/ The injector according to claim 1, wherein said head is provided with at least two main orifices designed to spray fuel jets in divergent main directions which between them form an angle β of between 5° and 45°.
7/ The injector according to claim 6, wherein each main jet is intercepted by at least two secondary jets sprayed through secondary orifices situated around said main orifice.
8/ The injector according to claim 1, wherein said main orifice and said secondary orifice are cylindrical holes, the diameter of said secondary orifice being less than the diameter of said main orifice.
9/ The fuel injector according to claim 2, wherein said concave portion has a continuous curvature.
10/ The injector according to claim 2, wherein said concave portion is formed by at least two facets, a primary facet into which a main orifice opens and a secondary facet into which a secondary orifice opens.
11/ Use of an injector according to claim 1, with a controlled-ignition engine, wherein said injector is arranged so as to spray the fuel directly into said combustion chamber.
12/ The use of an injector according to claim 11, wherein said injector is supplied with fuel at a pressure having a peak value of between 150 and 500 bar.
13/ The use of an injector according to claim 11, wherein the spray direction of said main orifice is arranged, as a function of the geometry of said combustion chamber and of the flow of gases in said chamber, so as to obtain a fuel-air ratio of between 0.7 and 1.2 in the vicinity of said ignition control means at the moment of ignition.
14/ A method of manufacturing an injector according to claim 2, wherein said concave portion of said outer face is produced by deformation of an initially flat wall portion.
15/ A method of manufacturing an injector according to claim 3, wherein said main orifice and said secondary orifice opening out perpendicularly to said outer surface are cut by electrical discharge machining.