System and method for cutting a passage in an airfoil
US-9776284-B2 · Oct 3, 2017 · US
US10160059B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10160059-B2 |
| Application number | US-201615059327-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 3, 2016 |
| Priority date | Mar 3, 2016 |
| Publication date | Dec 25, 2018 |
| Grant date | Dec 25, 2018 |
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A head assembly for a liquid jet guided laser system is disclosed having a coupling unit removably disposed to a laser focus optic module of the laser system. The coupling unit has a nozzle assembly removably connected to the coupling unit. The nozzle assembly has a liquid jet nozzle and a nozzle cap. The nozzle cap has a plurality of axial assist gas conduits and static assist gas conduits in fluid communication with an assist gas source extending through the nozzle cap body to individually transport assist gas to axial exit ports and static exit ports positioned to exhaust assist gas proximate the liquid jet. At least a portion of the plurality of axial assist gas conduits are partitioned from fluid communication with the liquid jet hole. A lateral movement assembly can be configured between the laser focus optic module and coupling unit.
Opening claim text (preview).
What is claimed is: 1. A head assembly for a liquid jet guided laser system comprising; a coupling unit removably disposed to a laser focus optic module of the laser system, the coupling unit comprising; a nozzle assembly removably connected to the coupling unit, the nozzle assembly defining an axial direction and radial direction and comprising a liquid jet nozzle and a nozzle cap, wherein the liquid jet nozzle is configured to form a liquid jet, the nozzle cap comprising; a nozzle cap body defining a liquid jet hole axially aligned and extending through the center of the nozzle cap body, a plurality of axial assist gas conduits and static assist gas conduits in fluid communication with an assist gas source, the plurality of axial assist gas conduits and plurality of static assist gas conduits entering the nozzle cap body through entrance ports positioned in an annular pattern concentric with the liquid jet hole and extending through the nozzle cap body to individually transport assist gas to axial exit ports and static exit ports positioned to exhaust assist gas proximate the liquid jet; and wherein at least a portion of the plurality of axial assist gas conduits are partitioned from fluid communication with the liquid jet hole. 2. The head assembly of claim 1 , wherein at least a portion of the axial exit ports are positioned to throw the assist gas at a liquid jet convergence angle θ in the range of about 10 degrees to about 40 degrees. 3. The head assembly of claim 1 , wherein at least a portion of the static exit ports are positioned for radial fluid communication with the liquid jet hole. 4. The head assembly of claim 1 , wherein the diameter of the plurality of axial assist gas conduits and the plurality of static assist gas conduits are in the range of approximately 0.005 inches to approximately 0.03 inches. 5. The head assembly of claim 1 , further comprising a diaphragm removably disposed in a diaphragm slot. 6. The head assembly of claim 5 , wherein the diaphragm is positioned perpendicular to the axial direction of the liquid jet and extends sufficient distance to block assist gas communication through the diaphragm. 7. The head assembly of claim 5 further comprising a diaphragm center hole defining an aspect ratio in the range of approximately 1:2 to 1:10. 8. The head assembly of claim 1 , wherein the coupling unit comprises a liquid for supplying an annular duct. 9. The head assembly of claim 1 , further comprising an assist gas manifold configured to supply assist gas to the plurality of axial assist gas conduits and plurality of static assist gas conduits through an annular space. 10. The head assembly of claim 1 , wherein the coupling unit comprises a window element removably disposed to the nozzle assembly. 11. A liquid jet guided laser system comprising; a lateral movement assembly configured to attach to a laser focus optic module; a coupling assembly removably attached to the lateral movement assembly wherein the lateral movement assembly allows adjusting positions of the coupling assembly in a plane perpendicular to a laser beam of the liquid jet guided laser system, the coupling assembly comprising; a nozzle assembly removably connected to a coupling unit, the nozzle assembly defining an axial direction and radial direction and comprising a liquid jet nozzle and a nozzle cap, wherein the liquid jet nozzle is configured to form a liquid jet, the nozzle cap comprising; a nozzle cap body defining a liquid jet hole axially aligned and extending through the center of the nozzle cap body, a plurality of axial assist gas conduits and static assist gas conduits in fluid communication with an assist gas source, the plurality of axial assist gas conduits and plurality of static assist gas conduits entering the nozzle cap body through entrance ports positioned in an annular pattern concentric with the liquid jet hole and extending through the nozzle cap body to individually transport assist gas to axial exit ports and static exit ports positioned to exhaust assist gas proximate the liquid jet; and wherein at least a portion of the plurality of axial assist gas conduits are partitioned from fluid communication with the liquid jet hole. 12. The laser system of claim 11 , wherein at least a portion of the axial exit ports are positioned to throw the assist gas at a liquid jet convergence angle θ in the range of about 10 degrees to about 40 degrees. 13. The laser system of claim 11 , wherein at least a portion of the static exit ports are positioned for radial fluid communication with the liquid jet hole. 14. The laser system of claim 11 , wherein the diameter of the plurality of axial assist gas conduits and plurality of static assist gas conduits is in the range of approximately 0.005 inches to approximately 0.03 inches. 15. The laser system of claim 11 , further comprising a diaphragm removably disposed in a diaphragm slot. 16. The laser system of claim 15 , wherein the diaphragm is positioned perpendicular to the axial direction of the liquid jet and extends sufficient distance to block assist gas communication through the diaphragm. 17. The laser system of claim 15 further comprising a diaphragm center hole defining an aspect ratio in the range of approximately 1:2 to 1:10. 18. The laser system of claim 11 , wherein the coupling unit comprises a liquid for supplying an annular duct. 19. The laser system of claim 11 , further comprising an assist gas manifold configured to supply assist gas to the plurality of axial assist gas conduits and plurality of static assist gas conduits through an annular space. 20. The laser system of claim 11 , wherein the coupling unit comprises a window element removably disposed to the nozzle assembly.
the fluid stream containing a liquid · CPC title
Detachable nozzles, e.g. exchangeable or provided with breakaway lines · CPC title
of liquid lasers · CPC title
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