CN1333198C - High vacuum heat insulation low temperature liquefied gas storage tank - Google Patents
High vacuum heat insulation low temperature liquefied gas storage tank Download PDFInfo
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- CN1333198C CN1333198C CNB2004100090131A CN200410009013A CN1333198C CN 1333198 C CN1333198 C CN 1333198C CN B2004100090131 A CNB2004100090131 A CN B2004100090131A CN 200410009013 A CN200410009013 A CN 200410009013A CN 1333198 C CN1333198 C CN 1333198C
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D88/00—Large containers
- B65D88/02—Large containers rigid
- B65D88/12—Large containers rigid specially adapted for transport
- B65D88/128—Large containers rigid specially adapted for transport tank containers, i.e. containers provided with supporting devices for handling
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/08—Mounting arrangements for vessels
- F17C13/083—Mounting arrangements for vessels for medium-sized mobile storage vessels, e.g. tank vehicles or railway tank vehicles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/08—Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/03—Orientation
- F17C2201/035—Orientation with substantially horizontal main axis
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/054—Size medium (>1 m3)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/01—Reinforcing or suspension means
- F17C2203/011—Reinforcing means
- F17C2203/012—Reinforcing means on or in the wall, e.g. ribs
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/01—Reinforcing or suspension means
- F17C2203/014—Suspension means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0337—Granular
- F17C2203/0341—Perlite
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0391—Thermal insulations by vacuum
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0626—Multiple walls
- F17C2203/0629—Two walls
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/01—Mounting arrangements
- F17C2205/0103—Exterior arrangements
- F17C2205/0107—Frames
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/01—Mounting arrangements
- F17C2205/0123—Mounting arrangements characterised by number of vessels
- F17C2205/0126—One vessel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/22—Assembling processes
- F17C2209/221—Welding
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/23—Manufacturing of particular parts or at special locations
- F17C2209/232—Manufacturing of particular parts or at special locations of walls
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/032—Hydrocarbons
- F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/03—Dealing with losses
- F17C2260/031—Dealing with losses due to heat transfer
- F17C2260/033—Dealing with losses due to heat transfer by enhancing insulation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0165—Applications for fluid transport or storage on the road
- F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
- F17C2270/0171—Trucks
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
本发明提供了一种高真空多层绝热低温液化气体储罐,其包括框架和罐体,罐体由外壳、内胆和连接外壳与内胆的组合支承结构组成,组合支承结构仅设置罐体两端的内外封头之间,就能承受径向载荷和轴向载荷,内胆和外壳的传热面积小,支承结构承载力大,内胆有效装载容积大。
The invention provides a high-vacuum multi-layer heat-insulated low-temperature liquefied gas storage tank, which includes a frame and a tank body. The tank body is composed of an outer shell, an inner tank, and a combined supporting structure connecting the outer shell and the inner tank. The combined supporting structure is only provided with the tank body Between the inner and outer heads at both ends, it can bear radial load and axial load, the heat transfer area of the inner tank and the outer shell is small, the bearing capacity of the supporting structure is large, and the effective loading volume of the inner tank is large.
Description
技术领域technical field
本发明涉及的是一种低温液化气体储运设备,更具体地说是涉及高真空绝热低温液化气储罐,其可以是适于高效地运输低温液化气体的罐车或罐式集装箱。本发明通过具备优越的抗冲击能力与隔热能力的小间隙高真空多层绝热内支承结构,实现了低温液化气体储运设备在运行过程中承受的冲击力和承运介质温度变化满足低温液化气体储运的要求,而且低温容器内胆和外筒之间的真空层最薄,最终实现低温液化气体的装载率最大。本发明属于低温工程与低温技术领域。The present invention relates to a low-temperature liquefied gas storage and transportation equipment, and more specifically relates to a high-vacuum heat-insulated low-temperature liquefied gas storage tank, which may be a tank truck or a tank container suitable for efficiently transporting low-temperature liquefied gas. The present invention realizes that the impact force and the temperature change of the carrier medium that the low-temperature liquefied gas storage and transportation equipment bears during the operation process meet the requirements of the low-temperature liquefied gas The requirements for storage and transportation, and the vacuum layer between the inner tank and the outer cylinder of the cryogenic container is the thinnest, and finally the loading rate of the cryogenic liquefied gas is maximized. The invention belongs to the field of cryogenic engineering and cryogenic technology.
背景技术Background technique
诞生于1909年的真空一粉末绝热技术使得低温储罐的性能有了极大的提高。到上世纪30年代末,真空一粉末绝热已广泛应用于以空气分离和液化为代表的整个低温领域。在上世纪50年代初,高真空多层绝热出现了,它是低温绝热历史上的一个重要发展,特别是在50年代末期,由于空间技术的发展,液氢、液氦的用量猛增,大大推动了高真空多层绝热的研究与应用,其中,运输低温液化气体的罐车和罐式集装箱就是主要的应用产品。The vacuum-powder insulation technology, born in 1909, has greatly improved the performance of cryogenic storage tanks. By the end of the 1930s, vacuum-powder insulation had been widely used in the entire low-temperature field represented by air separation and liquefaction. In the early 1950s, high-vacuum multilayer insulation appeared, which was an important development in the history of low-temperature insulation. Especially in the late 1950s, due to the development of space technology, the amount of liquid hydrogen and liquid helium increased sharply, greatly Promoted the research and application of high-vacuum multi-layer insulation, among which tank trucks and tank containers for transporting cryogenic liquefied gases are the main application products.
在低温技术领域,低温液化气体指-160℃以下以液体形式存在的气体,例如液氧、液氮、液氩、液氢、液氦、液体甲烷及LNG等。由于这类气体的液态体积比气态缩小600倍左右,因此往往以液态的方式储运。运输低温液化气体的设备,包括罐车和罐箱等,罐体是双层结构,内胆和外壳之间是真空层,内胆和外壳通过支承结构连接,由于运输法规的要求,储运设备(罐车和罐箱等)都有最大的外形尺寸限制,在限制了最大外形尺寸的情况下,储运设备(罐车和罐箱等)能装运的介质的有效容积就取决于真空层的厚度。In the field of cryogenic technology, cryogenic liquefied gases refer to gases that exist in liquid form below -160°C, such as liquid oxygen, liquid nitrogen, liquid argon, liquid hydrogen, liquid helium, liquid methane, and LNG. Since the liquid volume of this type of gas is about 600 times smaller than that of the gaseous state, it is often stored and transported in a liquid state. Equipment for transporting cryogenic liquefied gas, including tank trucks and tank containers, etc. The tank body is a double-layer structure, and there is a vacuum layer between the inner tank and the outer shell. The inner tank and the outer shell are connected by a supporting structure. Due to the requirements of transportation regulations, storage and transportation equipment ( Tank trucks and tank containers, etc.) have a maximum external dimension limit. In the case of limiting the maximum external dimensions, the effective volume of the medium that can be shipped by storage and transportation equipment (tank trucks and tank containers, etc.) depends on the thickness of the vacuum layer.
真空-粉末绝热罐车和罐箱是目前国内较为普遍的低温运输设备,是通过在外壳和内胆之间的真空层加珍珠岩等来实现隔热,为了达到满意的隔热效果,真空层较为厚,通常真空层厚度在200~300毫米,因此,实际装运货物的有效容积就被牺牲了;加上珍珠岩在运输过程中的沉积,使运输设备的隔热性能受到影响。于是,高真空多层绝热技术在运输设备中的应用被推广起来。实用新型ZL00216678.X、ZL00249960.6、ZL01272605.2就是高真空多层绝热技术在运输设备中的应用案例。Vacuum-powder insulation tank trucks and tank containers are relatively common low-temperature transportation equipment in China at present. The heat insulation is achieved by adding perlite to the vacuum layer between the shell and the inner tank. In order to achieve a satisfactory heat insulation effect, the vacuum layer is more Thick, usually the thickness of the vacuum layer is 200~300 mm, therefore, the effective volume of the actual shipment is sacrificed; plus the deposition of perlite during transportation, the heat insulation performance of the transportation equipment is affected. Therefore, the application of high-vacuum multi-layer insulation technology in transportation equipment has been promoted. Utility models ZL00216678.X, ZL00249960.6, and ZL01272605.2 are examples of the application of high-vacuum multilayer insulation technology in transportation equipment.
高真空多层绝热储运设备(罐车和罐箱等)是在罐体内胆的外表面缠绕隔热材料,通过把包含多层隔热材料的真空夹层抽高真空而形成绝热层,真空夹层越薄,罐体装载运输介质越多;但是绝热层越薄,连接内胆和外壳的支承结构越难布置,绝热层越薄,高真空度越低,内胆和外壳的传热越多,低温液化气体的热量损失越大,目前多层绝热技术,如ZL00249960.6和ZL01272605.2中,考虑到真空层中径向支撑的布置,外壳和内胆之间的真空层厚度也不得不在100毫米左右。内胆和外壳的内支承结构既要能够承受由于液体负荷、储罐重量以及相应冲击加速度所产生的力,还必须尽可能减少内支承结构所引起的漏热量,所以内支承结构是低温储罐设计的关键。已有的技术中,国内外目前采用的低温储罐上内支承结构有:1)内胆和外壳间的绝热垫块结构,但不能有效解决高真空多层绝热间距小引起支承漏热量大的问题和内筒体热胀冷缩所引起的高真空多层绝热层破坏或间断的问题;2)内外封头间不锈钢套管结构,制作困难、内外封头的间距大及抗冲击能力差,且漏热量比较大;3)吊拉带结构,不能有效解决热胀冷缩引起的抗冲击能力下降问题;4)实用新型ZL00216678.X的低温容器抗强冲击支承结构,要求封头间距大及常温转入低温时接触间隙增大,抗冲击水平降低。High-vacuum multi-layer heat insulation storage and transportation equipment (tank trucks and tank containers, etc.) is to wrap heat insulation materials on the outer surface of the tank inner liner, and form a heat insulation layer by vacuuming the vacuum interlayer containing multi-layer heat insulation materials. The vacuum interlayer The thinner the tank, the more transport medium is loaded on the tank; but the thinner the insulation layer, the more difficult it is to arrange the supporting structure connecting the inner tank and the outer shell, the thinner the thermal insulation layer, the lower the high vacuum, and the more heat transfer between the inner tank and the outer shell. The greater the heat loss of low-temperature liquefied gas, the current multi-layer insulation technology, such as ZL00249960.6 and ZL01272605.2, considering the arrangement of radial supports in the vacuum layer, the thickness of the vacuum layer between the outer shell and the inner tank has to be 100 mm or so. The inner support structure of the inner tank and the outer shell must not only be able to withstand the force generated by the liquid load, the weight of the storage tank and the corresponding impact acceleration, but also reduce the heat leakage caused by the inner support structure as much as possible, so the inner support structure is a cryogenic storage tank. key to design. Among the existing technologies, the upper and inner support structures of low-temperature storage tanks currently used at home and abroad include: 1) The heat-insulating pad structure between the inner tank and the outer shell, but it cannot effectively solve the problem of large heat leakage from the support due to the small distance between high-vacuum multi-layer heat insulation 2) The stainless steel casing structure between the inner and outer heads is difficult to manufacture, the distance between the inner and outer heads is large, and the impact resistance is poor. And the heat leakage is relatively large; 3) The structure of the suspension belt cannot effectively solve the problem of the decline in the impact resistance caused by thermal expansion and contraction; 4) The strong impact support structure of the low-temperature container of the utility model ZL00216678.X requires a large distance between the heads and When the normal temperature turns to low temperature, the contact gap increases and the impact resistance level decreases.
随着我国低温液化气体罐式储运的发展,在限定的尺寸范围内如何有效地增大低温液化气体的储存容积及提高隔热与抗冲击水平,是设计者们所追求的目标。本发明克服了现有的支承设计存在的不足,其特点是隔热层薄、隔热性能优越及储液体积大。With the development of storage and transportation of low-temperature liquefied gas tanks in my country, how to effectively increase the storage volume of low-temperature liquefied gas and improve the level of heat insulation and impact resistance within a limited size range is the goal pursued by designers. The invention overcomes the shortcomings of the existing support design, and is characterized by thin heat insulation layer, superior heat insulation performance and large liquid storage volume.
发明内容Contents of the invention
因此,本发明的目的在于提供一种高真空绝热低温液化气体储罐,其中在罐体端部的外壳封头和内胆封头之间采用了能够同时承受径向力和轴向力的组合支承结构,组合支承结构由适当的玻璃钢或类似材料加工而成,本发明提供的高真空绝热低温液化气体储罐基本上克服了因现有技术的局限和缺点而导致的一个或多个问题。Therefore, the object of the present invention is to provide a high-vacuum heat-insulated low-temperature liquefied gas storage tank, wherein a combination of radial force and axial force is adopted between the outer shell head and the inner liner head at the end of the tank body. The supporting structure, the combined supporting structure is processed by appropriate glass fiber reinforced plastic or similar materials, and the high-vacuum heat-insulated cryogenic liquefied gas storage tank provided by the present invention basically overcomes one or more problems caused by the limitations and shortcomings of the prior art.
本发明的其它优点、目的和特征将在下面的说明中给出,对于熟悉本领域的技术人员来说,其中的一部分优点、目的和特征可以通过以下的分析明显得出或是通过本发明的实践而得到。通过在文字说明部分、权利要求书以及附图中特别指出的结构,可以实现和获得本发明的目的和其它优点。Other advantages, purposes and characteristics of the present invention will be provided in the following description, for those skilled in the art, a part of advantages, purposes and characteristics can be clearly obtained through the following analysis or obtained through the present invention. obtained by practice. The objectives and other advantages of the invention will be realized and attained by the structure particularly pointed out in the written description, claims hereof as well as the appended drawings.
为了获得到这些优点和其它优点并根据本发明的目的,作为具体的和广义的描述为实现发明的目的,本发明所述的高真空绝热储罐包括:框架和罐体,所述罐体由外壳、内胆、外壳和内胆之间的高真空绝热层以及连接外壳与内胆的支承结构所组成,所述的外壳和内胆包括直筒段和封头,其中所述的支承结构为设置在罐体端部的外壳封头和内胆封头之间的承受径向力和轴向力的组合支承结构。In order to obtain these advantages and other advantages and according to the purpose of the present invention, as a specific and broad description to achieve the purpose of the invention, the high vacuum thermal insulation storage tank described in the present invention includes: a frame and a tank body, and the tank body is composed of It consists of an outer shell, an inner tank, a high-vacuum insulation layer between the outer shell and the inner tank, and a supporting structure connecting the outer shell and the inner tank. The outer shell and the inner tank include a straight section and a head, wherein the supporting structure is set A combined support structure that bears radial force and axial force between the outer shell head and the inner liner head at the end of the tank.
本发明所述的储罐包括框架和罐体。对于罐车来讲,框架指通过某种方式和罐体固定的汽车底盘;对于罐箱来讲,框架指通过某种方式固定在限定尺寸范围内的集装箱结构框架。The storage tank of the present invention includes a frame and a tank body. For tank trucks, the frame refers to the vehicle chassis that is fixed to the tank body in some way; for tank containers, the frame refers to the container structure frame that is fixed in a certain way within a limited size range.
在本发明所述的储罐中,由于其中采用的组合支承结构仅设置在罐体两端的内外封头之间,与实用新型ZL00249960.6和ZL01272605.2所涉及的罐体相比,省缺了径向支承,从而减少了内胆和外壳的连接面传热面积,从而获得更好的隔热效果,同时由于省缺了在直筒段的径向支承,在外壳和内胆的高真空绝热层可以减薄至50毫米,扩大了内胆有效容积,提高了装载效率。In the storage tank according to the present invention, since the combined supporting structure adopted therein is only arranged between the inner and outer heads at both ends of the tank body, compared with the tank bodies involved in utility models ZL00249960.6 and ZL01272605.2, the Radial support is added, thereby reducing the heat transfer area of the connecting surface between the inner tank and the outer shell, so as to obtain better heat insulation effect. The thickness of the layer can be reduced to 50 mm, which expands the effective volume of the inner tank and improves the loading efficiency.
根据本发明所述的储罐,其中所述的内胆封头呈中心内凹状形成反置小封头,所述小封头的弧面与所述外壳的封头弧面反向。According to the storage tank according to the present invention, the head of the liner is concave in the center to form a reversed small head, and the arc surface of the small head is opposite to the arc surface of the outer shell.
本发明所述的储罐的罐体外壳包括左外封头体、外直筒体、右外封头体及加强圈,与现有技术不同的是,外壳加强圈设在外壳外部,这样使在获得相同外壳内径、相同加强圈规格的情况下,外壳使用材料少,自重小、成本低、加强圈还起到保护外壳作用;内胆由左内封头体、内直筒体、右内封头体组成(根据附图2示明罐体左右),内胆封头和外壳封头反方向安装,内胆缠绕了多层绝热材料,内胆和外壳通过两端内外封头体间的组合支承结构来连接,并承受径向力和轴向力。由于内胆封头和外壳封头反方向安装,组合支承结构可以安置在内封头内,从而使内、外封头之间的间隙更窄,使在外壳等大的情况下,内胆的有效装载容积更大,这是实用新型ZL00216678.X、ZL00249960.6和ZL01272605.2所涉及的罐体都不具备的。The tank body shell of the storage tank according to the present invention includes a left outer head body, an outer straight cylinder body, a right outer head body and a reinforcement ring. Different from the prior art, the shell reinforcement ring is arranged outside the shell, so that In the case of the same inner diameter of the shell and the same specifications of the reinforcing ring, the shell uses less material, has a small weight, low cost, and the reinforcing ring also plays a role in protecting the shell; the inner tank is composed of a left inner head body, an inner straight cylinder body, and a right inner head Body composition (according to Figure 2 shows the left and right sides of the tank body), the head of the inner tank and the head of the outer shell are installed in opposite directions, the inner tank is wound with multiple layers of heat insulating materials, and the inner tank and the outer shell are supported by the combination of the inner and outer heads at both ends Structure to connect, and bear radial force and axial force. Since the head of the inner tank and the head of the outer shell are installed in opposite directions, the combined support structure can be placed in the inner head, so that the gap between the inner and outer heads is narrower, so that when the outer shell is equal in size, the inner tank The effective loading volume is larger, which is not available in the tank bodies involved in the utility models ZL00216678.X, ZL00249960.6 and ZL01272605.2.
根据本发明所述的储罐,其中所述的支承结构设置有一支承盘,其与所述的反置小封头相接触;另外还设有两个固定环,用于保持所述的支承盘,所述的固定环分布在所述支承盘的两侧,所述的支承盘与反置小封头之间设有可自动调节的接触间隙。According to the storage tank of the present invention, wherein the support structure is provided with a support plate, which is in contact with the reversed small head; in addition, two fixing rings are provided for holding the support plate , the fixed rings are distributed on both sides of the support plate, and an automatically adjustable contact gap is set between the support plate and the reversed small head.
根据本发明所述的储罐,其中还包括一设置在外壳封头和内胆封头之间并穿过所述支承盘的中心孔的轴向支承装置,所述的轴向支承装置包括:According to the storage tank according to the present invention, it also includes an axial support device arranged between the shell head and the liner head and passing through the central hole of the support plate, and the axial support device includes:
一支承管,与所述的外壳封头内侧相固定,支承管内壁设置有一突起部;A support tube, fixed to the inner side of the shell head, and a protrusion is provided on the inner wall of the support tube;
一支承轴,与所述的反置小封头相固定,穿过所述的突起部伸入所述的支承管中;A support shaft, fixed to the reversed small head, extends into the support tube through the protrusion;
一锁紧件,设置在所述支承轴的端部;其可以是一锁紧螺帽或类似的部件,以及第一垫块,其锁定在所述锁紧件与突起部之间和第二垫块,其锁定在所述反置小封头与该支承管的突起部之间,所述支承结构中用于传递轴向载荷的支承端的内胆封头与外壳封头的间距取决于输排液体与气体的管子液封及热胀冷缩补偿所需的间距,例如,该间距可以为约300毫米。另外,为了提高支承管的支承强度还可以使所述支承管的端部为一具有加强结构的端部。a locking member disposed at the end of the support shaft; it may be a lock nut or similar, and a first spacer locked between the locking member and the protrusion and a second spacer, which is locked between the inverted small head and the protrusion of the support tube, and the distance between the inner tank head and the outer shell head of the support end used to transmit axial load in the support structure depends on the transmission The distance required for liquid sealing and thermal expansion and contraction compensation of pipes for discharging liquid and gas, for example, the distance may be about 300 mm. In addition, in order to improve the supporting strength of the supporting tube, the end of the supporting tube can also be an end with a reinforced structure.
根据本发明所述的储罐,其中还包括一固定在外壳封头内的加强筒,所述的加强筒设置在支承管的外部,在所述加强筒和支承管之间还可以设置有一加强板。为了便于内胆的安装,在内胆的一个反置小封头上设置有与所述支承管相配合的水平工艺管,在所述外壳和内胆封头内还设置有加强板。According to the storage tank according to the present invention, it also includes a reinforcing tube fixed in the head of the shell, the reinforcing tube is arranged outside the supporting tube, and a reinforcing tube may be arranged between the reinforcing tube and the supporting tube. plate. In order to facilitate the installation of the inner tank, a horizontal process pipe matched with the support tube is arranged on a small inverted head of the inner tank, and a reinforcing plate is also arranged in the outer shell and the inner tank head.
组合支承结构主要包括左径向支承盘、右径向支承盘、右轴向垫块(上文中所称的第二垫块)、左轴向垫块(上文中所称的第一垫块)和支承管。左径向支承盘设置在罐体左端,右径向支承盘设置在罐体右端,共同承担着内胆及其装载介质所产生的径向力;右轴向垫块和左轴向垫块均设置在罐体左端,使罐体在移动过程中,内胆及装载介质产生的向右及向左的轴向载荷,压迫右轴向垫块和左轴向垫块后,通过支承管,传递给外壳。通过采用有限元结构与热分析软件,受控地设计出最大装载率下能满足受力和漏热量要求的内支承结构,带轴向支承端的封头间隙只要满足管子引出时结构需要,真正实现了与高真空多层绝热结构相匹配的内支承结构。组合支承结构中的左径向支承盘和右径向支承盘的外圈与内封头体向内筒体延伸的不锈钢管相接触,有利于轴向支承块的布置与降低轴向支承块的漏热量,玻璃钢盘的内圈与外封头体上钢管相接触,使任何径向受力水平一致,提高了该结构受力的可靠性,而隔热特性很好,内胆和外壳的径向传热面仅为内支承受力面,其余的圆柱面上是辐射传热,完全避免了实用新型ZL00249960.6和ZL01272605.2所涉及的罐体径向支承的漏热量内外封头间的间距小,提高装载率。选择合适的玻璃钢支承盘材料,通过有限元分析及试验验证,使内外圈接触间隙具有自调节能力、罐体从常温变到低温时,该径向支承盘内外圈接触间隙变化很小,大大提高了径向的抗冲击能力,并利于常温下的装配及间隙控制。同时,该发明充分利用了该玻璃钢材料抗压强度与导热系数的比值大与接触热阻的特性,使支承耐径向力的能力大,而漏热又小,解决了实用新型ZL00216678.X的低温容器抗强冲击支承结构中冷态接触间隙变大不利于抗冲击的难题。通过内封头体向内筒体延伸的不锈钢管来加长轴向玻璃钢压块的长度,降低轴向支承的漏热,解决了实用新型ZL00216678.X的低温容器抗强冲击支承结构中轴向支承漏热量无法控制的问题,同时确保有效空间内的最大储液体积,圆满地解决了内支承受力与隔热的矛盾。The combined support structure mainly includes the left radial support plate, the right radial support plate, the right axial pad (the second pad referred to above), and the left axial pad (the first pad referred to above) and support tube. The left radial support plate is set at the left end of the tank body, and the right radial support plate is set at the right end of the tank body, jointly bearing the radial force generated by the inner tank and its loading medium; the right axial pad and the left axial pad are both It is installed at the left end of the tank body so that during the moving process of the tank body, the right and left axial loads generated by the inner tank and the loading medium, after pressing the right axial pad and the left axial pad, are transmitted through the support tube. Give the crust. Through the use of finite element structure and thermal analysis software, the inner support structure that can meet the requirements of force and heat leakage under the maximum loading rate is controlled and designed. As long as the clearance of the head with the axial support end meets the structural requirements when the pipe is drawn out, it can be truly realized. The internal support structure matching the high vacuum multilayer insulation structure has been established. The outer rings of the left radial support plate and the right radial support plate in the combined support structure are in contact with the stainless steel tube extending from the inner head body to the inner cylinder, which is beneficial to the arrangement of the axial support block and reduces the weight of the axial support block. Heat leakage, the inner ring of the FRP disk is in contact with the steel pipe on the outer head body, so that any radial force level is consistent, which improves the reliability of the structure, and the heat insulation performance is very good. The diameter of the inner tank and the outer shell The heat transfer surface is only the inner support force surface, and the rest of the cylindrical surface is radiation heat transfer, which completely avoids the heat leakage of the radial support of the tank involved in the utility models ZL00249960.6 and ZL01272605.2. The small spacing increases the loading rate. Select the appropriate material of the FRP support disc, and through finite element analysis and test verification, the contact gap between the inner and outer rings has self-adjustment ability. When the tank body changes from normal temperature to low temperature, the contact gap between the inner and outer rings of the radial support disc changes very little, greatly improving Improve the radial impact resistance, and facilitate the assembly and clearance control at room temperature. At the same time, this invention makes full use of the characteristics of the high ratio of compressive strength to thermal conductivity and the thermal contact resistance of the FRP material, so that the support has a large ability to withstand radial force and small heat leakage, which solves the problem of the utility model ZL00216678.X The large contact gap in the cold state is not conducive to the impact resistance problem in the strong impact support structure of the cryogenic vessel. Extend the length of the axial FRP briquetting block through the stainless steel tube extending from the inner head body to the inner cylinder, reduce the heat leakage of the axial support, and solve the axial support in the anti-strong impact support structure of the low-temperature vessel of the utility model ZL00216678.X The problem of uncontrollable heat leakage, while ensuring the maximum liquid storage volume in the effective space, satisfactorily solves the contradiction between internal support force and heat insulation.
附图说明Description of drawings
图1是本发明高真空多层绝热低温液化气体储罐示意图;Fig. 1 is a schematic diagram of a high-vacuum multi-layer heat-insulated low-temperature liquefied gas storage tank of the present invention;
图2是罐体及内支承结构示意图。Fig. 2 is a schematic diagram of the tank body and the inner support structure.
图1中,37是框架、38是罐体;图2中1是外壳左封头、2是外壳左封头加强板、3是内胆左封头、4是内胆左封头加强板、5是左过渡接筒、6是左补强板、7是左加强筒、8是左加强板、9是左玻璃钢支承管、10是左封板、11是支承轴,其可以是不锈钢轴、12是锁紧件,其可以是螺帽、13是左反置小封头、14是左径向支承盘、15是第二垫块、16第一垫块、17是左径向支承盘左固定环、18是左径向支承盘右固定环、19是右径向支承盘、20是右反置小封头、21是工艺管、22是右径向支承盘右固定环、23是右径向支承盘左固定环、24是外壳右封头、25是外壳右封头加强板、26是内胆右封头、27是内胆右封头加强板、28是右过渡接筒、29是右补强板、30是右加强筒、31是右加强板、32是右支承管、33是右封板、34是内直筒体、35是外直筒体、36是外壳加强圈、39是高真空绝热层、40是多层缠绕绝热材料。In Figure 1, 37 is the frame, 38 is the tank body; in Figure 2, 1 is the left head of the shell, 2 is the reinforcement plate of the left head of the shell, 3 is the left head of the liner, 4 is the reinforcement plate of the left head of the liner, 5 is the left transition tube, 6 is the left reinforcing plate, 7 is the left reinforcing tube, 8 is the left reinforcing plate, 9 is the left fiberglass support tube, 10 is the left sealing plate, 11 is the supporting shaft, which can be a stainless steel shaft, 12 is a locking piece, which can be a nut, 13 is a left reversed small head, 14 is a left radial support plate, 15 is a second spacer, 16 is a first spacer, 17 is a left radial support plate left Fixed ring, 18 is the right fixed ring of the left radial support plate, 19 is the right radial support plate, 20 is the right reversed small head, 21 is the process tube, 22 is the right fixed ring of the right radial support plate, 23 is the right The left fixed ring of the radial support plate, 24 is the right head of the shell, 25 is the reinforcement plate of the right head of the shell, 26 is the right head of the inner tank, 27 is the reinforcement plate of the right head of the inner tank, 28 is the right transition tube, 29 is the right reinforcing plate, 30 is the right reinforcing tube, 31 is the right reinforcing plate, 32 is the right support pipe, 33 is the right sealing plate, 34 is the inner straight cylinder, 35 is the outer straight cylinder, 36 is the shell reinforcement ring, 39 is The high vacuum insulation layer, 40, is a multilayer winding insulation material.
具体实施方式:Detailed ways:
下面结合附图对本发明的具体实施作进一步描述。如图1所示,本发明包括框架37和罐体38,两者按照适当方式焊接在一起。如图2所示,罐体包括外壳左封头1、外壳左封头加强板2、内胆左封头3、内胆左封头加强板4、左过渡接筒5、左补强板6、左加强筒7、左加强板8、左支承管9、左封板10、不锈钢轴11、锁紧螺帽12、左反置小封头13、左径向支承盘14、第二垫块15、第一垫块16、左径向支承盘左固定环17、左径向支承盘右固定环18、右径向支承盘19、右反置小封头20、工艺管21、右径向支承盘右固定环22、右径向支承盘左固定环23、外壳右封头24、外壳右封头加强板25、内胆右封头26、内胆右封头加强板27、右过渡接筒28、右补强板29、右加强筒30、右加强板31、右支承管32、右封板33、内直筒体34、外直筒体35、外壳加强圈36、高真空绝热层39和多层缠绕绝热材料40。The specific implementation of the present invention will be further described below in conjunction with the accompanying drawings. As shown in Figure 1, the present invention comprises a frame 37 and a tank body 38 welded together in an appropriate manner. As shown in Figure 2, the tank body includes the left shell head 1, the left shell head reinforcement plate 2, the inner tank left head head 3, the inner tank left head reinforcement plate 4, the left transition tube 5, and the left reinforcement plate 6 , left reinforcing tube 7, left reinforcing plate 8, left supporting tube 9, left sealing plate 10, stainless steel shaft 11, lock nut 12, left reversed small head 13, left radial supporting plate 14, second spacer 15. The first spacer 16, the left radial support plate left fixed ring 17, the left radial support plate right fixed ring 18, the right radial support plate 19, the right reversed small head 20, the process tube 21, the right radial Support plate right fixed ring 22, right radial support plate left fixed ring 23, shell right head 24, shell right head reinforcement plate 25, inner tank right head 26, inner tank right head reinforcement plate 27, right transition joint Tube 28, right reinforcing plate 29, right reinforcing tube 30, right reinforcing plate 31, right support pipe 32, right sealing plate 33, inner straight cylinder 34, outer straight cylinder 35, shell reinforcement ring 36, high vacuum insulation layer 39 and Multiple layers of wrapping insulation material 40 .
外壳左封头1、外壳左封头加强板2、左补强板6、左加强筒7、左加强板8和左支承管9相互焊接在一起形成左外封头体。The left shell head 1, the left shell head reinforcement plate 2, the left reinforcement plate 6, the left reinforcement tube 7, the left reinforcement plate 8 and the left support pipe 9 are welded together to form the left outer head body.
内胆左封头3、左过渡接筒5、内胆左封头加强板4、左反置小封头13、左径向支承盘右固定环18和不锈钢轴11相互焊接在一起形成左内封头体。The left inner tank head 3, the left transition tube 5, the left inner tank head reinforcing plate 4, the left reversed small head 13, the left radial support plate right fixing ring 18 and the stainless steel shaft 11 are welded together to form a left inner Head body.
外壳右封头24、外壳右封头加强板25、右补强板29、右加强筒30、右加强板31和右支承管32相互焊接在一起形成右外封头体。The right shell head 24, the right shell reinforcement plate 25, the right reinforcement plate 29, the right reinforcement tube 30, the right reinforcement plate 31 and the right support pipe 32 are welded together to form the right outer head body.
内胆右封头26、右过渡接筒28、右反置小封头20、水平安装工艺管21、右径向支承盘左固定环23和内胆右封头加强板27相互焊接在一起形成右内封头体。The right head 26 of the inner tank, the right transition tube 28, the right reversed small head 20, the horizontal installation process pipe 21, the left fixed ring 23 of the right radial support plate and the right head reinforcement plate 27 of the inner tank are welded together to form Right inner head body.
右外封头体24和外直筒段35焊接而成外筒体组合段。左内封头体、右内封头体和内直筒段34相互焊接在一起形成内胆。内胆外表面缠绕多层绝热材料40。在安装过程中,首先,把右径向支承盘19放入内胆内,再放入右径向支承盘右固定环22,用专用工装压紧右径向支承盘右固定环22的内圈,右径向支承盘右固定环22与内胆上右过渡接筒28角焊接,外筒体组合段套入右径向支承盘19内。其次,把左径向支承盘14放入内胆内,再放入左径向支承盘左固定环17,用专用工装压紧左径向支承盘左固定环17的内圈,左径向支承盘左固定环17与内胆上左过渡接筒5角焊接,把第二垫块15放入内胆不锈钢支承轴11上,最后把左外封头体套入左径向支承盘14内,左外封头体上左封头1与外筒体组合段焊接。第一垫块16放入左支承管9内,用锁紧螺帽12旋紧到内胆不锈钢支承轴11上来压紧第一垫块16与第二垫块15,锁紧螺帽12与不锈钢支承轴11角焊接实现组合支承的安装。最后,左封板10与左补强板6角焊接与右补强板29与右封板33角焊接,形成罐体。外壳和内胆之间抽高真空形成高真空绝热层39。外壳加强圈36焊在外壳外表面。The right outer head body 24 and the outer straight section 35 are welded to form an outer cylinder combined section. The left inner head body, the right inner head body and the inner straight section 34 are welded together to form an inner container. The outer surface of the liner is wrapped with multiple layers of heat insulating material 40 . In the installation process, firstly, put the right radial support plate 19 into the inner tank, then put the right radial support plate right fixed ring 22, and press the inner ring of the right radial support plate right fixed ring 22 with special tooling , the right fixed ring 22 of the right radial support plate is welded with the upper right transition tube 28 of the inner tank, and the combined section of the outer cylinder is inserted into the right radial support plate 19. Next, put the left radial support plate 14 into the inner tank, then put the left radial support plate left fixed ring 17, press the inner ring of the left radial support plate left fixed ring 17 with special tooling, and the left radial support The left fixed ring 17 is welded to the 5 corners of the upper left transition tube of the inner tank, the second spacer 15 is placed on the stainless steel support shaft 11 of the inner tank, and finally the left outer head body is inserted into the left radial support disc 14, The left head 1 on the left outer head body is welded to the combined section of the outer cylinder body. The first spacer 16 is put into the left support pipe 9, and is screwed onto the inner tank stainless steel supporting shaft 11 with the lock nut 12 to compress the first spacer 16 and the second spacer 15, the lock nut 12 and the stainless steel Support shaft 11 fillet welding realizes the installation of combined support. Finally, the corner welding of the left sealing plate 10 and the left reinforcing plate 6 and the corner welding of the right reinforcing plate 29 and the right sealing plate 33 form the tank body. A high vacuum is drawn between the shell and the inner bag to form a high vacuum insulation layer 39 . Shell reinforcing ring 36 is welded on the outer surface of the shell.
当然,可以理解的是,本领域熟知的技术人员在本发明技术方案的基础上可以做出任何更改或变形,而它们均应属于本发明所附权利要求的范围。Of course, it can be understood that those skilled in the art can make any changes or deformations on the basis of the technical solution of the present invention, and they all should belong to the scope of the appended claims of the present invention.
Claims (12)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100090131A CN1333198C (en) | 2004-04-15 | 2004-04-15 | High vacuum heat insulation low temperature liquefied gas storage tank |
| PCT/CN2005/000447 WO2005100210A1 (en) | 2004-04-15 | 2005-04-05 | Super-vacuum insulation tank for cryogenic liquefied gas |
| DE112005000873T DE112005000873T5 (en) | 2004-04-15 | 2005-04-05 | Vacuum super-insulated tank for cryogenic liquefied gas |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100090131A CN1333198C (en) | 2004-04-15 | 2004-04-15 | High vacuum heat insulation low temperature liquefied gas storage tank |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1683816A CN1683816A (en) | 2005-10-19 |
| CN1333198C true CN1333198C (en) | 2007-08-22 |
Family
ID=35149889
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2004100090131A Expired - Lifetime CN1333198C (en) | 2004-04-15 | 2004-04-15 | High vacuum heat insulation low temperature liquefied gas storage tank |
Country Status (3)
| Country | Link |
|---|---|
| CN (1) | CN1333198C (en) |
| DE (1) | DE112005000873T5 (en) |
| WO (1) | WO2005100210A1 (en) |
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| CN2451917Y (en) * | 2000-11-07 | 2001-10-03 | 上海交通大学 | Liquefied natural gas transport storing tank |
| CN2515507Y (en) * | 2001-11-29 | 2002-10-09 | 张家港市圣达因化工机械有限公司 | Vehicular liquefied natural gas cylinder |
| CN2528733Y (en) * | 2001-11-29 | 2003-01-01 | 张家港市圣达因化工机械有限公司 | Thermal insulating tank-type container |
| CN2695767Y (en) * | 2004-04-15 | 2005-04-27 | 中国国际海运集装箱(集团)股份有限公司 | High vacuum adiabatic low temp liquified gas storage tank |
| CN2702155Y (en) * | 2004-04-15 | 2005-05-25 | 中国国际海运集装箱(集团)股份有限公司 | High vacuum heat insulation low-temperature liquefied gas storage tank |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN102190133A (en) * | 2011-03-23 | 2011-09-21 | 李彩琴 | Container type oiling device |
| CN105090743A (en) * | 2015-07-08 | 2015-11-25 | 武汉武船重型装备工程有限责任公司 | Supporting pipe seat for lower supporting structure of low-temperature storing tank for ship |
| TWI871560B (en) * | 2021-12-27 | 2025-02-01 | 日商川崎重工業股份有限公司 | Triple Shell Tank |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2005100210A1 (en) | 2005-10-27 |
| CN1683816A (en) | 2005-10-19 |
| DE112005000873T5 (en) | 2007-03-08 |
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