Nozzle for skewed fuel injection
A nozzle for a fuel injector is disclosed. The nozzle may have a body having a base end, a tip end, and a central bore extending from the base end to the tip end. The nozzle may also have a sac located within the central bore at the tip end. Further, the nozzle may have an orifice located within the tip end and in communication with the sac. The orifice may be skewed at an azimuthal angle relative to a radial direction of the central bore.
1. A nozzle for a fuel injector, comprising:
a body having a base end, a tip end, and a central bore extending from the base end to the tip end;
a sac located within the central bore at the tip end; and
a plurality of orifices located within the tip end and in communication with the sac, each orifice being skewed at an azimuthal angle, which is positive relative to a radial direction of the central bore, wherein the orifices include:
a first orifice skewed at a first azimuthal angle relative to a radial direction of the central bore, and
a second orifice skewed at a second azimuthal angle relative to a radial direction of the central bore,
wherein the first azimuthal angle and the second azimuthal angle are unequal.
2. The nozzle of claim 1 , wherein the each orifice is also skewed at a zenith angle relative to the central bore.
3. The nozzle of claim 1 , wherein the first and second azimuthal angles have a magnitude of about 0 to 6 degrees.
4. A method of injecting fuel in an engine having a combustion chamber, the method comprising:
pressurizing fuel;
directing a flow of pressurized fuel through a central bore of a nozzle member to a sac, the central bore extending from a base end to a tip end;
redirecting the fuel through a first orifice to the combustion chamber in a direction skewed at a first azimuthal angle relative to a radial direction of the central bore, the first orifice being disposed within a wall at the tip end and having a conical shape; and
redirecting the fuel through a second orifice to the combustion chamber in a direction skewed at a second azimuthal angle relative to a radial direction of the central bore, wherein the first azimuthal angle is different from the second azimuthal angle.
5. The method of claim 4 further including:
redirecting the fuel through each orifice to the combustion chamber in a direction which is also skewed at a zenith angle relative to the central bore.
6. The method of claim 5 further including:
determining a direction of air swirl in the combustion chamber;
determining a pressure of the fuel flowing through the central bore; and
selecting each azimuthal angle based on the direction of air swirl and the pressure of the fuel.
7. The method of claim 6 , wherein the magnitude of each azimuthal angle is about 0 to 6 degrees.
8. The method of claim 6 , wherein the azimuthal angle of each orifice redirects fuel against the direction of air swirl when the pressure of the fuel is lower than a predetermined pressure.
9. The method of claim 6 , wherein the azimuthal angle of each orifice redirects fuel in the direction of swirl when the pressure of the fuel is higher than a predetermined pressure.
10. The method of claim 9 , wherein the predetermined pressure is about 110 MPa.
11. A fuel injector, comprising:
a body;
a needle valve element disposed within the body;
a control chamber formed within the body at a base end of the needle valve element; and
a nozzle member including:
a base end, a tip end, and a central bore extending from the base end to the tip end, the central bore being configured to slidingly receive the needle valve element;
a sac located within the central bore at the tip end of the nozzle member; and
a plurality of orifices located within the tip end and in communication with the sac, each orifice being skewed at an azimuthal angle, which is positive relative to a radial direction of the central bore, wherein the orifices include:
a first orifice skewed at a first azimuthal angle relative to a radial direction of the central bore; and
a second orifice skewed at a second azimuthal angle relative to a radial direction of the central bore, wherein the first azimuthal angle is different from the second azimuthal angle.
12. The fuel injector of claim 11 , wherein the each orifice is skewed at a zenith angle relative to the central bore.
13. The nozzle of claim 1 , wherein the first and second orifices are disposed within a wall at the tip end and at least one of the first and second orifices has a conical shape.