Component geometry and method for blowout resistant welds
View Patent ↗In a method for reducing “blow-out” of annular welds for attaching components in a fuel injector, a relief region is formed on radially-facing surfaces of the components. The relief region is adjacent to a press-fit region. The components are then pressed together, and a weld is made in the relief region. A sealed gap is thereby formed in the relief region between the weld and the press-fit region. The sealed gap provides for the expansion of trapped gases that could otherwise “blow out” the liquid weld bead.
1. A method for forming a fuel injector having a fuel inlet, and fuel outlet and a fuel passageway extending from the fuel inlet to the fuel outlet along a longitudinal axis, the method comprising the steps of:
constructing a first fuel injector component comprising a radially outwardly facing annular surface;
constructing a second fuel injector component comprising a radially inwardly facing annular surface;
shaping at least one of the annular surfaces to form, when the surfaces overlap, a non-contact region having a gap between the surfaces, and a press-fit region where the first and second surfaces are in contact, the non-contact and press fit regions being adjacent;
assembling the first and second components by overlapping the annular surfaces; and
welding the annular surfaces together in the non-contact region to form an annular weld bead, the weld bead and the press-fit region bounding a substantially sealed and remaining portion of the gap.
2. The method of claim 1 , wherein the surfaces in the non-contact region are between 0.005 and 0.025 mm apart.
3. The method of claim 1 , wherein a center of the weld bead is at least 1 mm from the contact region.
4. The method of claim 1 , wherein the first fuel injector component is a pole piece and the second fuel injector component is a non-magnetic shell.
5. The method of claim 1 , wherein the step of welding the annular surfaces together comprises laser welding.
6. The method of claim 5 , wherein the step of laser welding further comprises the steps of:
rotating the assembled first and second components about a longitudinal axis; and
applying a laser welding beam.
7. The method of claim 6 , wherein the step of laser welding further comprises the steps of:
rotating the assembled first and second components at 200 RPM; and
applying a laser welding beam for 285 milliseconds at 850 Watts, then applying the laser welding beam for 45 milliseconds at 820 Watts.
8. The method of claim 1 , wherein the shaping step forms the non-contact region on a longitudinal side of the press-fit region opposite a valve body of the fuel injector.
9. A method for assembling a pole piece and a non-magnetic shell of a fuel injector, the pole piece comprising a radially outwardly facing annular surface and the non-magnetic shell comprising a radially inwardly facing annular surface, the method comprising the steps of:
forming an annular relief region on at least one of the annular surfaces;
assembling the non-magnetic shell and the pole piece with the annular surfaces overlapping; the first and second surfaces being in contact in a press-fit region, and the first and second surfaces defining a gap therebetween at the relief region;
welding an annular weld bead in the relief region, the weld bead joining the annular surfaces, the weld bead and the press-fit region bounding a substantially sealed and remaining portion of the gap.
10. The method of claim 9 , wherein the sealed portion of the gap has a volume of at least 0.037 mm 3 .
11. The method of claim 9 , wherein the surfaces in the gap are between 0.005 and 0.025 mm apart.
12. The method of claim 9 , wherein a center of the weld bead is at least 1 mm from the press-fit region.
13. The method of claim 9 , wherein the step of welding a weld bead comprises laser welding.
14. The method of claim 13 , wherein the step of laser welding further comprises the steps of:
rotating the assembled non-magnetic shell and pole piece about a longitudinal axis; and
applying a laser welding beam.
15. The method of claim 14 , wherein the step of laser welding further comprises the steps of:
rotating the assembled non-magnetic shell and pole piece at 200 RPM; and
applying a laser welding beam for 285 milliseconds at 850 Watts, then applying the laser welding beam for 45 milliseconds at 820 Watts.