Method for achieving final air gap and parallelism of a fuel injector control valve
View Patent ↗A method is provided for achieving final air gap and parallelism of a control valve of a fuel injector, the control valve having a body defining an transverse top face and including a thick disc magnetic armature having a planar transverse upper face. The method includes a) measuring the actual position from the armature upper face and the body top face and, determining the actual parallelism error between said faces; and b) ablating the armature to generate an ablated upper face parallel to the body top face, the distance from the ablated upper face to the body top face being a final air gap.
1. A method for achieving final air gap and parallelism of a control valve of a fuel injector, the control valve having a body extending about a main axis from a transverse top face to an opposed lower face and being provided with an axial hydraulic bore opening in a recess, the recess defining a chamber opening in the transverse top face, the control valve also having a spool comprising a disc magnetic armature having an axial central drilling opening at one end in a planar transverse upper face and at another end in an opposed lower face, and a stem fixed in the axial central drilling, the spool being arranged in the body in a rest position wherein, the stem is axially guided in the axial hydraulic bore, and the disc magnetic armature lies in the chamber, the planar transverse upper face being slightly recessed from the transverse top face, the method comprising:
a) measuring an actual position from the planar transverse upper face to the transverse top face, and determining an actual parallelism error between the planar transverse upper face and the transverse top face; and
b) ablating the disc magnetic armature to generate an ablated upper face parallel to the transverse top face, a distance from the ablated upper face to the transverse top face being a final air gap;
wherein the measuring comprises:
a1) determining a tilt axis and a line of greatest slope of the planar transverse upper face, the tilt axis and the line of greatest slope being perpendicular to each other, the tilt axis being a transverse axis about which the planar transverse upper face is angled;
a2) calculating a tilt height between ends of the line of greatest slope, the tilt height being a distance measured along the main axis from a highest point of the line of greatest slope to a lowest point of the line of greatest slope, the highest point being closer to the transverse top face and the lowest point being further recessed in the chamber; and
a3) dividing the tilt height in an individual ablating pass depth.
2. A method as claimed in claim 1 , wherein the ablating comprises:
b1) ablating the disc magnetic armature via successive passes of the individual depth, and generating the ablated upper face in successively ablating a plurality of parallel bands extending along the tilt axis.
3. A method as claimed in claim 2 wherein in the dividing in a3) the tilt height is of constant depth.
4. A method as claimed in claim 3 , wherein the constant depth is approximately 1 μm.
5. A method as claimed in claim 2 wherein during the ablating in b) one of the plurality of parallel bands which comprises the highest point of the line of greatest slope, is ablated several times and another one of the plurality of bands which comprises to the lowest point of the line of greatest slope is ablated only one time.
6. A method as claimed in claim 5 wherein the one of the plurality of parallel bands which comprises the highest point of the line of greatest slope is ablated as many time as the tilt height has been divided in a3).
7. A method as claimed in 1 , wherein the ablating step is performed using a picosecond or a femtosecond pulsed laser.
8. A control valve of a fuel injector, the control valve comprising:
a body extending about a main axis from a transverse top face to an opposed lower face and being provided with an axial hydraulic bore opening in a recess, the recess defining a chamber opening in the transverse top face; and
a spool comprising a disc magnetic armature having an axial central drilling opening at one end in a planar transverse upper face and at another end in an opposed lower face, and a stem fixed in the axial central drilling, the spool being arranged in the body in a rest position wherein, the stem is axially guided in the axial hydraulic bore, and the disc magnetic armature lies in the chamber, the planar transverse upper face being slightly recessed from the transverse top face;
wherein the planar transverse upper face is ablated per the following:
a) measuring an actual position from the planar transverse upper face to the transverse top face, and determining an actual parallelism error between the planar transverse upper face and the transverse top face; and
b) ablating the disc magnetic armature to generate an ablated upper face parallel to the transverse top face, a distance from the ablated upper face to the transverse top face being a final air gap;
wherein the final air gap is approximately 2 μm and the parallelism of the armature upper face and the body top face is approximately 10 μm.
9. A control valve of a fuel injector, the control valve comprising:
a body extending about a main axis from a transverse top face to an opposed lower face and being provided with an axial hydraulic bore opening in a recess, the recess defining a chamber opening in the transverse top face; and
a spool comprising a disc magnetic armature having an axial central drilling opening at one end in a planar transverse upper face and at another end in an opposed lower face, and a stem fixed in the axial central drilling, the spool being arranged in the body in a rest position wherein, the stem is axially guided in the axial hydraulic bore, and the disc magnetic armature lies in the chamber, the planar transverse upper face being slightly recessed from the transverse top face;
wherein the planar transverse upper face is ablated per the following:
a) measuring an actual position from the planar transverse upper face to the transverse top face, and determining an actual parallelism error between the planar transverse upper face and the transverse top face; and
b) ablating the disc magnetic armature to generate an ablated upper face parallel to the transverse top face, a distance from the ablated upper face to the transverse top face being a final air gap
wherein the measuring comprises:
a1) determining a tilt axis and a line of greatest slope of the planar transverse upper face, the tilt axis and the line of greatest slope being perpendicular to each other, the tilt axis being a transverse axis about which the planar transverse upper face is angled;
a2) calculating a tilt height between ends of the line of greatest slope, the tilt height being a distance measured along the main axis from a highest point of the line of greatest slope to a lowest point of the line of greatest slope, the highest point being closer to the transverse top face and the lowest point being further recessed in the chamber; and
a3) dividing the tilt height in an individual ablating pass depth.