SE466275B - CONTAINER, SPECIFICALLY FOR A PRESSURE FLUID - Google Patents
CONTAINER, SPECIFICALLY FOR A PRESSURE FLUIDInfo
- Publication number
- SE466275B SE466275B SE9001841A SE9001841A SE466275B SE 466275 B SE466275 B SE 466275B SE 9001841 A SE9001841 A SE 9001841A SE 9001841 A SE9001841 A SE 9001841A SE 466275 B SE466275 B SE 466275B
- Authority
- SE
- Sweden
- Prior art keywords
- adhesive
- joint
- end portion
- container
- halves
- Prior art date
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/58—Snap connection
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5042—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like covering both elements to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/128—Stepped joint cross-sections
- B29C66/1284—Stepped joint cross-sections comprising at least one butt joint-segment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/128—Stepped joint cross-sections
- B29C66/1286—Stepped joint cross-sections comprising at least one bevelled joint-segment
- B29C66/12861—Stepped joint cross-sections comprising at least one bevelled joint-segment comprising at least two bevelled joint-segments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
- B29C66/72141—Fibres of continuous length
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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
- B65D11/00—Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of plastics material
- B65D11/02—Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of plastics material of curved cross-section
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L47/00—Connecting arrangements or other fittings specially adapted to be made of plastics or to be used with pipes made of plastics
- F16L47/02—Welded joints; Adhesive joints
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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
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/16—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
- B29C65/4845—Radiation curing adhesives, e.g. UV light curing adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
- B29C65/5014—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being fibre-reinforced
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/712—Containers; Packaging elements or accessories, Packages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/712—Containers; Packaging elements or accessories, Packages
- B29L2031/7154—Barrels, drums, tuns, vats
- B29L2031/7156—Pressure vessels
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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
- F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
-
- 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
- F17C2209/227—Assembling processes by adhesive 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
- 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
- F17C2221/031—Air
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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
- F17C2223/0107—Single phase
- F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
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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
- F17C2223/035—High pressure (>10 bar)
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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
- F17C2270/05—Applications for industrial use
- F17C2270/0563—Pneumatic applications
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
Description
15 20 25 30 35 466 275 2 man åtminstone på den ena av de för hoplimning avsedda limytor- na har kvar ett relativt tjockt limskikt som ger erforderlig styrka och täthet i limfogen. At least one of the adhesive surfaces intended for gluing together has a relatively thick adhesive layer which gives the required strength and tightness in the adhesive joint.
Detta uppnås med en behållare av det slag som anges i ingressen till patentkravet 1 och som enligt uppfinningen har de i den kännetecknande delen av patentkravet 1 angivna kännetecknen.This is achieved with a container of the type stated in the preamble of claim 1 and which according to the invention has the features stated in the characterizing part of claim 1.
Genom att utföra skarven enligt uppfinningen uppnås att de påförda limskikten på behållarehalvornas ändpartier vid hop- skjutningen av de båda ändpartierna endast i begränsad ut- sträckning eller väsentligen inte alls påverkas, vilket medför att limskiktet med tillräckligt mycket lim föres ihop och bildar en limfog med önskad styrka och täthet. Dessutom är behållarehalvornas ändpartier utformade med så samverkande koniska ytor att man erhåller ett grepp som motverkar axiell isärdragning av de båda halvorna. För att bibehålla detta grepp är en förstärkningsmuff anordnad kring skarven i form av pålin- dad armeringstråd i kombination med en plast. Med hjälp av denna muff låses ändpartierna i sitt grepp med varandra så att limmet i limfogarna ej kan utsättas för krafter som skulle kunna bryta upp limfogarna.By performing the joint according to the invention it is achieved that the applied adhesive layers on the end portions of the container halves when the two end portions are pushed together only to a limited extent or substantially not at all, which means that the adhesive layer with sufficient adhesive is brought together and forms an adhesive joint with desired strength and density. In addition, the end portions of the container halves are designed with such cooperating conical surfaces that a grip is obtained which counteracts axial contraction of the two halves. To maintain this grip, a reinforcing sleeve is arranged around the joint in the form of wound reinforcement wire in combination with a plastic. With the aid of this sleeve, the end portions are locked in their grip with each other so that the glue in the glue joints cannot be exposed to forces that could break up the glue joints.
Några lämpliga utföringsformer av behållaren enligt uppfin- ningen visas som exempel på bifogade ritningar.Some suitable embodiments of the container according to the invention are shown as examples of the accompanying drawings.
Fig 1 är en sidovy av behållaren som består av två hoplimmade cylindriska halvor utförda i ett stycke med var sin ändgavel.Fig. 1 is a side view of the container consisting of two glued-together cylindrical halves made in one piece with each end end.
Fig 2 visar i förstorad skala ett snitt enligt linjen 2-2 i fig 1.Fig. 2 shows on an enlarged scale a section along the line 2-2 in Fig. 1.
Fig 3 är en detaljbild av den i skarven yttre cylinderhalvans ändparti i sektion sådant det ingår i fig 2.Fig. 3 is a detail view of the end portion of the outer half of the cylinder in the joint in section such as is included in Fig. 2.
Fig 4 är en detaljbild av det i skarven ingående inre ändpar- tiet i sektion sådant det ingår i fig 2. 10 15 20 25 30 35 466 275" 3 Fig 5 visar ett första mellanläge under inskjutningen av det yttre ändpartiet på det inre ändpartiet efter det att de båda ändpartiernas limytor har försetts med limskikt.Fig. 4 is a detail view of the inner end portion included in the joint in section as it is included in Fig. 2. Fig. 5 shows a first intermediate position during the insertion of the outer end portion on the inner end portion after the fact that the adhesive surfaces of the two end portions have been provided with adhesive layers.
Fig 6 visar ett andra mellanläge efter fortsatt inskjutning från läget i fig 5.Fig. 6 shows a second intermediate position after continued insertion from the position in Fig. 5.
Fig 7 visar ett tredje mellanläge efter fortsatt inskjutning till ett läge som ligger strax före slutläget enligt fig 2.Fig. 7 shows a third intermediate position after continued insertion to a position which is just before the final position according to Fig. 2.
Fig 8 visar en annan utföringsform av skarven vid behållaren enligt uppfinningen i ett limmat slutläge.Fig. 8 shows another embodiment of the joint at the container according to the invention in a glued end position.
Fig 9 visar ett mellanläge före slutläget i fig 8.Fig. 9 shows an intermediate position before the final position in Fig. 8.
Behållaren i fig 1 är sammansatt av två cylindriska halvor 10, 12 som var och en är utförd i ett stycke med en ändgavel 14 respektive 16.The container in Fig. 1 is composed of two cylindrical halves 10, 12 which are each made in one piece with an end end 14 and 16, respectively.
I skarven 18 mellan de båda halvorna är den ena halvans änd- parti 20 inskjutet över den andra halvans ändparti 22 så att det utanpåliggande ändpartiets 20 invändiga limytor anligger noga mot det innanförliggande ändpartiets 22 utvändiga limytor för att åstadkoma en så effektiv hoplimning av dessa till en limfog som säkert tätas mot förekomande stora gastryck i behållaren, i storleksordningen 5-100 bar. Limfogen kan även uppta väsentliga dragkrafter.In the joint 18 between the two halves, the end portion 20 of one half is slid over the end portion 22 of the other half so that the inner adhesive surfaces of the outer end portion 20 abut closely against the outer adhesive surfaces of the inner end portion 22 to effect such effective gluing together into a adhesive joints that are securely sealed against any large gas pressures in the container, in the order of 5-100 bar. The adhesive joint can also absorb significant tensile forces.
Halvorna 10 och 12 är tillverkade enligt den kända metod, där man först bygger upp ett skikt av längsgående och tvärgående glasfibertrådar på en kärna med hjälp av en robot och därefter anbringar glasfibertrådkroppen i ett yttre formverktyg. Slut- ligen injiceras plast i verktyget för att erhålla en glasfiber- armerad halva som kan uppta förekomande relativt stora axiella och radiella krafter. Plasten är vanligen en polyester som får härda innan verktyget öppnas.The halves 10 and 12 are made according to the known method, where a layer of longitudinal and transverse fiberglass wires is first built up on a core by means of a robot and then the fiberglass wire body is placed in an external molding tool. Finally, plastic is injected into the tool to obtain a fiberglass-reinforced half that can absorb relatively large axial and radial forces. The plastic is usually a polyester that is allowed to harden before the tool is opened.
Det yttre ändpartiet 20 skall relativt lätt kunna spännas ut till en större diameter, såsom beskrives nedan. Det tillverkas 10 15 20 25 30 35 466 275 4 därför med ett avsevärt mindre antal lindningsvarv av glas- fibertrâd än för halvan 10 i övrigt, eller helt utan lindnings- varv och endast med axiella glasfibertrådar som sträcker sig ut till i närheten av ändpartiets kant. Ändpartiets 20 invändiga limyta är sammansatt av två invändiga stympade koner 24, 26, och ändpartiet 22 har en limyta samman- satt av två utvändiga stympade koner 28, 30 som noga passar mot konerna 24, 26. Konernas breda basändar är vända mot varandra och har vid övergångsställena 32 respektive 33 sin största diameter. I det monterade läget sammanfaller övergângsställena 32, 33. Övergången 32 är lämpligen mjukt avrundad. Ändpartiet 20 har dessutom en ändyta 34 som är hoplimmad med en ändyta 36 hos ändpartiet 22.The outer end portion 20 should be relatively easy to stretch to a larger diameter, as described below. It is therefore manufactured with a considerably smaller number of winding turns of fiberglass wire than for half 10 otherwise, or completely without winding turns and only with axial fiberglass wires extending to near the edge of the end portion. . The inner adhesive surface of the end portion 20 is composed of two inner truncated cones 24, 26, and the end portion 22 has an adhesive surface composed of two outer truncated cones 28, 30 which closely fit the cones 24, 26. The wide base ends of the cones are facing each other and have at the crossings 32 and 33, respectively, their largest diameter. In the mounted position, the transition points 32, 33 coincide. The transition 32 is suitably softly rounded. The end portion 20 further has an end surface 34 which is glued together with an end surface 36 of the end portion 22.
I fig 2-7 är konernas 24, 28 konvinkel 2A större än konernas 26, 30 konvinkel 2B, vilket antydes i fig 3 med att vinkeln A är ca l2° (d v s en konvinkel 24°) och vinkeln B är ca 4° (d v s en konvinkel 8°.In Figs. 2-7, the cone angle 2A of the cones 24, 28 is larger than the cone angle 2B of the cones 26, 30, which is indicated in Fig. 3 by the angle A being about 12 ° (ie a cone angle 24 °) and the angle B being about 4 ° (ie and cone angle 8 °.
Före hopskjutning av halvorna enligt fig 5-7, påföres ett limskikt på alla limytorna. Limmet kan exempelvis vara ett härdlim av epoxityp.Before joining the halves according to Figs. 5-7, an adhesive layer is applied to all the adhesive surfaces. The adhesive can, for example, be a curing adhesive of epoxy type.
På limytorna 24, 26, 34 finns sålunda limskikt 24A, 26A respek- tive 34A. På limytorna 28, 30 och 36 finns limskikt 28A, 30A respektive 36A. Ändpartiet 20 har vid sin ände en ändkant 38 som är avrundad för att ej bilda en skrapkant. Ãndpartiet 22 löper å sin sida ut i ett i sektion kilformat kantparti 40, vilket är utsatt för gastrycket i behållaren och påverkas i riktning mot limytan 24 för att upprätthålla önskad anliggning mot denna.The adhesive surfaces 24, 26, 34 thus have adhesive layers 24A, 26A and 34A, respectively. On the adhesive surfaces 28, 30 and 36 there are adhesive layers 28A, 30A and 36A, respectively. The end portion 20 has at its end an end edge 38 which is rounded so as not to form a scraping edge. The end portion 22, in turn, extends into a section wedge-shaped edge portion 40, which is subjected to the gas pressure in the container and is actuated in the direction of the adhesive surface 24 in order to maintain the desired abutment against it.
Vid hopskjutning av halvornas ändpartier komer kanten 38 att träffa limytan 28 vid ett ställe 42, varefter kanten 38 glider på limskiktet 28A under viss minskning av dess tjocklek mellan 4). 10 15 20 25 466 2754 s punkten 42 och övergången 32 mellan limytorna 28 och 30. Det sålunda erhållna tunnare limskiktet betecknas med 28C.When the end portions of the halves are pushed together, the edge 38 will hit the adhesive surface 28 at a place 42, after which the edge 38 slides on the adhesive layer 28A while reducing its thickness between 4). 466 2754 s point 42 and the transition 32 between the adhesive surfaces 28 and 30. The thinner adhesive layer thus obtained is denoted by 28C.
På limytan 28 har dessutom kvarlämnats ett opåverkat limskikt 28B. U När kanten 38 befinner sig vid övergången 32 enligt fig 6 har ändpartiet 20 utvidgats radiellt under uppböjning så att konens 26 konvinkel har minskats i detta läge. Vid fortsatt inskjut- ning kommer limskiktet 26A att av övergångspunkten 32 jämnas ut till ett tunnare limskikt 26C på limytan 26.In addition, an unaffected adhesive layer 28B has been left on the adhesive surface 28. When the edge 38 is at the transition 32 according to Fig. 6, the end portion 20 has been expanded radially during bending so that the cone angle of the cone 26 has been reduced in this position. Upon continued insertion, the adhesive layer 26A will be smoothed by the transition point 32 to a thinner adhesive layer 26C on the adhesive surface 26.
Såsom illustreras i fig 7 komer limytan 26 med sitt tunna limskikt 26C att befinna sig fritt ovanför det opåverkade limskiktet 30A tills ändpartierna är i det närmaste helt hop- skjutna och limskikten 34A och 36A på ändytorna har bringats i kontakt med varandra.As illustrated in Fig. 7, the adhesive surface 26 with its thin adhesive layer 26C will be freely above the unaffected adhesive layer 30A until the end portions are almost completely pushed together and the adhesive layers 34A and 36A on the end surfaces have been brought into contact with each other.
Vid den slutliga hoplimningen kommer sålunda det normala lims- kiktet 24A att pressas ihop med det normala limskiktet 28B och med det tunnare limskiktet 28C. På andra sidan om övergången 32 komer det tunnare limskiktet 26C att pressas ihop med det nor- mala limskiktet 30A.Thus, upon final gluing, the normal adhesive layer 24A will be compressed with the normal adhesive layer 28B and with the thinner adhesive layer 28C. On the other side of the transition 32, the thinner adhesive layer 26C will be compressed with the normal adhesive layer 30A.
I varje limfog komer limningen sålunda att ske med hjälp av ett limskikt som har normal tjocklek och ett normalt eller tunnare limskikt efter hopskjutningen av ändpartierna.In each adhesive joint, the gluing will thus take place by means of an adhesive layer which has a normal thickness and a normal or thinner adhesive layer after the joining of the end portions.
Därefter lindas en armeringstrâd såsom glasfibertråd kring skarven tillsammans med en lämpligen UV-härdande plast för åstadkomande av en stark trådarmerad förstärkningsmuff 44, vilken låser ihop ändpartierna till det i fig 2 visade slutlä- get, där den koniska limytan 26 griper över den koniska limytan 30 i ett grepp som förhindrar axiell isärdragning av halvorna 10 och 12. I kombination med muffen 44 upprätthålles sålunda detta grepp som tillsammans med limfogarna, vilka är täta och starka, medför att skarven kan dimensioneras med enkla medel för att kunna motstå förekommande axiella drag- och tryck 10 15 20 25 ED Åse 275 6 krafter samt radiella krafter. Detta förband är sålunda enkelt och billigt att åstadkoma och tar liten plats på behållarens utsida.Thereafter, a reinforcing wire such as fiberglass wire is wound around the joint together with a suitable UV-curing plastic to provide a strong wire-reinforced reinforcing sleeve 44, which locks the end portions to the end position shown in Fig. 2, where the conical adhesive surface 26 engages the conical adhesive surface 30. in a grip which prevents axial retraction of the halves 10 and 12. In combination with the sleeve 44, this grip is thus maintained which, together with the adhesive joints, which are tight and strong, means that the joint can be dimensioned by simple means to withstand existing axial tension and pressure 10 15 20 25 ED Åse 275 6 forces and radial forces. This dressing is thus simple and inexpensive to make and takes up little space on the outside of the container.
Utföringsformen i fig 8 och 9 är i princip utförd på samma sätt som skarven i fig 2, varvid motsvarande detaljer i fig 8 har fått en tilläggssiffra nr 1 så att exempelvis halvan 10 i fig 2 får beteckningen 110 i fig 8 o s v.The embodiment in Figs. 8 and 9 is in principle designed in the same way as the joint in Fig. 2, the corresponding details in Fig. 8 having been given an additional number no. 1 so that, for example, half 10 in Fig. 2 is designated 110 in Fig. 8 and so on.
De båda dubbelkoniska limytorna 124, 126 har i detta fall en vinkel A.som är ca 12° (d v s en konvinkel 24°), medan vinkeln B är ca 10° (d v s en konvinkel 20°), vilket innebär att vinkeln B är väsentligt större i fig 8 än i fig 2. Konvinkeln 2B kan ligga i området 6°-30°.The two double-conical adhesive surfaces 124, 126 in this case have an angle A. which is about 12 ° (ie a cone angle 24 °), while the angle B is about 10 ° (ie a cone angle 20 °), which means that the angle B is substantially larger in Fig. 8 than in Fig. 2. The cone angle 2B may be in the range 6 ° -30 °.
Såsom framgår av fig 9 komer den avrundade kanten 138 att glida utmed hela limytan 128 och jämna ut detta till ett tun- nare limskikt 128C.As shown in Fig. 9, the rounded edge 138 will slide along the entire adhesive surface 128 and smooth it into a thinner adhesive layer 128C.
Den avrundade övergångskanten 132 komer att jämna ut limskik- tet 126121111 ett tunnare limskikt lzsc.The rounded transition edge 132 will even out the adhesive layer 126121111 a thinner adhesive layer lzsc.
Limskikten 124A och 130A blir däremot väsentligen opåverkade under hopskjutningen av halvorna 110 och 112 tills ändpartierna uppnår slutläget i fig 8.The adhesive layers 124A and 130A, on the other hand, become substantially unaffected during the joining of the halves 110 and 112 until the end portions reach the final position in Fig. 8.
Genom att den koniska ytan 126 har en större konicitet än ytan 26 i fig 2 komer ytorna 126 och 130 att få en starkare hop- koppling och därmed ett större motstånd mot att dragas isär.Because the conical surface 126 has a larger conicity than the surface 26 in Fig. 2, the surfaces 126 and 130 will have a stronger coupling and thus a greater resistance to being pulled apart.
Den trådarmerade muffen 144 låser skarvens delar effektivt i slutläget, vilket framgår av fig 8.The wire-reinforced sleeve 144 effectively locks the parts of the joint in the end position, as shown in Fig. 8.
Eftersom muffen 44 respektive 144 måste vara helt oföränderlig vid uppträdande radiella krafter på grund av gastrycket, kan det vid behov vara lämpligt att förstärka muffens trådarmering genom att armeringstrådarna utgöres av glasfibertråd och/eller ståltråd för att öka säkerheten.Since the sleeve 44 and 144, respectively, must be completely unchanged in the event of radial forces occurring due to the gas pressure, it may be appropriate, if necessary, to reinforce the wire reinforcement of the sleeve by the reinforcing wires being made of fiberglass wire and / or steel wire to increase safety.
Claims (2)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9001841A SE466275B (en) | 1990-05-22 | 1990-05-22 | CONTAINER, SPECIFICALLY FOR A PRESSURE FLUID |
PCT/SE1991/000361 WO1991018239A1 (en) | 1990-05-22 | 1991-05-21 | A container, particularly for pressure fluid |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9001841A SE466275B (en) | 1990-05-22 | 1990-05-22 | CONTAINER, SPECIFICALLY FOR A PRESSURE FLUID |
Publications (3)
Publication Number | Publication Date |
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SE9001841D0 SE9001841D0 (en) | 1990-05-22 |
SE9001841L SE9001841L (en) | 1991-11-23 |
SE466275B true SE466275B (en) | 1992-01-20 |
Family
ID=20379559
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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SE9001841A SE466275B (en) | 1990-05-22 | 1990-05-22 | CONTAINER, SPECIFICALLY FOR A PRESSURE FLUID |
Country Status (2)
Country | Link |
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SE (1) | SE466275B (en) |
WO (1) | WO1991018239A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4286737A1 (en) * | 2022-06-01 | 2023-12-06 | Airbus Operations, S.L.U. | Composite hydrogen tank for an aircraft |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE468649B (en) * | 1991-05-24 | 1993-02-22 | Kb Komposit Foersaeljnings Ab | ARMED PLASTIC CONTAINER, SATISFIED TO ASTAD A COMBUSTION BODY FOR THIS AND APPLIANCE BEFORE IMPLEMENTING THE SET |
US5419593A (en) * | 1993-10-22 | 1995-05-30 | Conley Corporation | Interlocking union for double containment pipe |
GB9700927D0 (en) * | 1997-01-17 | 1997-03-05 | Raychem Sa Nv | Pipe coupler |
SE0600586L (en) * | 2006-03-16 | 2007-09-17 | Polytec Composites Sweden Ab | Pressure vessels |
US11353160B2 (en) * | 2014-02-27 | 2022-06-07 | Hanwha Cimarron Llc | Pressure vessel |
JP7351267B2 (en) * | 2020-07-08 | 2023-09-27 | トヨタ自動車株式会社 | High pressure tank manufacturing method |
JP7384142B2 (en) | 2020-10-09 | 2023-11-21 | トヨタ自動車株式会社 | High pressure tank manufacturing method |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL7305984A (en) * | 1973-04-27 | 1974-10-29 | ||
US4006838A (en) * | 1974-11-25 | 1977-02-08 | Western Industries, Inc. | Brazing alloy and brazing paste for gas container joints |
CA1182146A (en) * | 1980-06-25 | 1985-02-05 | Major G. Butler | Mechanical pipe joint and method of forming the same |
DE3818066A1 (en) * | 1988-05-27 | 1989-12-07 | Sigri Gmbh | ADHESIVE CONNECTION OF CARBON OR GRAPHITE TUBES |
-
1990
- 1990-05-22 SE SE9001841A patent/SE466275B/en not_active IP Right Cessation
-
1991
- 1991-05-21 WO PCT/SE1991/000361 patent/WO1991018239A1/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4286737A1 (en) * | 2022-06-01 | 2023-12-06 | Airbus Operations, S.L.U. | Composite hydrogen tank for an aircraft |
Also Published As
Publication number | Publication date |
---|---|
SE9001841D0 (en) | 1990-05-22 |
WO1991018239A1 (en) | 1991-11-28 |
SE9001841L (en) | 1991-11-23 |
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