Debris diverter shield for fuel injector
View Patent ↗A tubular debris shield and diverter mounted in a high pressure flow passage within a fuel injector, provide the dual functions of passing the main flow of high pressure fuel with large debris particles to relatively large discharge openings, such as the injector spray holes, while allowing some high pressure fuel to flow through a multitude of very small transverse holes to a sensitive hydraulic component, such an injector control valve circuit. In one embodiment, the tube has a wall thickness in the range of about 0.1 to 0.5 mm at least about 2000 holes with a diameter in the range of about 20 to 30 microns.
1. A fuel injector comprising:
an elongated body having upper and lower ends, a longitudinal bore leading to an injector valve seat adjacent the lower end and to a tip with discharge holes at the lower end;
an injector valve reciprocable in said bore, having a lower end sealable against the injector valve seat and an upper end subject to fluid pressure in an injector control chamber;
a control valve with an upstream side in fluid communication with said injector control chamber and a downstream side in fluid communicating with a low pressure sump;
a high pressure fuel supply passage in the body, in fluid communication with said bore upstream of the injector valve seat, and a branch line from the high pressure passage in fluid communication with said injector control chamber and with the upstream side of said control valve;
an actuator for selectively closing and opening the control valve, whereby when the control valve is closed high pressure fuel in said control chamber urges the injector valve against the injector valve seat to prevent flow of high pressure fuel from said bore to the discharge holes and when the control valve is opened the control chamber is fluidly connected with the low pressure sump, thereby reducing the fluid pressure in the control chamber and on the upper end of the injector valve, lifting the injector valve off the injector seat and discharging fuel through the discharge holes;
a debris shield in the high pressure fuel supply passage upstream of said branch line, comprising a tube fixed to the body, with a central passage aligned with the fuel supply passage and a tube wall with a multiplicity of individual radial bore holes passing entirely through the tube wall;
wherein the body comprises an upper portion containing the control valve and an upper portion of the fuel supply passage, a lower portion containing the injector valve and a lower portion of the fuel supply passage, and a distinct central portion having upper and lower surfaces rigidly trapped between the upper and lower portions of the body and a shield chamber fluidly connecting the upper and lower portions of the fuel supply passage;
wherein the debris shield is situated in the shield chamber; and
wherein the tube has opposed ends extending from the upper to the lower surface of the central portion of the body, and the tube is fixed to the body in longitudinal compression between the upper and lower portions of the body, by compressive engagement with the lower surface of the upper portion and compressive engagement with the upper surface of the lower portion.
2. The injector of claim 1 , wherein the debris shield is situated in a shield chamber in the body, and the shield chamber is defined by a shield chamber wall spaced radially from the tube.
3. The injector of claim 1 , wherein the tube has opposed ends and the tube is fixed to the body at the ends.
4. The injector of claim 1 , wherein the shield chamber is defined by a shield chamber wall spaced radially from the tube.
5. The injector of claim 1 , wherein
said branch line leads from the shield chamber to a first (Z) orifice which delivers fuel to a first passage leading to the injector control chamber;
a second (A) orifice is provided between the first passage and a second passage leading to the control valve; and
the branch line and first and second orifices are in the central portion of the body.
6. The injector of claim 1 , wherein
the shield chamber is defined by a shield chamber wall spaced radially from the tube and including a collection gallery; and
the branch line extends from the collection gallery into the central body portion.
7. The injector of claim 5 , wherein
the shield chamber is defined by a shield chamber wall spaced radially from the tube and including a collection gallery; and
the branch line extends from the collection gallery into the central body portion.
8. The injector of claim 7 , wherein
the upper portion of the fuel supply passage and the tube are coaxially aligned at the upper surface of the central portion of the body, along a first axis that is parallel to and laterally offset from the bore;
fuel from the upper portion of the fuel supply passage must pass through the holes and gallery before flowing to said branch line;
the gallery extends to the lower surface of the central portion of the body;
the branch line extends from the lower surface of the central portion of the body from the gallery at an oblique upward angle toward the axis of the bore;
said first passage terminates within the central portion of the body between the first and second orifices and is oriented along an axis from the injector control chamber obliquely upward toward the upper portion of the fuel supply passage.
9. The injector of claim 1 , wherein the holes have a diameter less than 50 microns.
10. The injector of claim 9 , wherein the holes have a diameter less than 25 microns.
11. The injector of claim 1 , wherein the tube has a length in the range of 3-4 mm, said wall has a thickness in the range of 0.1 to 0.5 mm, and the tube has at least 2000 holes with a diameter in the range of 20 to 30 microns.
12. The injector of claim 1 , wherein high pressure fuel for injection passes axially through the tube and all high pressure fuel from the central passage delivered to the upstream side of the control valve passes entirely through the radial bore holes in the tube wall before delivery to the control valve.
13. The injector of claim 12 , wherein
the tube is situated in a shield chamber having a gallery outside the tube for accumulating fuel that has passed through the holes;
all the high pressure fuel for injection passes axially through the tube and all the high pressure fuel to the upstream side of the control valve passes from the gallery through at least one orifice.
14. The injector of claim 13 , wherein the control valve has a pintle that is actuated by a solenoid to seal against and lift from a seat with a minimum lift and the diameter of the holes in the tube is smaller than said minimum lift.
15. The injector of claim 12 , wherein the holes have a diameter of less than 0.025 mm.
16. The fuel injector of claim 1 , wherein the control valve has a pintle that is actuated by a solenoid to seal against and lift from a seat with a minimum lift, and the diameter of the holes in the tube is smaller than the minimum lift.