CN110145644A - A kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship - Google Patents

A kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship Download PDF

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Publication number
CN110145644A
CN110145644A CN201910463130.1A CN201910463130A CN110145644A CN 110145644 A CN110145644 A CN 110145644A CN 201910463130 A CN201910463130 A CN 201910463130A CN 110145644 A CN110145644 A CN 110145644A
Authority
CN
China
Prior art keywords
panel
plate
cryotronl
support plate
crossing cabin
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201910463130.1A
Other languages
Chinese (zh)
Inventor
崔貌
刘帅
李红波
季腾
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hudong Zhonghua Shipbuilding Group Co Ltd
Original Assignee
Hudong Zhonghua Shipbuilding Group Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hudong Zhonghua Shipbuilding Group Co Ltd filed Critical Hudong Zhonghua Shipbuilding Group Co Ltd
Priority to CN201910463130.1A priority Critical patent/CN110145644A/en
Publication of CN110145644A publication Critical patent/CN110145644A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L5/00Devices for use where pipes, cables or protective tubing pass through walls or partitions
    • F16L5/02Sealing
    • F16L5/022Sealing by welding

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

The invention discloses a kind of dedicated multi-joint cryotronl crossing cabin parts of LNG ship, including panel and support plate, the panel is all made of low temperature stainless steel with the support plate and is made, circumferential direction setting of the support plate along the panel, the support plate is vertical with the panel, run through on the panel and is above provided at least one perforation hole, the circumferential direction of the perforation hole is provided with annular compound plate, the length of the annular compound plate is greater than the thickness of the panel, and the both ends of the annular compound plate are located at the two sides of the panel.The present invention replaces low temperature stainless steel bulkhead using the crossing cabin part of an entirety, the cryotronl induction as a whole that more are intensively arranged, the installation of the cryotronl different suitable for a variety of latus rectums, reduce material cost, reduce welding difficulty, due to being provided with crossing cabin part, the crossing cabin hole on bulkhead can be expanded, positioning to cryotronl and lower through requiring, reduces the crossing cabin difficulty of cryotronl, facilitates the construction of worker and the cladding of insulation.

Description

A kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship
Technical field
The invention belongs to LNG ship oceangoing ship building technology fields, and in particular to a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship.
Background technique
In the prior art, during LNG ship designs, more cryogenic pipes is often had and are pierced by cargo Machine Room, and And these pipelines, at a distance of relatively closely, the method that cryotronl is pierced by bulkhead is a main points of LNG ship design.Conventional way is in cabin Direct aperture is passed through for cryotronl on wall, is welded and fixed between cryotronl and bulkhead by annular compound plate, due to the temperature of cryotronl Very low, meeting bursting by freezing bulkhead is spent, therefore, the bulkhead of the bulk zone around annular compound plate cannot use carbon steel, but use low temperature Stainless steel replaces.
In conclusion the design of the prior art mainly has following deficiency: (1) material cost of low temperature stainless steel bulkhead is high, Increase the manufacturing cost of LNG ship;(2) when stainless steel bulkhead is with the butt welding of carbon steel bulkhead, difficulty is high, and time-consuming;(3) bulkhead aperture Small, positioning to pipeline and through more demanding, site operation difficulty is big, while being also unfavorable for the cladding of exterior insulation.
Summary of the invention
Aiming at the problems existing in the prior art, the present invention provides a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship, this hair The bright cryotronl integral arrangement that can intensively arrange more, reduces material cost, reduces welding difficulty, to cryotronl It positions and runs through of less demanding, reduce the difficulty of crossing cabin, facilitate worker's construction and insulating wrapped.
To achieve the above object, the invention adopts the following technical scheme:
The present invention provides a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship, including panel and support plate, the panel and the branch Fagging is all made of low temperature stainless steel and is made, the support plate along the panel circumferential direction setting, the support plate with it is described Panel is vertical, and through at least one perforation hole is above provided on the panel, it is multiple that the circumferential direction of the perforation hole is provided with annular Plate, the length of the annular compound plate are greater than the thickness of the panel, and the both ends of the annular compound plate are located at the two sides of the panel, The length that the annular compound plate is located at the support plate side is less than the length of the support plate, when the latus rectum of the cryotronl is small When 500 millimeters, it is described annular compound plate with a thickness of 6 millimeters, when the latus rectum of the cryotronl be more than or equal to 500 millimeters when, institute State annular compound plate with a thickness of 8 millimeters.
The side that the middle part of the panel is located at the support plate as a preferred technical solution, is provided with stiffening plate, institute Stating between stiffening plate and the panel, the support plate and the panel is to be welded to connect, and the length of the stiffening plate is less than The length of the support plate.
Further technical effect, by the way that stiffening plate is arranged, so that the structure of panel is more stable, avoiding panel makes Due to meeting with stresses and deformation occurs during.
The stiffening plate is set as 3 as a preferred technical solution, including 2 longitudinal directions are disposed in parallel longitudinally reinforced Lateral stiffening plate between 2 longitudinally reinforced plates of plate and setting, the vertical longitudinally reinforced plate of the transverse direction stiffening plate.
Further technical effect, 3 stiffening plates form I-shaped structure, and structural stability is good, further avoids making Deformation occurs during.
The width of the stiffening plate is 10 millimeters smaller than the width of the support plate as a preferred technical solution,.
Further technical effect is deformed or is shifted because of temperature change to avoid crossing cabin part using such design When, the risk factors such as friction or even spark occur between stiffening plate and bulkhead.
The junction of the panel and the support plate is provided with multiple gussets, the muscle as a preferred technical solution, Plate is set to the outside of the support plate, and the width of the gusset is equal to the width of the support plate, the gusset and the face It is to be welded to connect between plate, the gusset and the support plate.
The setting of further technical effect, gusset can effectively improve integrally-built stability, and gusset is set to The outside of support plate, when the latus rectum of cryotronl is less than 500 millimeters, does not need gusset convenient for welding;When the latus rectum of cryotronl is big When 500 millimeters, need to increase gusset in the outside of support plate.
The panel, the support plate as a preferred technical solution, the stiffening plate, the gusset thickness be 12 millimeters.
Further technical effect, when the thickness of material reaches above-mentioned value, integral strength can reach use demand.
It is connected as a preferred technical solution, between the annular compound plate and the panel for deep penetration welding.
Compared with prior art, the invention has the benefit that the present invention replaces low temperature using the crossing cabin part of an entirety Stainless steel bulkhead, the cryotronl induction as a whole that more are intensively arranged, the installation of the cryotronl different suitable for a variety of latus rectums subtract Material cost is lacked, has reduced welding difficulty, due to being provided with crossing cabin part, the crossing cabin hole on bulkhead can have been expanded, to cryotronl Positioning and lower through requiring, reduce the crossing cabin difficulty of cryotronl, facilitate the construction of worker and the cladding of insulation.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with It obtains other drawings based on these drawings.
Fig. 1 is the top view of the dedicated multi-joint cryotronl crossing cabin part of LNG ship of the present invention.
Fig. 2 is the main view of the dedicated multi-joint cryotronl crossing cabin part of LNG ship of the present invention.
Fig. 3 is the structural schematic diagram of the dedicated multi-joint cryotronl crossing cabin part of LNG ship of the present invention.
Fig. 4 is the Stress calculation cloud atlas of the dedicated multi-joint cryotronl crossing cabin part of LNG ship of the present invention.
Wherein, appended drawing reference is described as follows: panel 1, support plate 2, stiffening plate 3, gusset 4, annular compound plate 5, poling Hole 6.
Specific embodiment
In the description of the present invention, it is to be understood that, term " longitudinal direction ", " transverse direction ", "upper", "lower", "front", "rear", The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside" is based on attached drawing institute The orientation or positional relationship shown, is merely for convenience of description of the present invention and simplification of the description, rather than the dress of indication or suggestion meaning It sets or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as to limit of the invention System.
As shown in Figure 1-Figure 3, the dedicated multi-joint cryotronl crossing cabin part of a kind of LNG ship, including panel 1, support plate 2, stiffening plate 3, gusset 4 and annular compound plate 5, panel 1, support plate 2, stiffening plate 3, gusset 4 and annular compound plate 5 are all made of the production of low temperature stainless steel It forms.Panel 1, support plate 2, stiffening plate 3, gusset 4 thickness be 12 millimeters.Wherein, the both ends of the main body of panel 1 are in circular arc Shape is provided with 4 perforation holes 6 on panel 1, wherein and the latus rectum positioned at 2 perforation holes 6 at both ends is 500 millimeters and 600 millimeters, The latus rectum for being located in the middle 2 perforation holes 6 is 300 millimeters.Perforation hole 6 was provided with annular compound plate 5, annular compound plate 5 along one week Connect between panel 1 for deep penetration welding, the annular compound plate 5 of 2 perforation holes, 6 circumferential direction at 1 both ends of panel with a thickness of 8 millimeters, face The circumferential annular compound plate 5 of 2 perforation holes 6 at the middle part of plate 1 with a thickness of 6 millimeters.The length of annular compound plate 5 is greater than the thickness of panel 1 Degree, the both ends of annular compound plate 5 are located at the two sides of panel 1, for being welded with cryotronl.Panel 1 is circumferentially arranged support Plate 2, support plate 2 is ring structure, vertical with panel 1, and the length that annular compound plate 5 is located at 2 side of support plate is less than support plate 2 Length.
The side that the middle part of panel 1 is located at support plate 2 is provided with stiffening plate 3, stiffening plate 3 and panel 1, support plate 2 and face It is to be welded to connect between plate 1, the width of stiffening plate 3 is less than the width of support plate 2, and the width of stiffening plate 3 is wider than support plate 2 It spends 10 millimeters small.Stiffening plate 3 is set as 3, including 2 longitudinal directions longitudinally reinforced plate disposed in parallel and setting 2 it is longitudinally reinforced Lateral stiffening plate between plate, the vertical longitudinally reinforced plate of lateral stiffening plate.Using such design, to avoid crossing cabin part because temperature becomes When changing and deforming, the risk factors such as friction or even spark occur between stiffening plate 3 and bulkhead.The company of panel 1 and support plate 2 The place of connecing is provided with multiple gussets 4, and gusset 4 is set to the outside of support plate 2, and the width of gusset 4 is equal to the width of support plate 2, muscle It is to be welded to connect between plate 4 and panel 1, gusset 4 and support plate 2.
The installation method of the present embodiment are as follows: crossing cabin part opens up corresponding with perforation hole 6 when installing and using on bulkhead Crossing cabin hole, the aperture in crossing cabin hole is greater than the aperture of perforation hole 6, in order to passing through for cryotronl, and guarantees that cryotronl will not be with cabin Wall contact.Support plate 2 and bulkhead, panel 1 and annular compound plate 5 are welded by the way of deep penetration welding, cryotronl is sequentially passed through Annular compound plate 5 is welded with cryotronl, completes the process that cryotronl is passed through to bulkhead by crossing cabin hole and perforation hole 6.
As shown in figure 4, sizing grid is not greater than 150 millimeters of x, 510 millimeters of mm according to Lloyd's Register of Shipping's standard, so The grid of 80 millimeters 80 millimeters of x of selection is calculated, the stress value of crossing cabin part is tested.Standard points out that allowable stress should be surrender Stress i.e. 1.2 times of 235 megapascal, so maximum permissible stress is 282 megapascal.It is maximum it can be seen from Stress calculation cloud atlas Stress value is 170 megapascal, meets allowable stress requirement.
Although above-described embodiment makes specific descriptions to the present invention, come for those of ordinary skill in the art It says, it is understood that can be modified within spirit and scope of the invention based on present disclosure not departing from Or improve, these modification and improvement are all within spirit and scope of the invention.

Claims (7)

1. a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship, which is characterized in that including panel (1) and support plate (2), the face Plate (1) is all made of low temperature stainless steel with the support plate (2) and is made, circumferential direction of the support plate (2) along the panel (1) Setting, the support plate (2) is vertical with the panel (1), runs through on the panel (1) and is above provided at least one perforation hole (6), the circumferential direction along the perforation hole (6) is provided with annular compound plate (5), and the length of the annular compound plate (5) is greater than the panel (1) thickness, the both ends of the annular compound plate (5) are located at the two sides of the panel (1), and the annular compound plate (5) is located at described The length of support plate (2) side is less than the length of the support plate (2), when the latus rectum of the cryotronl is less than 500 millimeters, institute State annular compound plate (5) with a thickness of 6 millimeters, when the latus rectum of the cryotronl be more than or equal to 500 millimeters when, it is described annular compound plate (5) with a thickness of 8 millimeters.
2. a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship as described in claim 1, which is characterized in that the panel (1) The side that middle part is located at the support plate is provided with stiffening plate (3), the stiffening plate (3) and the panel (1), the support plate It (2) is to be welded to connect between the panel (1), the length of the stiffening plate (3) is less than the length of the support plate (2).
3. a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship as claimed in claim 2, which is characterized in that the stiffening plate (3) 3 are set as, is added including the transverse direction between 2 longitudinally reinforced plates of 2 longitudinal directions longitudinally reinforced plate disposed in parallel and setting Strong plate, the vertical longitudinally reinforced plate of the transverse direction stiffening plate.
4. a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship as claimed in claim 2, which is characterized in that the stiffening plate (3) Width it is 10 millimeters smaller than the width of the support plate (2).
5. a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship as claimed in claim 4, which is characterized in that the panel (1) with The junction of the support plate (2) is provided with multiple gussets (4), and the gusset (4) is set to the outside of the support plate (2), The width of the gusset (4) is equal to the width of the support plate (2), the gusset (4) and the panel (1), the gusset (4) It is to be welded to connect between the support plate (2).
6. a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship as claimed in claim 5, which is characterized in that the panel (1), The support plate (2), the stiffening plate (3), the gusset (4) thickness be 12 millimeters.
7. a kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship as described in claim 1, which is characterized in that the annular compound plate (5) it is connect between the panel (1) for deep penetration welding.
CN201910463130.1A 2019-05-30 2019-05-30 A kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship Pending CN110145644A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910463130.1A CN110145644A (en) 2019-05-30 2019-05-30 A kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910463130.1A CN110145644A (en) 2019-05-30 2019-05-30 A kind of dedicated multi-joint cryotronl crossing cabin part of LNG ship

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110498023A (en) * 2019-08-30 2019-11-26 广船国际有限公司 A kind of design method of transfer platform and stiffening plate

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1372072A (en) * 1962-08-15 1964-09-11 Kobe Steel Works Coated collecting tube and similar device
DE1922549U (en) * 1962-08-15 1965-09-02 Kobe Steel Ltd PIPE-PANEL CONNECTION.
DE2318873A1 (en) * 1973-04-11 1974-10-24 Kraftwerk Union Ag PIPING ENTRY, IN PARTICULAR FROM A HOT STEAM PIPING OF A TURBINE SYSTEM
KR20120019895A (en) * 2010-08-27 2012-03-07 삼성중공업 주식회사 Piping member penetration structure
CN206347211U (en) * 2016-12-23 2017-07-21 无锡宝宏船舶机械有限公司 Thick deck crossing cabin part
CN208381507U (en) * 2018-04-17 2019-01-15 沪东中华造船(集团)有限公司 A kind of ultralow temperature piping crossing cabin sealing device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1372072A (en) * 1962-08-15 1964-09-11 Kobe Steel Works Coated collecting tube and similar device
DE1922549U (en) * 1962-08-15 1965-09-02 Kobe Steel Ltd PIPE-PANEL CONNECTION.
DE2318873A1 (en) * 1973-04-11 1974-10-24 Kraftwerk Union Ag PIPING ENTRY, IN PARTICULAR FROM A HOT STEAM PIPING OF A TURBINE SYSTEM
KR20120019895A (en) * 2010-08-27 2012-03-07 삼성중공업 주식회사 Piping member penetration structure
CN206347211U (en) * 2016-12-23 2017-07-21 无锡宝宏船舶机械有限公司 Thick deck crossing cabin part
CN208381507U (en) * 2018-04-17 2019-01-15 沪东中华造船(集团)有限公司 A kind of ultralow temperature piping crossing cabin sealing device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110498023A (en) * 2019-08-30 2019-11-26 广船国际有限公司 A kind of design method of transfer platform and stiffening plate
CN110498023B (en) * 2019-08-30 2021-07-06 广船国际有限公司 Design method of reinforcing plate of oil transportation platform

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Application publication date: 20190820

RJ01 Rejection of invention patent application after publication