Abstract
A welding torch using a shielding gas includes a diffuser and an external nozzle integrated or fastened to an insulator and a welding tip fastened to the diffuser. The welding torch includes: the amplification nozzle installed as an inner nozzle part and an outer nozzle part on the upper and lower parts of gas outlets of the diffuser. The inner nozzle part is installed to be inclined on the welding tip, and the external nozzle is partially or entirely opened.
Claims
1. A welding torch using a shielding gas comprising a diffuser and an external nozzle integrated or fastened to an insulator and a welding tip fastened to the diffuser, wherein the welding torch includes: the amplification nozzle installed as an inner nozzle part and an outer nozzle part on the upper and lower parts of gas outlets of the diffuser, the inner nozzle part is installed to be inclined on the welding tip, the external nozzle is partially or entirely opened.
2. The welding torch of claim 1, wherein through additional pipelines installed on the open parts opening a part or all of the external nozzle, the welding torch supplies cooling gas separately instead of introduced air.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0024] FIG. 1 is a separate perspective view of a welding torch provided with an amplification nozzle of shielding gas according to an embodiment of the present invention.
[0025] FIG. 2 is a cross-sectional view of FIG. 1 when combined.
[0026] FIG. 3 is a real picture of the welding torch shown in FIG. 1.
[0027] FIG. 4 is a separate perspective view of a general GMAW welding torch.
[0028] FIG. 5 is a variety of embodiments a, b, and c of the external nozzle of a welding torch provided with an amplification nozzle of shielding gas according to an embodiment of this present invention.
[0029] FIG. 6 is a separate perspective view of a welding torch in which a gas guide line is formed in inner nozzle part of an amplification nozzle of shielding gas according to an embodiment of this present invention.
[0030] FIG. 7 is a illustration showing uneven gas flow when using existing external nozzle.
[0031] FIG. 8, FIG. 9 are illustrations showing problems caused by external air inflow and spatter attachment when using existing external nozzle.
[0032] FIG. 10 is a illustration showing problems caused by eccentricity when using existing external nozzle.
[0033] FIG. 11 is a illustration showing the role of shielding the external wind caused by shielding gas and external air when using a welding torch equipped with a amplification nozzle of shielding gas according to an embodiment of this invention.
[0034] FIG. 12 is a illustration of the Coanda effect of air flowing through the nozzle along the curved surface.
DETAILED DESCRIPTION
[0035] Hereinafter, embodiments of this present invention will be described in detail by referring to the attached drawings so that those having ordinary skill in the art may easily implement this present invention. However, this present invention may be implemented in various different forms and is not limited to the embodiments described herein.
[0036] The basic principle of this present invention is to use the Coanda effect, a flow phenomenon that flows along a curved surface, and since the pressure near the high-speed fluid flows is low, the surrounding fluid is drawn into this flow and the flow rate increases, therefore it uses the principle of decreasing the dynamic pressure and increasing the static pressure of the flow rate by increasing the cross-sectional area of the flow path, and is characterized by consisting of an amplification nozzle of shielding gas and an inclination surface (Coanda Surface).
[0037] For example, from FIG. 12 if Ps' air passes through the nozzle and flows at high speed along the curved surface due to the Coanda effect, the pressure is lower and the flow rate of Qadd is absorbed, and as the cross-sectional area increases, the speed decreases and the pressure increases.
[0038] It has been studied and patented in various ways using the above principles: Air Supercharger for Engines (Korean Patent Rejection, 1020070044550)—quote: U.S. Patent Publication No. 5402938, Internal Combustion Engine (Korean Patent Registration, 1020070086730), Turbocharger (Korean Patent Registration, 1020070086731), Fluid Amplifier (Korean Patent Registration, 1020100044071), Fan without Wings (Korean Patent Registration, 1020117006901), etc.
[0039] The configuration of a welding torch with an amplification nozzle and an inclination surface (Coanda Surface) in accordance with this present invention will be described in detail with reference to the attached drawings as follows.
[0040] As shown in FIG. 1 or FIG. 2, the welding torch of this present invention includes a diffuser (120) and an external nozzle (140) integrated or fastened to an insulator (110) and a welding tip (130) fastened to the diffuser (120), wherein the welding torch includes: the amplification nozzle (200) is installed as an inner nozzle part (210) and an outer nozzle part (220) on the upper and lower parts of gas outlets (121) of the diffuser (120), the inner nozzle part (210) is installed to be inclined on the welding tip (130), the external nozzle (140) is partially or entirely opened, wherein the welding torch is characterized by the shielding gas from the gas outlets (121) of the diffuser (120) increases of velocity and decreases of pressure while passing through the amplification nozzle (200), so that it absorbs surrounding air, and joins the external air introduced through the open parts (141) of the external nozzle (140) to increase the total flow rate, and as the total flow rate continues along the inclination surface (Coanda Surface) where the cross-section increases, the dynamic pressure i.e. velocity decreases and the static pressure increases due to the Coanda effect, therefore the total flow rate continues along the guide part, and so by straightness toward the welding parts is secured, the total flow rate surrounds uniformly the circumference of the welding parts at the end of the welding tip (130) and forms stably a thick shielding gas layer with the flow rate and the pressure more increasing than the shielding gas from the gas outlets (121) of the diffuser (120), wherein the welding torch serves to enable work even in a windy external environment.
[0041] In addition, the inner nozzle part (210) and the outer nozzle part (220) of the amplification nozzle (200) through which the shielding gas flows, and the inner surface of the external nozzle (140) are selectively formed with straight or spiral gas guidelines, thereby making the flow of the shielding gas more stable and laminar, and maintaining the flow of the shielding gas for a longer time at the welding parts, so that it is possible to maximize the effectiveness of the same shielding gas flow rate. As shown in FIG. 6, the gas guideline may be formed in an engraved shape or a protruding embossed shape, and may be designed in consideration of operator's convenience of use. In addition, when the effect of the spiral gas guideline is maximized, spatters generated at the welding parts do not bounce toward the welding tip but bounce out of the circumference due to a whirlwind effect.
[0042] As shown in FIGS. 1 and 2, the external nozzle (140) is constituted such that when the shielding gas from the gas outlets (121) of the diffuser (120) increases of velocity while passing through the amplification nozzle (200), its main function unlike the prior can be limited to a function only as an insulating guide in consideration of safety. However, depending on the type of shielding gas and welding conditions, the external nozzle (140) of a certain portion corresponding to the inclination surface (Coanda Surface, 212) of the inner nozzle part (210) may be sealed.
[0043] Also, as shown in FIG. 5 a, b and c, the external nozzle (140) of this present invention may be constituted in several different shapes.
[0044] FIG. 5a shows a shape in which all of it are opened to maintain only a cylindrical frame for insulation, FIG. 5b shows a linear shape alternating opening and closing, and FIG. 5c shows a shape with multiple openings in several places, wherein the open parts (141) of it can be formed fully as well as partially as shown in FIG. 1 and so like the existing external nozzle shape, all shapes efficient for work such as some tapered shapes will be possible.
[0045] In addition, the welding torch can use gas for a variety of purposes such as cooling gas (e.g. nitrogen gas) separately through additional pipelines installed on the open parts (141) opening a part or all of the external nozzle (140) instead of introduced air. When using the heterogeneous gas as described above, attention should be paid to each flow rate, pressure, and external nozzle shape together with the shielding gas.
[0046] As shown in FIG. 1 or FIG. 2, the amplification nozzle (200) includes an inner nozzle part (210) and an outer nozzle part (220) which are installed on the upper and lower parts of gas outlets (121) of the diffuser (120), and the inner nozzle part (210) is installed to be inclined (inclination surface, Coanda Surface, 212) on the welding tip (130), wherein when unfolded (or opened), it looks like a fan-shaped (or fanwise), and as one embodiment it may be configured as an integral type or a separate type, and is made up of a thin plate metal with spring force to facilitate fastening and separating from the diffuser (120) and the welding tip (130) so that the operator can easily attach and detach it, and to adjust the gap (214) between the inner nozzle part (210) and the outer nozzle part (220), the protrusions (215) on the inner nozzle part (210) can be positioned at regular intervals on the cylinder. Locking grooves (122, 123) are formed on the diffuser (120), and ends of the inner nozzle part (210) and the outer nozzle part (220) are manufactured in a hemispherical shape so as to be positioned in the locking grooves (122, 123). The gap (214) is preferably 0.2 to 2.0 mm for general vehicle and heavy equipment welding with a current of 600 A or less. Although the gap (214) may vary depending on the type of shielding gas and welding conditions, it becomes an important factor in determining the total flow rate surrounding the welding parts by introducing the surrounding air.
[0047] As shown in FIG. 1 or FIG. 2, the inclination angle (213) of the inclination surface (Coanda Surface, 212) on the inner nozzle part is selected so that the shielding gas passing through the amplification nozzle (200) may flow efficiently due to the Coanda effect. It will be closely related to the material and surface roughness of the inclination surface (Coanda Surface, 212) and the type of shielding gas. If the inclination angle (213) is small, the flow of the shielding gas will maintain a high speed and its pressure is lower than the surrounding air even when reaching the guide part (131), so that the possibility of causing turbulent flow increases due to introducing the surrounding air, or if the inclination angle is big, it will be lost the Coanda effect and may be emitted from the inclination surface (Coanda Surface, 212). In other words, the inclination angle becomes an important factor in determining the speed and pressure of the total flow rate including the shielding gas and the introduced air. It is preferably 5 to 30 degrees.
[0048] As shown in FIG. 1 or FIG. 2, the guide part (131) of the welding tip (130) ensures straightness toward the welding parts while maintaining the total flow rate including the shielding gas and the introduced air in a stable and uniform laminar, so that the total flow rate surrounds uniformly the circumference of the welding parts, wherein the welding torch serves to enable work even in a windy external environment. It is preferably 5 to 15 mm. However, in some cases, the inclination angle (132) may be given as + (upper) or − (lower). In other words, if the welding parts is widely protected due to the sufficient flow rate, + inclination angle can be given.
[0049] As shown in FIG. 1 or FIG. 2, the welding tip angle (133) of the welding tip (130) may be 90 degrees, but it is usually an acute angle, wherein it may preferably be a obtuse angle of 45° or more so that the shielding gas may continue to go straight along the guide part, that is, the Coanda effect is not generated.
