Low pressure fuel injector nozzle
View Patent ↗A nozzle for a low pressure fuel injector that improves the control and size of the spray angle, as well as enhances the atomization of the fuel delivered to a cylinder of an engine.
1. A nozzle for a low pressure fuel injector, the fuel injector delivering fuel to a cylinder of an engine, the nozzle comprising:
a nozzle body defining a valve outlet and a longitudinal axis;
a metering plate connected to the nozzle body and in fluid communication with the valve outlet;
the metering plate defining a nozzle cavity receiving fuel from the valve outlet;
the metering plate defining a plurality of exit cavities receiving fuel from the nozzle cavity, each exit cavity radially spaced from the valve outlet and oriented along a radial axis, each exit cavity meeting the nozzle cavity at an exit orifice; and
each exit orifice having one or more axis of symmetry, and wherein none of the one or more axis of symmetry is aligned with the radial axis.
2. The nozzle of claim 1 , wherein at least one exit orifice is triangular.
3. The nozzle of claim 1 , wherein at least one exit orifice is trapezoidal.
4. The nozzle of claim 1 , wherein at least one exit orifice is square or rectangular.
5. The nozzle of claim 1 , wherein at least one exit orifice is ellipsoidal.
6. The nozzle of claim 1 , wherein all of the plurality of exit cavities are evenly distributed along a circular pattern having a diameter greater than a diameter of the valve outlet.
7. A nozzle for a low pressure fuel injector, the fuel injector delivering fuel to a cylinder of an engine, the nozzle comprising:
a nozzle body defining a valve outlet and a longitudinal axis;
a metering plate connected to the nozzle body and in fluid communication with the valve outlet;
the metering plate defining a nozzle cavity receiving fuel from the valve outlet, the nozzle cavity defined by a side wall and a bottom wall;
the metering plate defining a plurality of exit cavities receiving fuel from the nozzle cavity, each exit cavity radially spaced from the longitudinal axis and oriented along a radial axis; and
the side wall of the nozzle cavity being positioned adjacent the plurality of exit cavities and including a series of arcuate segments to provide a tangential component to the fuel flowing into the plurality of exit cavities.
8. The nozzle of claim 7 , wherein the curvature of the arcuate segments is asymmetric relative to the radial axes.
9. The nozzle of claim 7 , wherein the curvature of the arcuate segments has a changing slope.
10. The nozzle of claim 7 , wherein the side wall and its arcuate segments define a plurality of triangularly shaped arms.
11. The nozzle of claim 10 , wherein the arms are located circunferentially between adjacent exit cavities.
12. The nozzle of claim 7 , wherein the side wall has a flower-shape.
13. The nozzle of claim 12 , wherein the pedals are oblong.
14. The nozzle of claim 7 , wherein the side wall has a radial position which varies circumferentially around the metering plate.
15. The nozzle of claim 7 , wherein the bottom wall slopes downwardly in the area proximate each exit cavity.
16. A nozzle for a low pressure fuel injector, the fuel injector delivering fuel to a cylinder of an engine, the nozzle comprising:
a nozzle body defining a valve outlet and a longitudinal axis;
a metering plate connected to the nozzle body and in fluid communication with the valve outlet;
the metering plate defining a nozzle cavity receiving fuel from the valve outlet, the nozzle cavity defined by a side wall and a bottom wall;
the metering plate defining a plurality of exit cavities receiving fuel from the nozzle cavity, each exit cavity radially spaced from the longitudinal axis and oriented along a radial axis;
each exit cavity having a frustum shape extending between an upstream end of the exit cavity and a downstream end of the exit cavity, the upstream end having a smaller diameter than the downstream end, the upstream end defining an exit orifice in communication with the nozzle cavity, each exit orifice having one or more axis of symmetry, and wherein none of the one or more axis of symmetry is aligned with the radial axis.
17. The nozzle of claim 16 , wherein the side wall is comprised of a series of arcuate segments to provide a tangential component to the fuel flowing into the plurality of exit cavities.
18. The nozzle of claim 17 , wherein the curvature of the arcuate segments is asymmetric relative to the radial axes.