Spray pattern control with angular orientation in fuel injector and method
AssigneeSiemens VDO Automotive Corporation
InventorWilliam Peterson
Life of this patent
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AssigneeSiemens VDO Automotive Corporation
InventorWilliam Peterson
Estimating the term…
Metering components of a fuel injector that allow spray targeting and distribution of fuel to be configured using non-angled or straight orifice having an axis parallel to a longitudinal axis of the fuel metering components. Metering orifices are located about the longitudinal axis and defining a first virtual circle greater than a second virtual or bolt circle defined by a projection of the sealing surface onto the metering disc so that all of the metering orifices are disposed outside the second virtual or bolt circle within one quadrant of the circle. A channel is formed between the seat orifice and the metering disc that allows the fuel injector to generate a spray pattern along the longitudinal axis that forms a flow area on a virtual plane transverse to the longitudinal axis. The fuel injector of the preferred embodiments can be calibrated to an angular position about the longitudinal axis to achieve a desired targeting of a flow area and desired flow area distribution and atomization of the fuel injector. A method of targeting the fuel flow area is also provided.
1-11. (Canceled)
12 A method of targeting fuel flow area with a fuel injector having housing enclosing a passageway extending between an inlet and outlet along a longitudinal axis, a seat and a metering disc proximate the outlet, the seat having a sealing surface facing the inlet and forming a seat orifice, a terminal seat surface spaced from the sealing surface and facing the outlet, a first channel surface generally oblique to the longitudinal axis and disposed between the seat orifice and the terminal seat surface, a closure member disposed in the passageway in one position to occlude the passageway and in another position to permit fuel flow through the passageway and the seat orifice, the metering disc including at least two metering orifices, the method comprising:
13 The method of claim 12, wherein the locating of the metering orifices comprises generating a generally conical spray pattern of the fuel flow path along the longitudinal axis as a function of one of a first arcuate spacing and an aspect ratio of the at least two metering orifices, a size of the conical spray pattern being defined by an included angle of the outer perimeter of the conical spray pattern downstream of the fuel injector, and the aspect ratio being generally equal to approximately a length of each metering orifice between the second channel and outer surfaces of the metering disc divided by approximately the largest distance perpendicular to the longitudinal axis between any two diametrical inner surfaces of each metering orifice.
14 The method of claim 13, wherein the generating comprises one of:
15 The method of claim 14, wherein the included angle comprises an angle between approximately 10 to 25 degrees, and a first arcuate spacing comprises a distance of at least approximately equal to the distance between the second and outer surfaces of the metering disc.
16 The method of claim 13, wherein the generating comprises changing the cone size by one of:
17 The method of claim 14, wherein the flowing comprises generating at least two vortices disposed within a perimeter of each of the at least two metering orifices such that atomization of the flow path is enhanced outward of each of the at least two metering orifices.
18 The method of claim 12, wherein the flowing of fuel comprises configuring the first channel surface between an inner edge at approximately a first distance from the longitudinal axis and at approximately a first spacing along the longitudinal axis relative to the metering disc and an outer edge at approximately a second distance from the longitudinal axis and at approximately a second spacing from the metering disc along the longitudinal axis, such that a product of the first distance and first spacing is generally equal to a product of the second distance and second spacing.
19 The method of claim 18, wherein the second distance is located at an intersection of a plane transverse to the longitudinal axis and the channel surface such that the intersection is at least 25 microns radially outward of the perimeter of a metering orifice.
20 The method of claim 12, wherein the flowing of fuel comprises distributing fuel substantially across a flow area on the virtual plane at least 50 millimeters from an outer surface of the metering disc along the longitudinal axis.
21 The method of claim 12, wherein the orientating comprises: