IP Library › Granted Patent US 11,179,804
Granted Patent B2
US 11,179,804 · App. 16/075,991 · Granted Nov 23, 2021

Laser machining nozzle

Inventors: Won Jae Lee (Hwaseong-si, KR); Hak Jae Lee (Gimhae-si, KR); Sung Jun Jo (Seoul, KR); Yang Jae Shin (Hwaseong-si, KR)
Assignee: HK CO., LTD.
B23K26/1476B23K26/142B23K26/38
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Quick Facts
Patent No.
US 11,179,804
App. No.
16/075,991
Granted
Nov 23, 2021
Kind
B2
Abstract

A laser machining nozzle includes: a nozzle body coupled to a machining head; and a flow path formed through the nozzle body in a longitudinal axis of the nozzle body to allow a machining-assist gas to be injected toward a workpiece therethrough while a laser beam is emitted toward the workpiece, wherein the flow path comprises a first flow path formed in a flow direction of the machining-assist gas and generating a supersonic flow of the machining-assist gas; a second flow path connected to the first flow path in the flow direction of the machining-assist gas and expanding a volume of the machining-assist gas having passed through the first flow path; and a flow path boundary defining a boundary between the first flow path and the second flow path.

Claims (27)

1. A laser machining nozzle comprising:

a nozzle body coupled to a machining head; and

a flow path formed through the nozzle body in a longitudinal axis of the nozzle body to allow a machining-assist gas to be injected toward a workpiece therethrough while a laser beam is emitted toward the workpiece,

wherein the flow path comprises:

a first flow path formed in a flow direction of the machining-assist gas and generating a supersonic flow of the machining-assist gas;

a second flow path connected to the first flow path in the flow direction of the machining-assist gas and expanding a volume of the machining-assist gas having passed through the first flow path; and

a flow path boundary defining a boundary between the first flow path and the second flow path,

wherein the first flow path comprises:

a subsonic flow-generating portion having a cross-sectional area gradually decreasing in the flow direction of the machining-assist gas from a gas inlet through which the machining-assist gas flows into the nozzle body;

a supersonic flow-generating portion connected to the subsonic flow-generating portion and having a cross-sectional area gradually increasing from the subsonic flow-generating portion in the flow direction of the machining-assist gas; and

a sonic flow boundary defining a boundary between the subsonic flow-generating portion and the supersonic flow-generating portion and allowing the machining-assist gas to be converted from a subsonic flow to a supersonic flow,

wherein a ratio (L 1 :L 2 ) of a flow path length L 1 of the subsonic flow-generating portion to a flow path length L 2 of the supersonic flow-generating portion in the flow direction of the machining-assist gas is 3:11 based on the flow direction of the machining-assist gas,

wherein, when the subsonic flow-generating portion has a diameter D 1 at the sonic flow boundary and the supersonic flow-generating portion has a diameter D 2 at the flow path boundary, D 2 /D 1 is greater than 1.7 and less than 2.0.

2. The laser machining nozzle according to claim 1 , wherein the second flow path comprises:

a first extension extending from the flow path boundary in a direction intersecting the flow direction of the machining-assist gas; and

a second extension extending from the first extension toward a flow path-terminated portion at which the second flow path is terminated.

3. The laser machining nozzle according to claim 2 , wherein the first extension is perpendicular to the flow direction of the machining-assist gas and the second extension is parallel to the flow direction of the machining-assist gas.

4. The laser machining nozzle according to claim 2 , wherein an obtuse angle is defined between the first extension and the second extension.

5. The laser machining nozzle according to claim 2 , wherein the first extension and the second extension forms an arc shape between the flow path boundary and the flow path-terminated portion.

6. The laser machining nozzle according to claim 1 , wherein the second flow path comprises a third extension extending from the flow path boundary and inclined such that a cross-sectional area of the flow path increases toward a flow path-terminated portion at which the second flow path is terminated.

7. The laser machining nozzle according to claim 1 , wherein the flow path further comprises a flow path-terminated portion at which the second flow path is terminated, and a cross-sectional area of the second flow path at the flow path-terminated portion is larger than a cross-sectional area of the first flow path at the flow path boundary.

8. The laser machining nozzle according to claim 1 , wherein the machining-assist gas supplied to the gas inlet has a pressure of 18 to 22 bar.

9. The laser machining nozzle according to claim 1 , wherein the nozzle body comprises:

a coupling portion coupled to the machining head;

a gripping portion extending from the coupling portion to have a larger cross-sectional area than the coupling portion; and

an outlet extending from the gripping portion to have a smaller cross-sectional area than the gripping portion,

the coupling portion, the gripping portion and the outlet being integrated to form a single body.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 7, 2018
From: LEE, WON JAE; LEE, HAK JAE; JO, SUNG JUN; SHIN, YANG JAE
To: HK CO., LTD.
Reel/Frame 046566/0572 →
Priority Claims (2)
KR 10-2016-0022454 · Feb 25, 2016 · national
KR 10-2017-0012904 · Jan 26, 2017 · national
Continuity (1)
Related Publication 20210138583A1 · May 13, 2021