阅读说明：本技术 一种燃料舱波纹板与角钢过渡区域连续焊接方法 (Continuous welding method for transition area of corrugated plate and angle steel of fuel tank ) 是由 龚海磊 杨新杰 蔡春茂 薛卫中 徐向阳 张彬 陆晓华 刘安成 刘炳 余强 于 2021-08-31 设计创作，主要内容包括：一种燃料舱波纹板与角钢过渡区域连续焊接方法,包括焊接过程,所述焊接过程采用惰性气体进行保护焊,将第一待焊接件搭接在第二待焊接件上；焊接过程的参数为焊接电流为50-60A,焊接电压为8-10V,焊接速度为8-18mm/min,保护气氩气的流量为10-15L/min,焊接枪与焊接面的垂直面的倾角为5-15°,电源极性采用直流,且采用正接的方式进行焊接；本发明能够解决舱室壁板拐角处不同板厚过渡区域的焊接施工难题,实现了波纹角板在薄、厚板搭接过渡区域连续焊接,保证波纹角板过渡区域的焊缝质量,提高该区域的接头外观及探伤合格率,改善了施工环境、缩短了建造工期,降低了生产成本。(A continuous welding method for a transition region of a corrugated plate and angle steel of a fuel compartment comprises a welding process, wherein inert gas is adopted for shielded welding in the welding process, and a first part to be welded is lapped on a second part to be welded; the parameters of the welding process are that the welding current is 50-60A, the welding voltage is 8-10V, the welding speed is 8-18mm/min, the flow of the protective gas argon is 10-15L/min, the inclination angle of the welding gun and the vertical plane of the welding surface is 5-15 degrees, the polarity of the power supply adopts direct current, and the welding is carried out in a positive connection mode; the invention can solve the difficult problem of welding construction in the transition areas with different plate thicknesses at the corners of the cabin wall plate, realizes the continuous welding of the corrugated angle plate in the overlapping transition areas of the thin plate and the thick plate, ensures the weld quality of the transition area of the corrugated angle plate, improves the appearance of the joint and the flaw detection qualification rate of the area, improves the construction environment, shortens the construction period and reduces the production cost.)

1. A continuous welding method for a transition region of a corrugated plate and angle steel of a fuel compartment is characterized by comprising a welding process, wherein inert gas is adopted for shielded welding in the welding process, and a first part to be welded (1) is lapped on a second part to be welded (2); the parameters of the welding process are that the welding current is 50-60A, the welding voltage is 8-10V, the welding speed is 8-18mm/min, the flow of the protective gas argon is 10-15L/min, the inclination angle of the welding gun (3) and the vertical plane of the welding surface is 5-15 degrees, the polarity of the power supply adopts direct current, and the welding is carried out in a positive connection mode.

2. The continuous welding method for the transition area between the corrugated plate and the angle steel of the fuel tank is characterized in that the assembly distance between the first part to be welded (1) and the second part to be welded (2) is 0-0.3mm during the welding process.

3. The continuous welding method for the transition area of the corrugated plate and the angle steel of the fuel tank as claimed in claim 1 or 2, further comprising a pre-welding treatment process, wherein the pre-welding treatment process adopts acetone solvent to clean the surface radius of the welding area within 60 mm.

4. The method of claim 1, comprising a weld ending process, wherein the weld ending process is closed by shielding gas for 3-5 seconds.

5. The continuous welding method for the transition area of the corrugated plate and the angle steel of the fuel tank as claimed in claim 1, wherein the welding speed of the welding at the straight position is 12-18mm/min, or the welding speed of the welding at the transverse position is 10-15 mm/min; or the welding speed of the horizontal welding is 8-14' mm/min, or the welding speed of the vertical position welding is 10-14mm/min, or the welding speed of the vertical position welding is 8-14mm/min, or the welding speed of the overhead position welding is 12-15 mm/min.

Technical Field

The invention relates to the field of welding, in particular to a continuous welding method for a transition region of corrugated plates and angle steel of a fuel compartment.

Background

In recent years, the Mark III type film tank is widely concerned due to the characteristics of high utilization rate of internal space of ships, low evaporation rate, low raw material and manufacturing cost and the like, and is successfully applied to a plurality of ultra-large container ships, the container ships have the remarkable characteristic of having a Mark III type film LNG dual-fuel tank, and the structural construction welding part mainly relates to the welding of a main shielding corrugated plate.

Corrugated sheets are typically 304L stainless steel sheets 1.2mm thick with longitudinal and transverse corrugated grooves, typically welded using filler wire argon tungsten arc welding. The structure is complex, so that the welding difficulty is high, especially the corrugation and the area and the lap joint transition area have high requirements on the operation of a welder, and the welding quality is difficult to ensure. Compared with the welding of the flat plate of the No.96 type film cabin, the automatic welding degree is lower, the automatic welding difficulty of the corrugated groove area is higher, and the welding quality is difficult to guarantee.

The main shielding buckled plate welding design type mainly has 3 big types, the buckled plate that first type 1.2mm is thick and the buckled plate overlap joint that 1.2mm is thick, the buckled plate that second type 1.2mm is thick and the main buckled plate intersect spare of the thick stainless steel gasket overlap joint of 2.0mm, the third type is the buckled plate that 1.2mm is thick and the thick stainless steel angle steel overlap joint of 8 mm.

At present, for the angle steel of conventional corrugated plate band angle and corrugated plate overlap joint transition region, because the plate thickness difference is great, in order to obtain good penetration, avoid the welding seam surplus height not enough, current parameter needs real-time adjustment when 1.2mm corrugated plate and 8mm stainless steel angle steel weld, and this operation level requirement to welder is higher. In the third corner area, especially corrugated plate is difficult to weld continuously in the overlapping transition area of thin and thick plates. In the welding process of the transition from the stainless steel corner to the lapped corrugated plate, the current needs to be changed while the welding process is not interrupted. Because the welding parameters of different areas are inconsistent, the welding parameters need to be adjusted in the welding process, and the parameters are difficult to adjust during manual welding, so that welding penetration or other defects are easy to generate, and repairing are needed.

Disclosure of Invention

In view of the above-mentioned shortcomings of the prior art, the present invention provides a continuous welding method for overlapping corrugated plates and stainless steel angle bars.

The invention provides a continuous welding method for a transition region of a corrugated plate and angle steel of a fuel compartment, which comprises a welding process, wherein inert gas is adopted for shielded welding in the welding process, and a first part to be welded is lapped on a second part to be welded; the parameters of the welding process are that the welding current is 50-60A, the welding voltage is 8-10V, the welding speed is 8-18mm/min, the flow of the protective gas argon is 10-15L/min, the inclination angle of the welding gun and the vertical plane of the welding surface is 5-15 degrees, the polarity of the power supply adopts direct current, and the welding is carried out in a positive connection mode.

Preferably, in the welding process, the assembly distance between the first part to be welded and the second strip welding part is 0-0.3 mm.

Preferably, the method further comprises a pre-welding treatment process, wherein the acetone solvent is adopted to clean the welding area surface within 60 mm.

Preferably, a welding ending process is included, and the welding ending process protective gas can be closed for 3-5 seconds in an extending mode.

Preferably, the bottom of slag pot is provided with the dwang, the one end of dwang rotate connect in slag pot bottom, the other end rotate connect in the lifting rod.

Preferably, the welding speed of the straight position welding is 12-18mm/min, or the welding speed of the horizontal position welding is 10-15 mm/min; or the welding speed of the horizontal welding is 8-14' mm/min, or the welding speed of the vertical position welding is 10-14mm/min, or the welding speed of the vertical position welding is 8-14mm/min, or the welding speed of the elevation position welding is 12-15 mm/min.

As mentioned above, the continuous welding method for the transition area of the corrugated plate and the angle steel of the fuel tank has the following beneficial effects: the welding construction problem of different plate thickness transition regions at the corners of the cabin wall plate can be solved, the continuous welding of the corrugated angle plate in the thin and thick plate lap joint transition regions is realized, the welding seam quality of the corrugated angle plate transition region is ensured, the joint appearance and the flaw detection qualification rate of the region are improved, the construction environment is improved, the construction period is shortened, and the production cost is reduced.

Drawings

Fig. 1 is a schematic view of a welding gun according to the present invention welding a first member to be welded and a second member to be welded.

Fig. 2 is a schematic view of a first member to be welded according to the present invention.

Fig. 3 is a schematic view of a first member to be welded according to the present invention.

Fig. 4 is a schematic view of welding performed when the first member to be welded and the second member to be welded are in a straight state according to the present invention.

Fig. 5 is a schematic view of welding performed when the first member to be welded and the second member to be welded are in an overhead welding state according to the present invention.

Fig. 6 is a front view of the first member to be welded and the second member to be welded in the welding position in the present invention.

Fig. 7 is a side view of the first member to be welded and the second member to be welded in the horizontal position according to the present invention.

Fig. 8 is a front view of the first member to be welded and the second member to be welded in the horizontal position according to the present invention.

Fig. 9 is a side view of the first member to be welded and the second member to be welded in the horizontal position according to the present invention.

Fig. 10 is a schematic view of welding performed when the first member to be welded and the second member to be welded are in the standing position according to the present invention.

Fig. 11 is a schematic view of welding performed when the first member to be welded and the second member to be welded are in the standing position according to the present invention.

Fig. 12 is a schematic view of the throat when the first member to be welded and the second member to be welded are welded in the present invention.

Description of reference numerals:

1. a first part to be welded; 2. a second part to be welded; 21. a first to-be-welded part; 22. a second part to be welded; 3. a welding gun; 12. a first lap weld; 13. a second lap weld.

Detailed Description

The following description of the embodiments of the present invention is provided for illustrative purposes, and other advantages and effects of the present invention will become apparent to those skilled in the art from the present disclosure.

It should be understood that the structures, ratios, sizes, and the like shown in the drawings and described in the specification are only used for matching with the disclosure of the specification, so as to be understood and read by those skilled in the art, and are not used to limit the conditions under which the present invention can be implemented, so that the present invention has no technical significance, and any structural modification, ratio relationship change, or size adjustment should still fall within the scope of the present invention without affecting the efficacy and the achievable purpose of the present invention. In addition, the terms such as "upper", "lower", "left", "right" and "middle" used in the present specification are for clarity of description, and are not intended to limit the scope of the present invention, and changes or modifications of the relative relationship may be made without substantial technical changes.

As shown in fig. 1-12, an embodiment of a continuous welding method for a transition region between a corrugated plate and an angle steel of a fuel tank provided by the invention comprises a welding process, wherein the welding process adopts inert gas for shielded welding, and a first part to be welded 1 is overlapped on a second part to be welded 2; the parameters of the welding process are that the welding current is 50-60A, the welding voltage is 8-10V, the welding speed is 12-18mm/min, the flow of the protective gas argon is 10-15L/min, the inclination angle alpha of the welding gun 3 and the vertical surface of the welding surface is 5-15 degrees, the polarity of the power supply adopts direct current, and the welding is carried out in a positive connection mode. During specific welding, the adopted equipment can be a portable argon arc welding machine with the model OTC TIG MINI200P I, and the welding mode of the self-melting argon tungsten-arc welding without wire filling is adopted.

As shown in fig. 1, in the present embodiment, the welding process mainly welds the first member to be welded 1 on the second member to be welded 21 and the second member to be welded 22. Wherein the first piece to be welded 1 is a corrugated plate of 304L, and the plate thickness is 1.2 mm; the second part to be welded 2 comprises a first part to be welded 21 and a second part to be welded 22, wherein the first part to be welded 21 is 304L stainless steel, and the plate thickness is 8 mm; one part of the first part to be welded 1 is overlapped on a first part to be welded 21, and the other part is overlapped on a second part to be welded 22, wherein the second part to be welded 22 is a corrugated plate of 304L, and the plate thickness is 1.2 mm. Although the first members to be welded 1 are respectively overlapped on members to be welded of different materials and different plate thicknesses, the welding gun 3 can weld the first members to be welded 1 and the second members to be welded 22 (i.e., the second lap weld 13) to the overlap of the first members to be welded 1 and the second members to be welded 21 (i.e., the first lap weld 12) until the welding is completed. In practice, only the welding of the first member to be welded 1 and the second member to be welded 21 needs to be considered.

When the Mark III type film cabin is built, the method can solve the welding construction problem of different plate thickness transition areas at the corners of the cabin wall plate, realizes the continuous welding of the corrugated angle plate in the thin plate and thick plate lap joint transition areas (namely the first part to be welded 1, the second part to be welded 21 and the second part to be welded 22), ensures the welding seam quality of the corrugated angle plate transition area, improves the joint appearance and the flaw detection qualification rate of the area, improves the construction environment, shortens the construction period and reduces the production cost. Meanwhile, the current parameters are prevented from being adjusted in real time when the 1.2mm corrugated plate and the 8mm stainless steel angle steel are welded, and the operation level of a welder is reduced.

It should be noted that the lap clearance between the first to-be-welded part 1 and the second to-be-welded part 2 is 0-0.3mm, or the lap clearance between the first to-be-welded part 1 and the second to-be-welded part 2 is 0-0.3mm during welding. Because the invention adopts the self-melting welding of the base material, the gap is convenient for the connection of the first part to be welded 1 and the second part to be welded 2.

Of course, in order to remove oil, rust, scale and other substances harmful to welding in the weld zone. The surface of the weld zone may be cleaned within 60mm using acetone solvent prior to welding.

A continuous welding method for a transition area of a corrugated plate and angle steel of a fuel compartment further comprises a welding ending process, and protective gas can be prolonged for 3-5s and closed in the welding ending process.

And performing nondestructive testing 24 hours after welding. And (4) coloring detection (PT), wherein the detection result meets the requirement of the qualified grade in the ISO-23277 weld nondestructive testing-coloring detection standard. And also requires macroscopic metallographic examination of the weld size to fit the desired size.

As shown in FIG. 12, the dimensional requirements of the good weld cross section after welding are satisfied, and the expected dimensional requirements, wherein, for the formed weld, the throat a is greater than or equal to 0.8mm, the weld width W is greater than or equal to 3 and less than or equal to 5.2mm, the penetration width La is greater than or equal to 2.0mm, and the penetration P is greater than or equal to 0.5 mm.

In practice, the relative positions of the first part to be welded 1 and the second part to be welded 2 are different, the optimal welding speed is also different, and the important point of welding is the welding between the first part to be welded 1 and the second part to be welded 21. The first part to be welded 1 is a corrugated plate of 304L with the thickness of 1.2mm, wherein the length multiplied by the width of the corrugated plate is 100mm multiplied by 250 mm; the second member to be welded, first 21, is a 304L stainless steel plate 8mm thick, wherein the length × width of the stainless steel plate is 150mm × 250mm, for example, and welding is performed.

As shown in fig. 4, the vertical direction (i.e., the up-down direction) of the first member to be welded 1 coincides with the thickness direction of the first member to be welded 1, and the vertical direction (i.e., the up-down direction) of the second member to be welded 21 coincides with the thickness direction of the second member to be welded 21. The lower end face of the first part to be welded 1 is tightly attached to the upper end face of the second part to be welded 21, and the first lap weld 12 is located on the upper end face of the second part to be welded 21. At this time, it can be said that the two pieces to be welded are located in a straight position, and at the same time, the welding speed is preferably 12 to 18 mm/min.

As shown in fig. 5, the vertical direction (i.e., the up-down direction) of the first member to be welded 1 coincides with the thickness direction of the first member to be welded 1, and the vertical direction (i.e., the up-down direction) of the second member to be welded 21 coincides with the thickness direction of the second member to be welded 21. The upper surface of the first part to be welded 1 is tightly attached to the lower end surface of the second part to be welded 21, and the first lap weld 12 is located on the lower end surface of the second part to be welded 21. In this case, the two workpieces to be welded can be referred to as overhead welding positions, and the welding speed is 12-15 mm/min.

As shown in fig. 6 and 7, the vertical direction (i.e., the up-down direction) of the first workpiece to be welded 1 coincides with the width direction of the first workpiece to be welded 1, and the vertical direction (i.e., the up-down direction) of the second workpiece to be welded 21 coincides with the width direction of the second workpiece to be welded 21. The front end face of the first to-be-welded part 1 is a 150mm × 250mm end face, the rear end face of the second to-be-welded part 21 is a 100mm × 250mm end face, the front end face of the first to-be-welded part 1 is tightly attached to the rear end face of the second to-be-welded part 21, the first lap weld 12 is located on the middle upper portion of the front end face of the second to-be-welded part 21, and during welding, the welding direction is along the length direction of the first to-be-welded part 1 and the second to-be-welded part 21, namely, the left and right direction is shown as the arrow direction in fig. 6. At the moment, two pieces to be welded are positioned at the horizontal position, and the welding speed is 10-15 mm/min.

As shown in fig. 8 and 9, the vertical direction (i.e., the up-down direction) of the first workpiece to be welded 1 coincides with the width direction of the first workpiece to be welded 1, and the vertical direction (i.e., the up-down direction) of the second workpiece to be welded 21 coincides with the width direction of the second workpiece to be welded 21. The front end face of the first to-be-welded part 1 is a 150mm multiplied by 250mm end face, the rear end face of the second to-be-welded part 21 is a 100mm multiplied by 250mm end face, the front end face of the first to-be-welded part 1 is tightly attached to the rear end face of the second to-be-welded part 21, and the first lap weld 12 is located at the middle lower portion of the front end face of the second to-be-welded part 21. When welding, the welding direction is along the length direction of the first member to be welded 1 and the second member to be welded 21, i.e., the left-right direction as shown by the arrow direction in fig. 8. At the moment, two pieces to be welded are in the horizontal lower position, and the welding speed is 8-14 mm/min.

As shown in fig. 10, the vertical direction (i.e., the up-down direction) of the first member to be welded 1 coincides with the longitudinal direction of the first member to be welded 1, and the vertical direction (i.e., the up-down direction) of the second member to be welded 21 coincides with the longitudinal direction of the second member to be welded 21. The front end face of the first to-be-welded part 1 is a 150mm × 250mm end face, the rear end face of the second to-be-welded part 21 is a 100mm × 250mm end face, the front end face of the first to-be-welded part 1 is closely attached to the rear end face of the second to-be-welded part 21, and during welding, the welding direction is along the length direction of the first to-be-welded part 1 and the second to-be-welded part 21, namely, the up-down direction shown by arrows in fig. 10. At the moment, two pieces to be welded are positioned at the vertical position, and the welding speed is 10-14 mm/min.

As shown in fig. 11, the vertical direction (i.e., the up-down direction) of the first member to be welded 1 coincides with the longitudinal direction of the first member to be welded 1, and the vertical direction (i.e., the up-down direction) of the second member to be welded 21 coincides with the longitudinal direction of the second member to be welded 21. The front end face of the first part to be welded 1 is 150mm multiplied by 250mm, the rear end face of the second part to be welded 21 is 100mm multiplied by 250mm, and the front end face of the first part to be welded 1 is tightly attached to the rear end face of the second part to be welded 21. When welding, the welding direction is along the length direction of the first member to be welded 1 and the second member to be welded 21, i.e., the up-down direction as indicated by the arrows in fig. 11. At the moment, two pieces to be welded are in the vertical position, and the welding speed is 8-14 mm/min.

The foregoing embodiments are merely illustrative of the principles and utilities of the present invention and are not intended to limit the invention. Any person skilled in the art can modify or change the above-mentioned embodiments without departing from the spirit and scope of the present invention. Accordingly, it is intended that all equivalent modifications or changes which can be made by those skilled in the art without departing from the spirit and technical spirit of the present invention be covered by the claims of the present invention.