CN106995036B - The restorative procedure of diamond shape independent liquid cargo tank protective layer - Google Patents

The restorative procedure of diamond shape independent liquid cargo tank protective layer Download PDF

Info

Publication number
CN106995036B
CN106995036B CN201610044427.0A CN201610044427A CN106995036B CN 106995036 B CN106995036 B CN 106995036B CN 201610044427 A CN201610044427 A CN 201610044427A CN 106995036 B CN106995036 B CN 106995036B
Authority
CN
China
Prior art keywords
protective layer
area
repaired
cargo tank
defect
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.)
Active
Application number
CN201610044427.0A
Other languages
Chinese (zh)
Other versions
CN106995036A (en
Inventor
陈建平
陈兵
李小灵
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.)
Jiangnan Shipyard Group Co Ltd
Original Assignee
Jiangnan Shipyard 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 Jiangnan Shipyard Group Co Ltd filed Critical Jiangnan Shipyard Group Co Ltd
Priority to CN201610044427.0A priority Critical patent/CN106995036B/en
Publication of CN106995036A publication Critical patent/CN106995036A/en
Application granted granted Critical
Publication of CN106995036B publication Critical patent/CN106995036B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B71/00Designing vessels; Predicting their performance
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B11/00Interior subdivision of hulls
    • B63B11/02Arrangement of bulkheads, e.g. defining cargo spaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B81/00Repairing or maintaining vessels

Abstract

The present invention provides a kind of restorative procedure of diamond shape independent liquid cargo tank protective layer; the protective layer is laid on the insulating layer of the cargo tank, and the reparation of the protective layer includes mainly inspection to protective layer, determines area to be repaired, cleaned to area to be repaired, being repaired to area to be repaired.The present invention is according to the difference of protective layer defect kind, using different restorative procedures, it is ensured that the laying covering of protective layer energy continuous uniform is on the insulating layer, it is ensured that the insulating layer of cargo tank is not damaged by the external world.The advantage that there are also repairing effects is good by the present invention, repairing quality is high.

Description

The restorative procedure of diamond shape independent liquid cargo tank protective layer
Technical field
The present invention relates to the restorative procedures of diamond shape independent liquid cargo tank protective layer in liquefied gas carrier more particularly to liquefied gas carrier.
Background technique
The design temperature of large-scale full-cool liquefied gas carrier (VLGC) is generally -50 degree.Diamond shape independent tank is independent liquid goods The one kind in cabin, diamond shape independent liquid cargo tank (hereinafter referred to as cargo tank) load cargo temperature it is low, it is therefore necessary to a set of row it Effective insulation system achievees the effect that keep the temperature and prevent temperature from spreading.Currently, the insulation system of cargo tank is mainly by insulating Insulating layer (abbreviation insulating layer) and sealer (abbreviation protective layer) two parts composition.This two-part laying must have strictly Operational procedure to ensure reliable in quality.Also there is stringent inspection to check that program, accurate detection go out to protect after the completion of construction Existing for sheath the defects of crackle, and repair in time.If the defect of the protective layer cannot repair in time, can to insulate Layer loses due protection and becomes easy and be damaged.And once insulating layer is damaged, breakage will form notch, in turn So that the thermal insulating ability decline of entire cargo tank, also affects the operation of hull if serious.Therefore, how high in time It is those skilled in the art's technical issues that need to address that defective protective layer is repaired on effect ground.
Summary of the invention
The technical problem to be solved in the present invention is that providing a kind of diamond shape independent liquid cargo tank guarantor with strong points, reliable operation The restorative procedure of sheath.
In order to solve the above-mentioned technical problem, the present invention adopts the following technical scheme that:A kind of diamond shape independent liquid cargo tank protective layer Restorative procedure, the protective layer is laid on the insulating layer of the cargo tank, and the reparation of the protective layer includes the following steps:
After S1, protective layer are laid, check protective layer thering is the region of crackle and defect to make a mark and conduct Area to be repaired;
S2, area to be repaired is cleaned using detergent;
S3, the temperature and humidity for measuring repairing environment, the temperature of area to be repaired are higher than 0 DEG C, and 5 DEG C~50 DEG C of room temperature, Humidity is not higher than 75%;
S4, when area to be repaired is that crackle and maximum width are less than or equal to 1mm, spray new protective layer, spraying area edge Crackle peripherally and outwardly extend at least 200mm;When area to be repaired is crackle and maximum width is greater than 1mm, first in crackle Filler is filled, then sprays new protective layer, spraying area peripherally and outwardly extends at least 200mm along crackle;Work as area to be repaired For defect and when defect area is greater than 3mm2, defect area is first expanded at least one times, is then filled in the defect after expansion Filler, finally sprays new protective layer, spraying area along defect after expansion peripherally and outwardly extension at least 200mm.
Preferably, in S2, the detergent is ethylene glycol ethyl ether or methylene chloride.
Preferably, in S4, when area to be repaired is crackle and maximum width is greater than 1mm, after filling filler 3~5 days New protective layer is sprayed again.
Preferably, in S4, when area to be repaired is defect and defect area is greater than 3mm2, after filling filler 3~5 days New protective layer is sprayed again.
Preferably, in S4, when area to be repaired is crackle and maximum width is less than or equal to 1mm, new protection thickness Degree is not more than 1mm.
Preferably, in S4, when area to be repaired is crackle and maximum width is greater than 1mm, the thickness of new protective layer is not Greater than 1mm.
Preferably, in S4, when area to be repaired is defect and defect area is greater than 3mm2, the thickness of new protective layer is not Greater than 1mm.
Preferably, in S4, when repairing area to be repaired, a room temperature and humidity, room temperature and humidity are recorded per hour Repair when job requirement is unsatisfactory for suspend.
As described above, the restorative procedure of diamond shape independent liquid cargo tank protective layer of the present invention, has the advantages that:
The present invention is according to the difference of cargo tank protective layer defect kind, using different restorative procedures, it is ensured that protective layer The laying covering of energy continuous uniform is on the insulating layer, it is ensured that the insulating layer of cargo tank is not damaged by the external world.Through the invention to guarantor The repairing effect that sheath carries out specific aim reparation is good, repairing quality is high, guarantees the integrality of cargo tank protective layer entirety.
Detailed description of the invention
Fig. 1 is the cargo tank structure sectional view in the present invention.
Fig. 2 is the first crackle view of protective layer in the present invention.
Fig. 3 is the reparation view of the first crackle of protective layer in the present invention.
Fig. 4 is second of crackle view of protective layer in the present invention.
Fig. 5 is the reparation view of second of crackle of protective layer in the present invention.
Fig. 6 is protective layer defect view in the present invention.
Fig. 7 is the reparation view of protective layer defect in the present invention.
In figure:1, cargo tank 2, insulating layer
3, protective layer 31, new protective layer
32, new protective layer 33, new protective layer
4, crackle 5, crackle
51, filler 6, defect
61, filler
Specific embodiment
Structure depicted in Figure of description, ratio, size etc., only to cooperate the revealed content of specification, with Understand for those skilled in the art and read, be not intended to limit the invention enforceable qualifications, therefore does not have technically Essential meaning, the modification of any structure, the change of proportionate relationship or the adjustment of size can be generated not influencing the present invention Under effect and the purpose that can reach, should all still it fall in the range of disclosed technology contents can cover.Meanwhile Cited such as "upper", "lower", "front", "rear", " centre " term in this specification are merely convenient to being illustrated for narration, and It is non-that to limit the scope of the invention, relativeness is altered or modified, under the content of no substantial changes in technology, when Also it is considered as the enforceable scope of the present invention.
Diamond shape independent liquid cargo tank is one kind of independent liquid cargo tank, is placed in liquefied gas carrier and is used to load oil gas or natural The cryogenic cargos such as gas.In order to allow independent liquid cargo tank (hereinafter referred to as cargo tank) to play the role of keeping the temperature and prevent temperature from spreading, such as Shown in Fig. 1, need successively to lay insulating layer 2 and protective layer 3 in the outer surface of cargo tank 1, the insulating layer 2 plays heat-insulation and heat-preservation Effect, protective layer 3 is laid on insulating layer 2 and plays a protective role to insulating layer 2.The present invention is the reparation of the protective layer 3 Method, specifically, the reparation of the protective layer 3 includes the following steps in conjunction with Fig. 1-Fig. 7:
Firstly, check after the laying of protective layer 3 is good and is fully cured protective layer 3, there are crackle and defect Region makes a mark and as area to be repaired.When inspection, the length and width of crackle is measured with graduated scale by manually estimating, Go out the area of defect by the size estimation of measurement.In addition, then protective layer 3 answers hand herein for that can tear the protective layer 3 fallen manually It is dynamic to remove and wait subsequent unified reparation.In this step by the data markers measured area to be repaired or unified record in order to It is subsequent that different defects are targetedly repaired.
After protective layer 3 checks well, area to be repaired is cleaned using detergent, removal dust, oil, rouge and water Deng.The detergent is the detergents such as ethylene glycol ethyl ether or methylene chloride.
After area to be repaired is cleaned, the temperature and humidity of repairing environment is measured, the temperature of area to be repaired is higher than 0 DEG C, 5 DEG C~50 DEG C of room temperature, humidity is not higher than 75%.Because new protective layer 31 is to spray the insulating layer 2 that is laid in fluid form On, if area to be repaired temperature is lower than 0 DEG C, new protective layer 31 is easy to freeze, and is unfavorable for carrying out defective locations effective Ground reparation;And room temperature is too low or the excessively high bonding that also will affect new protective layer 31 with insulating layer 2;Humidity is excessive to will lead to new protection Layer 31 should not solidify.
After above-mentioned work is carried out, start to repair area to be repaired, uses different reparations for different defects Method.With reference to Fig. 2, Fig. 3, when area to be repaired is crackle 4 and maximum width is less than or equal to 1mm, the new protective layer of direct spraying 31, by verification experimental verification, spraying area enables to this area to be repaired when peripherally and outwardly extending at least 200mm along crackle 4 New protective layer 31 and original 3 transition of protective layer it is abundant, bonding effect is more preferable.Because new protective layer 31 is to spray in liquid form It applies, so a small amount of new protective layer 31, which can penetrate into crackle 4, plays repair when spraying.It is new to protect when repairing this defect The thickness of layer 31 is not more than 1mm.After having sprayed new protective layer 31, the sum of the thickness of new protective layer 31 and original protective layer 3 It is greater than 1mm..
With reference to Fig. 4, Fig. 5, when area to be repaired is crackle 5 and maximum width is greater than 1mm, need first to fill in crackle Then filler 51 sprays new protective layer 32.By verification experimental verification, spraying area peripherally and outwardly extends at least 200mm along crackle 5 When enable to the new protective layer 32 of this area to be repaired and original 3 transition of protective layer abundant, bonding effect is good.The filler 51 be Ma Supreme Being rouge or sealed binder.When repairing this defect, in order to guarantee repairing effect, sprayed again after filling filler 3~5 days Then new protective layer 32 sprays new protective layer 32 according to the solidification situation of filler the purpose is to first filler be allowed to be fully cured.By Test is drawn a conclusion:Spraying that new protective layer 32 is ideal after filling 3 days of filler, filler solidification effect at this time is good, The whole duty cycle can be effectively ensured.When practical operation, need before spraying new protective layer 32 first to having had been filled with Filler 51 is checked:Whether the thickness for first checking for filler 51 meets the requirements, ungratified to be modified, is levelling;Then again It sees whether filler 51, protective layer 3 and insulating layer 2 bond completely, is unsatisfactory for being filled again with filler 51 for bonding requirement, Zhi Daoman Sufficient job requirement.When repairing this defect, in order to save filler while guaranteeing repairing effect, the thickness of new protective layer 32 is little In 1mm.After having sprayed new protective layer 32, the sum of the thickness of new protective layer 32 and original protective layer 3 is greater than 1mm..
With reference to Fig. 6, Fig. 7, when area to be repaired is defect 6 and defect area is greater than 3mm2, first 6 area of defect is expanded At least one times, filler then is filled in the defect after expansion, finally sprays new protective layer 33, spraying area is lacked along after expansion The peripherally and outwardly extension at least 200mm of damage.Why the area of defect 6 is expanded, is the protective layer 3 because of 6 edge of defect More crisp, the protective layer 3 that 6 edge of defect is likely to result in when spraying new protective layer 33 is broken, so influence new protective layer 33 with The bonding effect of protective layer 3 originally.By verification experimental verification, spraying area along defect after expansion peripherally and outwardly extension at least When 200mm, enable to the new protective layer 33 of this area to be repaired and original 3 transition of protective layer abundant, bonding effect is more preferable. The filler 61 is Ma Supreme Being rouge or sealed binder.When repairing this defect, in order to guarantee repairing effect, in filling filler 3~5 days Spray new protective layer 33 again afterwards, purpose is also first filler to be allowed to be fully cured, and then sprays new protect according to the solidification situation of filler Sheath 33.It draws a conclusion through overtesting:Spray that new protective layer 33 is ideal after filling 5 days of filler, filler at this time is solid Change works well, and the whole duty cycle can be effectively ensured.When practical operation, spray before new protective layer 33 first to filler 61 It is checked, whether the thickness that also first check for filler 61 meets the requirements, ungratified to be modified, is levelling;Then it sees again Whether filler 61, protective layer 3 and insulating layer 2 bond completely, being filled again with filler 61 for bonding requirement are unsatisfactory for, until meeting Job requirement.When repairing this defect, in order to save filler while guaranteeing repairing effect, the thickness of new protective layer 33 is not more than 1mm.After having sprayed new protective layer 33, the sum of the thickness of new protective layer 33 and original protective layer 3 is greater than 1mm..
When occurring defect of the area no more than 3mm2 on protective layer 3, visually it is hardly visible, whole to cargo tank 1 Influence also can be ignored substantially, therefore not need to be repaired.And when occurring intensive needle pore defect on protective layer 3, Directly new protective layer is sprayed in defect area.
In practical operation, no matter which kind of defect is repaired, requires to record a room temperature and humidity, room per hour Mild humidity is unsatisfactory for patch work when job requirement and suspends, and then uses the relevant devices such as thermoregulator, dehumidifier by room In mild humidity regulation to claimed range, or is handled by shipyard according to special status and restart repair.
In conclusion the restorative procedure of diamond shape independent liquid cargo tank protective layer of the present invention, it can be effectively to the protection of cargo tank Layer is repaired, reliable operation, high-efficient.So the present invention effectively overcome some practical problems in the prior art to There is very high utility value and uses meaning.
The principle of the present invention and its effect is only illustrated in above embodiment, and is not intended to limit the present invention.This hair It is bright to be improved under the premise of without prejudice to overall thought there are many more aspect, it all can be for those skilled in the art Without prejudice under spirit and scope of the invention, can carry out modifications and changes to above-described embodiment.Therefore, technical field such as Middle all equivalent modifications for being completed without departing from the spirit and technical ideas disclosed in the present invention of tool usually intellectual or Change, should be covered by the claims of the present invention.

Claims (8)

1. a kind of restorative procedure of diamond shape independent liquid cargo tank protective layer, the protective layer is laid in the insulating layer of the cargo tank On, which is characterized in that the reparation of the protective layer includes the following steps:
After S1, protective layer are laid, check protective layer thering is the region of crackle and defect to make a mark and as to be repaired Multiple region;
S2, area to be repaired is cleaned using detergent;
S3, the temperature and humidity for measuring repairing environment, the temperature of area to be repaired are higher than 0 DEG C, and 5 DEG C~50 DEG C of room temperature, humidity Not higher than 75%;
S4, when area to be repaired is that crackle and maximum width are less than or equal to 1mm, spray new protective layer, spraying area is along splitting Line peripherally and outwardly extends at least 200mm;When area to be repaired is crackle and maximum width is greater than 1mm, first filled in crackle Filler, then sprays new protective layer, and spraying area peripherally and outwardly extends at least 200mm along crackle;When area to be repaired is scarce Damage and defect area be greater than 3mm2 when, first by defect area expand at least one times, then fill filler in the defect after expansion, Finally spray new protective layer, spraying area along defect after expansion peripherally and outwardly extension at least 200mm.
2. the restorative procedure of diamond shape independent liquid cargo tank protective layer according to claim 1, it is characterised in that:In S2, institute Stating detergent is ethylene glycol ethyl ether or methylene chloride.
3. the restorative procedure of diamond shape independent liquid cargo tank protective layer according to claim 1, it is characterised in that:In S4, when For crackle and when maximum width is greater than 1mm, filling sprays new protective layer after filler 3~5 days again for area to be repaired.
4. the restorative procedure of diamond shape independent liquid cargo tank protective layer according to claim 1, it is characterised in that:In S4, when For defect and when defect area is greater than 3mm2, filling sprays new protective layer after filler 3~5 days again for area to be repaired.
5. the restorative procedure of diamond shape independent liquid cargo tank protective layer according to claim 1, it is characterised in that:In S4, when For crackle and when maximum width is less than or equal to 1mm, the new degree for protecting thickness is not more than 1mm for area to be repaired.
6. the restorative procedure of diamond shape independent liquid cargo tank protective layer according to claim 1, it is characterised in that:In S4, when For crackle and when maximum width is greater than 1mm, the thickness of new protective layer is not more than 1mm for area to be repaired.
7. the restorative procedure of diamond shape independent liquid cargo tank protective layer according to claim 1, it is characterised in that:In S4, when For defect and when defect area is greater than 3mm2, the thickness of new protective layer is not more than 1mm for area to be repaired.
8. the restorative procedure of diamond shape independent liquid cargo tank protective layer according to claim 1, it is characterised in that:In S4, When repairing area to be repaired, records a room temperature per hour and humidity, room temperature and humidity are unsatisfactory for repair when job requirement Pause.
CN201610044427.0A 2016-01-22 2016-01-22 The restorative procedure of diamond shape independent liquid cargo tank protective layer Active CN106995036B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610044427.0A CN106995036B (en) 2016-01-22 2016-01-22 The restorative procedure of diamond shape independent liquid cargo tank protective layer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610044427.0A CN106995036B (en) 2016-01-22 2016-01-22 The restorative procedure of diamond shape independent liquid cargo tank protective layer

Publications (2)

Publication Number Publication Date
CN106995036A CN106995036A (en) 2017-08-01
CN106995036B true CN106995036B (en) 2018-11-16

Family

ID=59428713

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610044427.0A Active CN106995036B (en) 2016-01-22 2016-01-22 The restorative procedure of diamond shape independent liquid cargo tank protective layer

Country Status (1)

Country Link
CN (1) CN106995036B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113277033B (en) * 2021-05-24 2022-11-11 中国舰船研究设计中心 Minor bulkhead crack repair method
JP2024510062A (en) * 2022-01-24 2024-03-06 寧徳時代新能源科技股▲分▼有限公司 Housing and its repair method, related secondary batteries, battery modules, battery packs, and power consumption devices

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1268088A2 (en) * 2000-03-16 2003-01-02 Volkswagen Aktiengesellschaft Method for removing minor lacquer imperfections
JP3826803B2 (en) * 2002-02-05 2006-09-27 日産自動車株式会社 How to repair the coating
JP2008086958A (en) * 2006-10-04 2008-04-17 Nippon Paint Co Ltd Method of repairing laminated coated film
CN101216141A (en) * 2008-01-04 2008-07-09 中国航空工业第一集团公司北京航空材料研究院 Pipeline damage rehabilitation method
CN102335804A (en) * 2010-07-21 2012-02-01 贵州贵航无人机有限责任公司 Method for repairing metal skin by using composite material
JP5056557B2 (en) * 2008-04-14 2012-10-24 日産自動車株式会社 How to repair a super-metallic coating film
CN103484021A (en) * 2013-09-05 2014-01-01 上海杰阳实业有限公司 Small-area damage repairing liquid and repairing process for oil paint surface of wood facing
CN104439886A (en) * 2014-10-21 2015-03-25 山东钢铁股份有限公司 Sticking and reinforcing device and sticking and repairing method for cracks on cast iron outer shell of diffusion pump of vacuum furnace
CN104624458A (en) * 2015-02-15 2015-05-20 无锡市崇安区科技创业服务中心 Automobile paint repair method

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1268088A2 (en) * 2000-03-16 2003-01-02 Volkswagen Aktiengesellschaft Method for removing minor lacquer imperfections
JP3826803B2 (en) * 2002-02-05 2006-09-27 日産自動車株式会社 How to repair the coating
JP2008086958A (en) * 2006-10-04 2008-04-17 Nippon Paint Co Ltd Method of repairing laminated coated film
CN101216141A (en) * 2008-01-04 2008-07-09 中国航空工业第一集团公司北京航空材料研究院 Pipeline damage rehabilitation method
JP5056557B2 (en) * 2008-04-14 2012-10-24 日産自動車株式会社 How to repair a super-metallic coating film
CN102335804A (en) * 2010-07-21 2012-02-01 贵州贵航无人机有限责任公司 Method for repairing metal skin by using composite material
CN103484021A (en) * 2013-09-05 2014-01-01 上海杰阳实业有限公司 Small-area damage repairing liquid and repairing process for oil paint surface of wood facing
CN104439886A (en) * 2014-10-21 2015-03-25 山东钢铁股份有限公司 Sticking and reinforcing device and sticking and repairing method for cracks on cast iron outer shell of diffusion pump of vacuum furnace
CN104624458A (en) * 2015-02-15 2015-05-20 无锡市崇安区科技创业服务中心 Automobile paint repair method

Also Published As

Publication number Publication date
CN106995036A (en) 2017-08-01

Similar Documents

Publication Publication Date Title
CN106995036B (en) The restorative procedure of diamond shape independent liquid cargo tank protective layer
CN106760560B (en) Complicated arc list construction of Pyramid engineering method
Tay et al. Predicting delamination in plastic IC packages and determining suitable mold compound properties
CN103736645B (en) RTV anti-pollution flashover coating recoating method of insulator coated with RTV anti-pollution flashover coating
CN103515327B (en) Kovar metal structure for laser seal welding and laser welding method
CA2419240A1 (en) Method for estimating and reducing uncertainties in process measurements
CN102331328A (en) Field hydrostatic test method for water-proof system of building deformation joint
CN108867230A (en) A kind of method for repairing and mending of asphalt pavement crack
CN109435258A (en) A kind of encapsulating method of wind turbine blade root connection system
CN109740252B (en) Method for evaluating early-stage freezing performance of concrete by utilizing transient temperature field analysis
CN105292377B (en) The test method of wooden model anchor lip
CN110027229A (en) A kind of defect mending method based on the integrally formed heat insulation material of recoverable airship
CN205981088U (en) Foil gage seal structure
CN106114538A (en) A kind of adhering method of low-floor rail vehicle outer plaque
CN110439314A (en) A kind of heat preserving exterior wall infiltration repairerment method
CN104875983B (en) Holding vessel with macromolecular material multiple-anticorrosion inwall and construction technology
CN104537458A (en) Method and system for risk assessment of polycrystalline silicon production pressure vessels
CN109036824B (en) Dry-type air-core reactor full-encapsulation protection process method
CN107966233B (en) stress-strain testing method for metal hydride hydrogen storage tank
CN106994433A (en) The restorative procedure of rhombus independent liquid cargo tank insulating barrier
CN105711756B (en) The installation method of the vertical bearing insulation of A type independent liquid cargo tank inside bottom surfaces
CN104743135B (en) Strain gauge protection method
CN113640298A (en) Transmission system RTV coating defect detection method and system
CN103344749A (en) Method for observing rusted cracks of reinforced concrete based on two-stage rust crack model
CN102966049B (en) Method for treating vertical crack of reinforced concrete bridge abutment

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant