Disclosure of Invention
The invention aims to provide a natural gas storage tank double-layer pipeline which reduces welding seams and is convenient to produce and manufacture and a manufacturing method thereof.
The utility model provides a marine natural gas storage tank double-deck pipeline, locates including inner tube and cover the sleeve pipe in the inner tube outside, the inner tube is equipped with the straight portion of inner tube and inner tube curved portion, the sleeve pipe includes the straight portion of sleeve pipe and sleeve pipe curved portion, sleeve pipe curved portion with inner tube curved portion corresponds the setting, the straight portion of sleeve pipe with the straight portion of inner tube corresponds the setting, sleeve pipe curved portion includes a plurality of mitre pipes, and is a plurality of the mitre pipe welds the concatenation each other and forms sleeve pipe curved portion, two pass through between the straight portion of sleeve pipe the sleeve pipe curved portion is connected.
In one embodiment, the diameter of the beveled tube is equal to the diameter of the straight portion of the sleeve.
In one embodiment, the inner pipe bend and the sleeve bend comprise a plurality of pipe bends.
In one embodiment, the inner diameter of the sleeve is greater than the outer diameter of the inner tube, and a gap exists between the sleeve and the inner tube.
In one embodiment, a limiting structure is arranged at an end of the inner pipe straight part, and the limiting structure is supported between the outer side wall of the inner pipe and the inner side wall of the sleeve.
In one embodiment, the number of the limiting structures is multiple, the limiting structures are kept on the same circumference, and the limiting structures mutually enclose a through hole for the straight part of the inner pipe to pass through.
In one embodiment, the limiting structure comprises a heat insulation plate and a supporting plate, the supporting plate is arranged on the inner side wall of the sleeve, one end of the heat insulation plate is connected with the supporting plate through a screw, and the other end of the heat insulation plate is abutted to the outer side wall of the inner pipe.
A manufacturing method of a double-layer pipeline of a natural gas storage tank for a ship comprises the following steps:
the linear inner pipe penetrates through a first straight sleeve part of the sleeve, the first straight sleeve part is arranged at the first straight inner pipe part of the inner pipe, and a second straight inner pipe part at the end part of the inner pipe is exposed;
bending the exposed inner pipe to form an inner pipe bending part between the first inner pipe straight part and the second inner pipe straight part;
the straight part of the second inner pipe penetrates through the plurality of oblique cutting pipes, the oblique cutting pipes are welded and connected from the end face of the straight part of the first sleeve pipe, the oblique cutting pipes are mutually welded and connected to form a sleeve pipe bent part, and the sleeve pipe bent part is matched with the inner pipe bent part;
the second inner pipe straight part penetrates through the second sleeve straight part, the end face of the second sleeve straight part is connected with the end face of the beveled pipe in a welding mode, and the second sleeve straight part is connected with the sleeve bent part.
In one embodiment, the end of the inner pipe straight portion is provided with a plurality of limiting structures, the limiting structures mutually enclose a through hole, and when the inner pipe straight portion passes through the sleeve pipe straight portion, the inner pipe straight portion needs to pass through the through hole.
In one embodiment, the number of the second inner pipe straight portion, the number of the inner pipe bent portions, the number of the sleeve bent portions, and the number of the second sleeve straight portions are two, and the two sleeve bent portions are sequentially welded between the first sleeve straight portion and the two second sleeve straight portions respectively.
In the double-layer pipeline of the natural gas storage tank and the manufacturing method thereof, the straight part of the first sleeve is sleeved in the middle of the inner pipe. And then the inner tank is bent into the shape required by the design. And respectively sleeving a plurality of oblique cutting pipes on the inner pipes. The plurality of beveled pipes are welded along the angle of the inner pipe bent portion to form a sleeve bent portion. When the manufacture of the sleeve bending part is finished, the second sleeve straight part is sleeved, and the second sleeve straight part is connected with the inclined cutting pipe in a welding mode, so that the manufacture of the double-layer pipeline is finished. In the natural gas storage tank double-layer pipeline and the manufacturing method thereof, the welding seams of the natural gas storage tank double-layer pipeline are a plurality of annular welding seams which are connected among a plurality of oblique pipes and connected between the oblique pipes and the straight part of the sleeve. Compared with the traditional manufacturing method of the double-layer pipeline of the natural gas storage tank, the length of the annular welding line of the double-layer pipeline of the natural gas storage tank is far smaller than that of the axial welding line, and the double-layer pipeline of the natural gas storage tank is convenient to machine and manufacture. Moreover, the sleeve does not need to be cut into half according to the axial direction of the sleeve, a large amount of cutting work can be reduced, and the sleeve is convenient to manufacture.
Detailed Description
While this invention is susceptible of embodiment in different forms, there is shown in the drawings and will herein be described in detail, specific embodiments thereof with the understanding that the present description is to be considered as an exemplification of the principles of the invention and is not intended to limit the invention to that as illustrated.
Thus, a feature indicated in this specification will serve to explain one of the features of one embodiment of the invention, and does not imply that every embodiment of the invention must have the stated feature. Further, it should be noted that this specification describes many features. Although some features may be combined to show a possible system design, these features may also be used in other combinations not explicitly described. Thus, the combinations illustrated are not intended to be limiting unless otherwise specified.
In the embodiments shown in the drawings, directional references (such as upper, lower, left, right, front and rear) are used to explain the structure and movement of the various elements of the invention not absolutely, but relatively. These descriptions are appropriate when the elements are in the positions shown in the drawings. If the description of the positions of these elements changes, the indication of these directions changes accordingly.
The preferred embodiments of the present invention will be further described in detail below with reference to the accompanying drawings.
Referring to fig. 2, the invention provides a marine natural gas storage tank double-layer pipeline and a manufacturing method thereof.
The marine natural gas storage tank double-layered pipeline 1 of the present embodiment includes aninner pipe 10 and asleeve 20 fitted around the outer side of theinner pipe 10. Thesleeve 20 is a stainless steel sleeve. Theinner pipe 10 is a stainless steel pipe. Theinner pipe 10 is used for running a natural gas medium and is used for meeting the requirements of a process system. The stainless steel pipe guarantees the intensity and the rigidity of inner tube, satisfies the operation requirement of natural gas storage tank pipeline. Thesleeve 20 serves to insulate theinner pipe 10 and, at the same time, to generate leakage if cracks are generated at the connection portion of theinner pipe 10 and the joint or the connection portion of theinner pipe 10. Thesleeve 20 acts as a secondary shield to prevent cryogenic natural gas from leaking to the hull deck.
Specifically, theinner pipe 10 is provided with an inner pipestraight portion 11 and an inner pipebent portion 12. And bending and molding the inner pipe according to design requirements. The inner pipestraight part 11 is used for extending to a bending part, and the bending part is provided with an innerpipe bending part 12. The innerpipe bending part 12 enables the inner pipestraight part 11 to change the direction, and design requirements are conveniently met.
Theinner tube 10 is a one-piece tube. Theinner tube 10 of integral type structure can satisfy the intensity demand of inner tube to guarantee that theinner tube 10 can stably use.
Thesleeve 20 includes a sleevestraight portion 21 and a sleevebent portion 22. Thesleeve bend 22 is disposed to correspond to theinner pipe bend 12. The sleevestraight portion 21 is provided corresponding to the inner pipestraight portion 11.
Thecasing bend 22 comprises a plurality ofchamfered tubes 221. The plurality ofchamfered tubes 221 are welded to each other to form thecasing bend 22. The twostraight portions 21 are connected by abent portion 22.
The diameter of thebeveled tube 221 is equal to the diameter of thestraight portion 21 of the sleeve. Thebeveled tube 221 is beveled from thestraight portion 21 of the sleeve. The curvature of thebent portion 22 of the casing formed by splicing the plurality ofchamfered tubes 221 can be adjusted by adjusting the angle of the end surface of the chamferedtube 221.
Theinner pipe bend 12 and thesleeve bend 22 include a plurality of them. In particular, in the present embodiment, the marine natural gas tank double-layered pipeline has an S-shape. Both theinner tube 10 and thesleeve 20 are S-shaped. The number of the inner pipestraight portions 11 and the number of the sleevestraight portions 21 are three. The inner-tubestraight portion 11 includes a first inner-tubestraight portion 111 located in the middle and second inner-tubestraight portions 112 located at both ends of the first inner-tubestraight portion 111. Accordingly, thestraight sleeve portion 21 includes a firststraight sleeve portion 211 at the middle and secondstraight sleeve portions 212 at both ends of the firststraight sleeve portion 211.
Theinner pipe bend 12 and thesleeve bend 22 are two in number. Two adjacent inner pipestraight portions 11 are connected by an inner pipebent portion 12. Two adjacentstraight portions 21 are connected by abent portion 22.
It is understood that in other embodiments, the number of the inner pipestraight portion 11 and the sleevestraight portion 21 may be 2, 4, etc. The number of the inner pipebent portion 12 and the sleevebent portion 22 is 1, 2, or the like. Therefore, the shape of the double-layer pipeline of the natural gas storage tank for the ship can be triangular, wavy and the like. The shapes of theinner tube 10 and thesleeve 20 are not limited herein.
The inner diameter of thesleeve 20 is larger than the outer diameter of theinner pipe 10. Theinner tube 10 is inserted into thesleeve 20, and thesleeve 20 is sleeved on the outer side of theinner tube 10. A certain gap is formed between thesleeve 20 and theinner tube 10, so that the oblique cutting tube can be conveniently sleeved into theinner tube 10.
Referring to fig. 3, a limiting structure 30 is disposed at an end of the inner tubestraight portion 11. The limiting structure 30 is supported between the outer sidewall of theinner tube 10 and the inner sidewall of thesleeve 20. Moreover, the number of the limiting structures 30 is plural, and the plurality of limiting structures 30 are kept on the same circumference. Specifically, in the present embodiment, there are three limiting structures 30. The relative position of thesleeve 20 and theinner pipe 10 is adjusted to enable the inner pipestraight part 11 to pass through a through hole surrounded by the limiting structures 30. The limiting structure 30 has a limiting effect in the installation process of theinner tube 10 and thesleeve 20, and can ensure the concentricity of theinner tube 10 and thesleeve 20 in the installation process, and ensure the smooth installation of theinner tube 10 and thesleeve 20.
The position limiting structure 30 includes aheat insulation plate 31 and asupport plate 32. Thesupport plate 32 is provided on the inner side wall of thesleeve 20. It will be appreciated that thesupport plate 32 is fixedly welded to the inner side wall of thesleeve 20. Thesupport plate 32 is a stainless steel plate.
One end of theheat insulation plate 31 is connected to thesupport plate 32 by afastener 33. The other end of theheat insulation plate 31 abuts against the outer sidewall of theinner pipe 10. Furthermore, theheat insulation plate 31 is provided with awaist hole 34. The waist holes 34 extend in the radial direction of theinner pipe 10. Thefastener 33 is arranged in thewaist hole 34 in a penetrating way and can slide along thewaist hole 34. The end of theheat insulation plate 31 close to theinner pipe 10 is arc-shaped. The arc shape is matched with the arc shape of the outer wall of theinner pipe 10, so that theheat insulating plate 31 can be completely abutted against theinner pipe 10. It is understood that thefastener 33 may be a bolt and a nut.
In a low-temperature use environment, since thesupport plate 32 is connected with theheat insulation plate 31 by thefastener 33, the displacement deformation caused by the cooling shrinkage of theinner pipe 10 is generated, and thefastener 33 can move along the extending direction of thewaist hole 34 and move towards theinner pipe 10 along the radial direction of theinner pipe 10, thereby adjusting the connecting position of thesupport plate 32 and theheat insulation plate 31. When theinner tube 10 is deformed at low temperature, the secondary stress generated by the low-temperature shrinkage of theinner tube 10 can be released through the waist holes 34. Meanwhile, the gap of the height of theheat insulation plate 31 at least exists between thesleeve 20 and theinner pipe 10, so that the cold insulation in the later period is not influenced. The limiting structure 30 can be stably supported between the first inner pipestraight portion 111 and the first sleevestraight portion 211.
And, a plurality of limit structures 30 are symmetrically distributed along the circumferential direction of the outer sidewall of theinner tube 10. Theheat insulation plates 31 of the respective position restricting structures 30 can be respectively abutted against the outer side walls of theinner pipes 10. Since the plurality of position-limiting structures 30 are symmetrically distributed along the circumference of the outer sidewall of theinner pipe 10, the heat-insulatingplate 31 can also be symmetrically distributed with respect to the outer sidewall of theinner pipe 10. Therefore, theheat insulation plates 31 can be symmetrically distributed on the periphery of theinner pipe 10, theheat insulation plates 31 can stably abut against the outer side wall of theinner pipe 10, the pressure action of theheat insulation plates 31 on theinner pipe 10 is kept balanced, and the phenomenon that theinner pipe 10 is greatly deformed due to cooling to affect the normal use of theinner pipe 10 is avoided.
The gap between thesleeve 20 and theinner pipe 10 may be filled with an insulating layer. The heat preservation layer is used for preserving the heat of the marine natural gas storage tank double-layer pipeline.
Referring to fig. 4, a method for manufacturing a marine natural gas storage tank double-layer pipeline includes the following steps:
in step S11, the straight inner tube passes through the straightfirst sleeve portion 211 of the sleeve, the straightfirst sleeve portion 211 is disposed at the straight firstinner tube portion 111 of theinner tube 10, and the straight secondinner tube portion 112 of the inner tube end is exposed.
The first inner pipestraight portion 111 is located in the middle of the inner pipe. At this time, theinner tube 10 is still a straight tube, and theinner tube 10 can directly penetrate into thesleeve 20, so as to solve the problem of the sleeve of the first sleevestraight part 211 at the middle first inner tubestraight part 111.
The end of the straight portion of inner tube is equipped with a plurality of limit structure 30, and a via hole is enclosed into each other to a plurality of limit structure 30. When the first inner pipestraight portion 111 passes through the first sleevestraight portion 211, the first inner pipestraight portion 111 needs to pass through the through hole.
The end of the first inner pipestraight part 111 is connected with the first sleevestraight part 211 by the limiting structure 30. The limiting structure 30 has a limiting effect during the installation process of theinner tube 10 and thesleeve 20, so as to ensure the concentricity of theinner tube 10 and thesleeve 20.
When the first inner pipestraight portion 111 is cooled and contracted, the limiting structure 30 can be stably supported between the first inner pipestraight portion 111 and the first sleeve pipestraight portion 211. The first inner pipestraight part 111 is prevented from being seriously deformed, and the stable support between theinner pipe 10 and thesleeve 20 is prevented from being influenced.
In step S12, the two ends of the exposedinner tube 10 are bent to form the inner tubebent portion 12 between the first inner tubestraight portion 111 and the second inner tubestraight portion 112.
Theinner tube 10 is bent into an S-shape or other shape according to the design requirements. Specifically, in the present embodiment, there are two inner pipe bentportions 12, which are located at both ends of the first inner pipestraight portion 111. Then, both ends of theinner tube 10 are linear, i.e., two second inner-tubestraight portions 112 are formed.
At this time, the second inner pipestraight portions 112 at the two ends of theinner pipe 10 are exposed, and can be directly bent, thereby facilitating the operation.
In step S13, the second inner pipestraight portion 112 passes through the plurality ofchamfered tubes 221, the chamferedtubes 221 are welded from the end surface of the first sleevestraight portion 211, the plurality ofchamfered tubes 221 are welded to each other to connect the sleevebent portion 22, and the sleevebent portion 22 is fitted to the inner pipebent portion 12.
Thechamfered tube 221 includes a plurality of tubes. The first oblique cutting pipe can be directly sleeved at the end of the first sleevestraight part 211, one end face of the first oblique cutting pipe is welded with the end face of the first sleevestraight part 211, and thewelding seam 23 surrounds the end face of the first sleeve straight part. The second beveled pipe is sleeved on thebent part 12 of the inner pipe and is welded with the end face of the other end of the first beveled pipe, and thewelding seam 23 is also annular.
The inner pipebent portion 12 and the sleevebent portion 22 are both provided. The number of the second inner-tubestraight portions 112 is also two, and a plurality of the chamferedtubes 221 need to be respectively sleeved at the free ends of the two second inner-tubestraight portions 112.
It is understood that, in other embodiments, when the number of thebeveled pipes 221 is small and the radian of the corresponding formed sleevebent portion 22 is small, thebeveled pipes 221 may be welded and spliced to form the sleevebent portion 22, and then the sleevebent portion 22 is sleeved on theinner pipe 10 and welded to the first inner pipestraight portion 111.
In step S14, the second inner pipestraight portion 112 penetrates the second sleevestraight portion 212, and the end surface of the second sleevestraight portion 212 is welded to the end surface of thebeveled pipe 221, so that the second sleevestraight portion 212 is connected to the sleevebent portion 22.
When the end surfaces of the two sleevebent portions 22 are welded to the two ends of the first sleevestraight portion 211, the second sleevestraight portion 212 is inserted into the second inner tubestraight portion 112, and the second sleevestraight portion 212 is welded to the end surface of the other end of the sleevebent portion 22.
Also, the connection between the second innerstraight tube portion 112 and the secondstraight sleeve portion 212 operates similarly to when the first innerstraight tube portion 111 and the firststraight sleeve portion 211 are connected to each other. The end of the second inner pipestraight portion 112 is provided with a plurality of limiting structures 30. When the second inner-tubestraight portion 112 passes through the second-sleevestraight portion 212, the second inner-tubestraight portion 112 needs to pass through the through hole defined by the plurality of limiting structures 30. The end of the second inner pipestraight part 112 is connected with the second sleevestraight part 212 by the limiting structure 30. When the second inner pipestraight portion 112 is cooled and contracted, the limiting structure 30 can be stably supported between the second inner pipestraight portion 112 and the second sleevestraight portion 212.
Specifically, two second casingstraight portions 212 are provided, and the two second casingstraight portions 212 are respectively connected to the two casingbent portions 22 by welding.
In the above natural gas storage tank double-layer pipeline 1 and the manufacturing method thereof, the welding seam of the natural gas storage tank double-layer pipeline 1 is a plurality of annular welding seams which are connected between a plurality ofoblique pipes 221 and connected between theoblique pipes 221 and thestraight part 21 of the sleeve. Compared with the traditional manufacturing method of the double-layer pipeline of the natural gas storage tank, the length of the annular welding line of the double-layer pipeline 1 of the natural gas storage tank is far smaller than that of the axial welding line, and the processing and the manufacturing are convenient. Moreover, thesleeve 20 does not need to be cut into half according to the axial direction of the sleeve, and meanwhile, a large amount of cutting work can be reduced, and the manufacturing is convenient.
While the present invention has been described with reference to several exemplary embodiments, it is understood that the terminology used is intended to be in the nature of words of description and illustration, rather than of limitation. As the present invention may be embodied in several forms without departing from the spirit or essential characteristics thereof, it should also be understood that the above-described embodiments are not limited by any of the details of the foregoing description, but rather should be construed broadly within its spirit and scope as defined in the appended claims, and therefore all changes and modifications that fall within the meets and bounds of the claims, or equivalences of such meets and bounds are therefore intended to be embraced by the appended claims.