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 circumferentially spaced exit cavities receiving fuel from the nozzle cavity, each exit cavity radially spaced from the longitudinal axis and oriented along a radial axis; and
each exit cavity having an upstream portion and a downstream portion, the upstream portion defined by a series of at least three steps, the upstream portion of each exit cavity narrowing towards the downstream portion.
2. The nozzle of claim 1 , wherein the series of steps define a series of recirculation zones.
3. The nozzle of claim 2 , wherein each recirculation zone is located on an upper surface of each step.
4. The nozzle of claim 1 , wherein the series of steps form a generally conical shape.
5. The nozzle of claim 1 , wherein each step is annular in shape.
6. The nozzle of claim 5 , wherein each step forms a square or rectangular ring-shape.
7. The nozzle of claim 1 , wherein each exit cavity defines an exit axis, each exit axis being tilted in the radial direction relative to the longitudinal axis to increase the spray angle of the nozzle.
8. The nozzle of claim 1 , wherein each exit cavity defines an exit axis, each exit axis being tilted in a plane perpendicular to the respective radial axis, each exit axis being non-parallel to the longitudinal axis to produce a swirl component to the fuel exiting the nozzle.
9. The nozzle of claim 1 , wherein each step is formed by a first surface of the exit cavity being angled relative to a second surface of the exit cavity.
10. The nozzle of claim 1 , wherein each step includes a radial surface extending radially and wherein each radial surface is located radially within the exit cavity.
11. The nozzle of claim 1 , wherein the series of steps are concentrically arranged.
12. 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 circumferentially spaced 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 an upstream portion and a downstream portion, the upstream portion defined by a series of steps, each step being formed by a first surface of the exit cavity being angled relative to a second surface of the exit cavity the upstream portion of each exit cavity narrowing towards the downstream portion; and
the metering plate including an upper surface and a lower surface, and wherein neither the first surface nor the second surface are formed by the upper or lower surfaces.
13. The nozzle of claim 12 , wherein the series of steps define a series of recirculation zones.
14. The nozzle of claim 13 , wherein each recirculation zone is located on an upper surface of each step.
15. The nozzle of claim 12 , wherein the series of steps form a generally conical shape.
16. The nozzle of claim 12 , wherein each step is annular in shape.
17. The nozzle of claim 16 , wherein each step forms a square or rectangular ring-shape.
18. The nozzle of claim 12 , wherein each exit cavity defines an exit axis, each exit axis being tilted in the radial direction relative to the longitudinal axis to increase the spray angle of the nozzle.
19. The nozzle of claim 12 , wherein each exit cavity defines an exit axis, each exit axis being tilted in a plane perpendicular to the respective radial axis, each exit axis being non-parallel to the longitudinal axis to produce a swirl component to the fuel exiting the nozzle.
20. The nozzle of claim 12 , wherein each step includes a radial surface extending radially and wherein each radial surface is located radially within the exit cavity.