US20060180959A1 - Method of coupling a component to a fuel fill tube - Google Patents

Method of coupling a component to a fuel fill tube Download PDF

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Publication number
US20060180959A1
US20060180959A1 US11/276,148 US27614806A US2006180959A1 US 20060180959 A1 US20060180959 A1 US 20060180959A1 US 27614806 A US27614806 A US 27614806A US 2006180959 A1 US2006180959 A1 US 2006180959A1
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US
United States
Prior art keywords
parison
hot
component
mold
filler neck
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.)
Abandoned
Application number
US11/276,148
Inventor
Chad McClung
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.)
Stant USA Corp
Original Assignee
Stant USA Corp
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 Stant USA Corp filed Critical Stant USA Corp
Priority to US11/276,148 priority Critical patent/US20060180959A1/en
Assigned to STANT MANUFACTURING INC. reassignment STANT MANUFACTURING INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MCCLUNG, CHAD A.
Publication of US20060180959A1 publication Critical patent/US20060180959A1/en
Assigned to GMAC COMMERICAL FINANCE LLC, AS AGENT reassignment GMAC COMMERICAL FINANCE LLC, AS AGENT SECURITY AGREEMENT Assignors: STANDARD-THOMSON CORPORATION, STANT CORPORATION, STANT MANUFACTURING INC.
Assigned to STANT MANUFACTURING INC., STANDARD-THOMSON, STANT CORPORATION reassignment STANT MANUFACTURING INC. RELEASE BY SECURED PARTY (SEE DOCUMENT FOR DETAILS). Assignors: GMAC COMMERICAL FINANCE LLC, AS AGENT
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/42Component parts, details or accessories; Auxiliary operations
    • B29C49/4242Means for deforming the parison prior to the blowing operation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/022Particular heating or welding methods not otherwise provided for
    • B29C65/028Particular heating or welding methods not otherwise provided for making use of inherent heat, i.e. the heat for the joining comes from the moulding process of one of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/12Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
    • B29C66/122Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section
    • B29C66/1222Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section comprising at least a lapped joint-segment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/12Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
    • B29C66/122Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section
    • B29C66/1224Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section comprising at least a butt joint-segment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/13Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
    • B29C66/131Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General 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
    • B29C66/51Joining 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
    • B29C66/53Joining single elements to tubular articles, hollow articles or bars
    • B29C66/534Joining single elements to open ends of tubular or hollow articles or to the ends of bars
    • B29C66/5344Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially annular, i.e. of finite length, e.g. joining flanges to tube ends
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General 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
    • B29C66/61Joining from or joining on the inside
    • B29C66/612Making circumferential joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General 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
    • B29C66/72General 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
    • B29C66/723General 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 being multi-layered
    • B29C66/7234General 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 being multi-layered comprising a barrier layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/82Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps
    • B29C66/826Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined
    • B29C66/8266Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined using fluid pressure directly acting on the parts to be joined
    • B29C66/82661Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined using fluid pressure directly acting on the parts to be joined by means of vacuum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/83General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/832Reciprocating joining or pressing tools
    • B29C66/8322Joining or pressing tools reciprocating along one axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03Fuel tanks
    • B60K15/04Tank inlets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L55/00Devices or appurtenances for use in, or in connection with, pipes or pipe systems
    • F16L55/10Means for stopping flow from or in pipes or hoses
    • F16L55/115Caps
    • F16L55/1157Caps using hooks, pawls, or other movable or insertable locking members
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2791/00Shaping characteristics in general
    • B29C2791/001Shaping in several steps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2791/00Shaping characteristics in general
    • B29C2791/004Shaping under special conditions
    • B29C2791/006Using vacuum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/02Combined blow-moulding and manufacture of the preform or the parison
    • B29C49/04Extrusion blow-moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/20Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor of articles having inserts or reinforcements ; Handling of inserts or reinforcements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/42Component parts, details or accessories; Auxiliary operations
    • B29C49/4242Means for deforming the parison prior to the blowing operation
    • B29C49/4244Means for deforming the parison prior to the blowing operation during or after laying preform into the final mould
    • B29C49/4245Means for deforming the parison prior to the blowing operation during or after laying preform into the final mould aided by air floating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/42Component parts, details or accessories; Auxiliary operations
    • B29C49/4273Auxiliary operations after the blow-moulding operation not otherwise provided for
    • B29C49/428Joining
    • B29C49/42806Joining auxiliary parts to the article, e.g. handle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General 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
    • B29C66/71General 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General 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
    • B29C66/73General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/737General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
    • B29C66/7377General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline
    • B29C66/73773General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being semi-crystalline
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General 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
    • B29C66/73General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B29C66/73921General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/04Polymers of ethylene
    • B29K2023/06PE, i.e. polyethylene
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2059/00Use of polyacetals, e.g. POM, i.e. polyoxymethylene or derivatives thereof, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/0079Liquid crystals
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0065Permeability to gases
    • B29K2995/0067Permeability to gases non-permeable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0068Permeability to liquids; Adsorption
    • B29K2995/0069Permeability to liquids; Adsorption non-permeable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2023/00Tubular articles
    • B29L2023/004Bent tubes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/712Containers; Packaging elements or accessories, Packages
    • B29L2031/7172Fuel tanks, jerry cans

Definitions

  • the present disclosure relates to blow-molding methods, and particularly to methods of coupling a component to an element formed in a blow mold. More particularly, the present disclosure relates to formation of a fuel tank filler neck using a blow-molding process.
  • a component such as an inlet cup or inlet check valve is mated and bonded to a parison while the parison is located in a closed blow mold.
  • the parison is formed in the blow mold to define a fuel tank filler neck in an illustrative embodiment.
  • a vacuum is used to draw a hot parison into a mold cavity and inflation air is blown into a central passageway formed in the hot parison to inflate the parison in the mold cavity.
  • a first filler neck component e.g., an inlet cup
  • a first filler neck component is mated to a first end of the hot parison in the mold cavity to melt a portion of the first filler neck component and bond the first filler neck component to the first end of the hot parison.
  • a second filler neck component (e.g., an inlet check valve) is mated to a second end of the hot parison in the mold cavity to melt a portion of the second filler neck component and bond the second filler neck component to the second end of the hot parison.
  • FIG. 1 is a perspective view of a fuel tank coupled to a tank filler neck including an inlet cup and closure cap at an outer end of the filler neck and an inlet check valve at an inner end of the filler neck;
  • FIG. 2 is a sectional view showing a “closed” blow mold in accordance with the present disclosure and showing an extruded uninflated parison located in a mold cavity formed between first and second mold dies and showing an inlet cup arranged to be mated with an upper end of the parison and an inlet check valve arranged to be mated with a lower end of the parison;
  • FIG. 3 is a sectional view similar to FIG. 2 after “inflation air” has been blown into the closed blow mold to inflate the parison deployed in the mold cavity and showing the inlet cup after it has been mated with the upper end of the inflated parison and the inlet check valve after it has been mated with the lower end of the inflated parison;
  • FIG. 4 is an enlarged sectional view showing a fixture moving toward the closed blow mold and carrying an inlet cup to be mated with an upper end of the inflated parison located in the closed blow mold;
  • FIG. 5 is a view similar to FIG. 4 showing the inlet cup mated to the parison before withdrawal of the fixture from the inlet cup and from the closed blow mold;
  • FIG. 6 is a view similar to FIGS. 4 and 5 of another embodiment in accordance with the present disclosure wherein a vacuum is used to draw a parison to mate with an inlet cup positioned as an “insert” in a mold.
  • a vehicle fuel system 10 comprises a fuel tank 12 , a filler neck 14 having a lower end 16 coupled to fuel tank 12 and an upper end 18 , and a removable closure cap 20 coupled to upper end 18 of filler neck 14 to close an open mouth 22 formed in the upper end of filler neck 14 as shown, for example, in FIG. 1 .
  • Vehicle fuel system 10 also comprises an inlet check valve 24 and an inlet cup 26 coupled to filler neck 14 as filler neck 14 is formed in a blow mold 28 using methods disclosed herein as suggested, for example, in FIGS. 2 and 3 .
  • Inlet check valve 24 is configured to lie in a fuel-conducting passageway 15 formed in filler neck 14 and regulate flow of liquid fuel and fuel vapor therethrough.
  • inlet check valve 24 includes a “one-way” valve member 30 that is slidable between a passageway-closing position shown in FIG. 1 and a passageway-opening position (not shown).
  • a fuel-dispensing pump nozzle (not shown) contacts and moves valve member 30 inwardly against a yieldable biasing spring 32 to assume the opened position so that liquid fuel can flow past the one-way valve member 30 and into a fuel reservoir 34 provided in an interior region 36 of fuel tank 12 .
  • Inlet cup 26 includes a mount 38 and a nozzle restrictor 40 coupled to mount 38 and formed to include an aperture 42 as shown, for example, in FIGS. 1 and 4 .
  • Mount 38 is coupled to outer end 18 of filler neck 14 by any suitable means and is sized to receive an inner portion of closure cap 20 therein.
  • Aperture 42 is sized to receive a dispensing portion of a pump nozzle (not shown) therein during tank refueling.
  • a hot extruded uninflated parison 44 is drawn using a vacuum 46 through an elongated mold cavity 48 defined by first and second mold dies 51 , 52 .
  • These mold dies 51 , 52 are included in blow mold 28 and are shown in a “closed” position in FIGS. 2-5 . It is within the scope of the present disclosure to apply vacuum 46 to elongated mold cavity 48 via either first opening 48 ′ or second opening 48 ′′.
  • inflation air 50 is blown into a central passageway 54 formed in hot extruded parison 44 to inflate parison 44 while parison 44 is deployed in the closed mold cavity 48 .
  • inflation air 50 expands the thin-walled hot-extruded parison 44 in radially outwardly extending directions to mate with half-round surfaces 151 , 152 (or any other suitable surfaces) formed in first and second mold dies 51 , 52 .
  • a component such as inlet check valve 24 , inlet cup 26 , or other suitable element is mated with parison 44 as suggested in FIG. 3 to cause a portion of the component contacting the hot parison 44 to “melt” so that a bond will develop between parison 44 and the mating component as the “hot” materials comprising parison 44 and the mating component solidify as they cool.
  • Means is provided for moving a component to mate with a portion of a hot parison 44 to cause a bond to be established between parison 44 and that component.
  • a fixture 60 is provided to carry inlet cup 26 into open mouth 62 of the inflated, hot, extruded parison 44 and hold inlet cup 26 in open mouth 62 until the plastics material comprising mount 38 of inlet cup 26 bonds to parison 44 .
  • fixture 60 is withdrawn, leaving inlet cup 26 mated with inflated parison 44 as shown, for example, in FIG. 3 .
  • parison 44 is made of polyarylamide (PAA). Parison 44 could also be made of liquid crystalline polyethylene (LCP). PAA is suitable for blow-molding. LCP is a low-permeation material suitable for blow-molding. Exterior portions of mount 38 can be made of PAA, LCP, or some suitable material that bonds to PAA, LCP, or the material used to make parison 44 .
  • PAA polyarylamide
  • LCP liquid crystalline polyethylene
  • Exterior portions of mount 38 can be made of PAA, LCP, or some suitable material that bonds to PAA, LCP, or the material used to make parison 44 .
  • mount 38 of inlet cup 26 is made of polyethylene or a combination of polyethylene and acetal. It is within the scope of this disclosure to position inlet cup 26 as an insert in a mold 70 and draw a vacuum 72 using vacuum supply 74 through inlet cup 26 via openings formed in nozzle restrictor 40 to move parison 44 in direction 76 to mate inlet cup 26 to a parison in the mold as suggested diagrammatically in FIG. 6 .
  • inlet cup 26 By mating and bonding a component such as inlet cup 26 to parison 44 while parison 44 is located in a closed mold 28 , secondary processes are not needed to couple an inlet cup to a filler neck after the filler neck is removed from a mold.
  • Inlet cup 26 is mated and bonded to parison 44 to yield a more robust joint or union between inlet cup 26 and parison 44 .
  • An o-ring seal between inlet cup 26 and filler neck 14 may or may not be needed.
  • a method of coupling a component to a fuel fill tube in accordance with the present disclosure comprises the steps of providing an elongated mold cavity 48 between a first mold die 51 mated to a second mold die 52 , and using a vacuum 46 to draw a hot extruded parison 44 into elongated mold cavity 48 as suggested in FIG. 2 .
  • Hot extruded parison 44 is formed to include opposite first and second ends 47 , 49 and a central passageway 54 extending therethrough between first and second ends 47 , 49 .
  • the present method further comprises the steps of blowing inflation air 50 through an opening 47 ′ formed in first end 47 into central passageway 54 to inflate hot extruded parison 44 while hot extruded parison 44 is located in elongated mold cavity 48 and mating a first filler neck component 26 to first end 47 of hot extruded parison 44 after inflation of hot extruded parison 44 . It is also within the scope of the present disclosure to blow inflation air 50 through an opening 49 ′ formed in second end 49 to enlarge opening 47 ′ in first end 47 to receive first filler neck component 26 therein.
  • the mating step occurs while parison material comprising hot extruded parison 44 that has been heated to a hot temperature above a melting point of component material comprising first filler neck component 26 to (1) transfer heat associated with hot extruded parison 44 to first filler neck component 26 to melt some of the component material included in first filler neck component 26 and (2) cause said some of the component material to mate with parison material in hot extruded parison 44 so that a bond develops between mating portions of hot extruded parison 44 and first filler neck component 26 as hot extruded parison 44 and first filler neck component 26 cool to anchor first filler neck component 26 to the parison 44 .
  • the mating step further comprises the steps of mounting first filler neck component 26 on a fixture 60 and moving fixture 60 into central passageway 54 formed in hot extruded parison 44 through an opening 47 ′ formed in first end 47 of hot extruded parison 44 to deposit a portion of the first filler neck component 26 in the central passage to facilitate transfer of heat from parison material in hot extruded parison 44 to component material of first filler neck component 26 ′ located in central passageway 54 of hot extruded parison 44 as suggested in FIGS. 4 and 5 .
  • the mating step further comprises the step of separating fixture 60 from first filler neck component 26 after parison 44 and component materials have cooled and bonded to anchor first filler neck component 26 to parison 44 .
  • the using step further comprises the steps of introducing a hot extruded parison 44 into elongated mold cavity 48 through a first cavity inlet 48 ′ formed in one end of elongated mold cavity 48 while first mold die 51 is mated to second mold die 52 and applying a vacuum 46 to hot extruded parison 44 through a second cavity inlet 48 ′′ formed in an opposite end of elongated mold cavity 48 while first mold die 51 is mated to second mold die 52 to move hot extruded parison through elongated mold cavity 48 in a direction 55 toward second cavity inlet 48 ′′ as suggested in FIG. 2 .
  • the applying step ends before the blowing step begins in an illustrative embodiment. Inflation air 50 is blown through first cavity inlet 48 ′ into central passageway 54 of hot extruded parison 44 .
  • a second filler neck component 24 is mated to second end 49 of hot extruded parison 44 after inflation of hot extruded parison 44 as suggested in FIGS. 2 and 3 .
  • This mating step occurs while parison material comprising the hot extruded parison has been heated to a hot temperature above a melting point of component material comprising second filler neck component 24 to (1) transfer heat associated with hot extruded parison 44 to second filler neck component 24 to melt some of the component material included in second filler neck component 24 and (2) cause said some of the component material to mate with parison material in hot extruded parison 44 so that a bond develops between mating portions of hot extruded parison 44 and second filler neck component 24 as hot extruded parison 44 and second filler neck component 24 cool to anchor second filler neck component 24 to parison 44 . It is within the scope of the present disclosure to blow inflation air 50 through opening 49 ′ formed in second end 49 of parison 44 to enlarge opening

Abstract

A component is mated to a parison placed in a blow mold. The parison is configured to define a fuel fill tube.

Description

  • This application claims priority under 35 U.S.C. § 119(e) to U.S. Provisional Application Ser. No. 60/653,833, filed Feb. 17, 2005, which is expressly incorporated by reference herein.
  • BACKGROUND
  • The present disclosure relates to blow-molding methods, and particularly to methods of coupling a component to an element formed in a blow mold. More particularly, the present disclosure relates to formation of a fuel tank filler neck using a blow-molding process.
  • SUMMARY
  • In accordance with the present disclosure, a component such as an inlet cup or inlet check valve is mated and bonded to a parison while the parison is located in a closed blow mold. The parison is formed in the blow mold to define a fuel tank filler neck in an illustrative embodiment.
  • In accordance with one illustrative method, a vacuum is used to draw a hot parison into a mold cavity and inflation air is blown into a central passageway formed in the hot parison to inflate the parison in the mold cavity. A first filler neck component (e.g., an inlet cup) is mated to a first end of the hot parison in the mold cavity to melt a portion of the first filler neck component and bond the first filler neck component to the first end of the hot parison. A second filler neck component (e.g., an inlet check valve) is mated to a second end of the hot parison in the mold cavity to melt a portion of the second filler neck component and bond the second filler neck component to the second end of the hot parison.
  • Features of the present disclosure will become apparent to those skilled in the art upon consideration of the following detailed description of illustrative embodiments exemplifying the best mode of carrying out the disclosure as presently perceived.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The detailed description particularly refers to the accompanying figures in which:
  • FIG. 1 is a perspective view of a fuel tank coupled to a tank filler neck including an inlet cup and closure cap at an outer end of the filler neck and an inlet check valve at an inner end of the filler neck;
  • FIG. 2 is a sectional view showing a “closed” blow mold in accordance with the present disclosure and showing an extruded uninflated parison located in a mold cavity formed between first and second mold dies and showing an inlet cup arranged to be mated with an upper end of the parison and an inlet check valve arranged to be mated with a lower end of the parison;
  • FIG. 3 is a sectional view similar to FIG. 2 after “inflation air” has been blown into the closed blow mold to inflate the parison deployed in the mold cavity and showing the inlet cup after it has been mated with the upper end of the inflated parison and the inlet check valve after it has been mated with the lower end of the inflated parison;
  • FIG. 4 is an enlarged sectional view showing a fixture moving toward the closed blow mold and carrying an inlet cup to be mated with an upper end of the inflated parison located in the closed blow mold;
  • FIG. 5 is a view similar to FIG. 4 showing the inlet cup mated to the parison before withdrawal of the fixture from the inlet cup and from the closed blow mold; and
  • FIG. 6 is a view similar to FIGS. 4 and 5 of another embodiment in accordance with the present disclosure wherein a vacuum is used to draw a parison to mate with an inlet cup positioned as an “insert” in a mold.
  • DETAILED DESCRIPTION OF THE DRAWINGS
  • A vehicle fuel system 10 comprises a fuel tank 12, a filler neck 14 having a lower end 16 coupled to fuel tank 12 and an upper end 18, and a removable closure cap 20 coupled to upper end 18 of filler neck 14 to close an open mouth 22 formed in the upper end of filler neck 14 as shown, for example, in FIG. 1. Vehicle fuel system 10 also comprises an inlet check valve 24 and an inlet cup 26 coupled to filler neck 14 as filler neck 14 is formed in a blow mold 28 using methods disclosed herein as suggested, for example, in FIGS. 2 and 3.
  • Inlet check valve 24 is configured to lie in a fuel-conducting passageway 15 formed in filler neck 14 and regulate flow of liquid fuel and fuel vapor therethrough. In the illustrated embodiment, inlet check valve 24 includes a “one-way” valve member 30 that is slidable between a passageway-closing position shown in FIG. 1 and a passageway-opening position (not shown). During refueling, liquid fuel discharged into an “open” filler neck 14 by a fuel-dispensing pump nozzle (not shown) contacts and moves valve member 30 inwardly against a yieldable biasing spring 32 to assume the opened position so that liquid fuel can flow past the one-way valve member 30 and into a fuel reservoir 34 provided in an interior region 36 of fuel tank 12. Reference is made to U.S. Pat. No. 5,568,828 and application Ser. No. 10/810,982, filed Mar. 26, 2004, for disclosures relating to vehicle fuel systems and inlet check valves, which patent and application are hereby incorporated by reference herein.
  • Inlet cup 26 includes a mount 38 and a nozzle restrictor 40 coupled to mount 38 and formed to include an aperture 42 as shown, for example, in FIGS. 1 and 4. Mount 38 is coupled to outer end 18 of filler neck 14 by any suitable means and is sized to receive an inner portion of closure cap 20 therein. Aperture 42 is sized to receive a dispensing portion of a pump nozzle (not shown) therein during tank refueling.
  • As suggested, for example, in FIG. 2, a hot extruded uninflated parison 44 is drawn using a vacuum 46 through an elongated mold cavity 48 defined by first and second mold dies 51, 52. These mold dies 51, 52 are included in blow mold 28 and are shown in a “closed” position in FIGS. 2-5. It is within the scope of the present disclosure to apply vacuum 46 to elongated mold cavity 48 via either first opening 48′ or second opening 48″.
  • As suggested in FIGS. 2 and 3, inflation air 50 is blown into a central passageway 54 formed in hot extruded parison 44 to inflate parison 44 while parison 44 is deployed in the closed mold cavity 48. As suggested, for example, in FIG. 3, inflation air 50 expands the thin-walled hot-extruded parison 44 in radially outwardly extending directions to mate with half-round surfaces 151, 152 (or any other suitable surfaces) formed in first and second mold dies 51, 52. While parison 44 is hot, a component such as inlet check valve 24, inlet cup 26, or other suitable element is mated with parison 44 as suggested in FIG. 3 to cause a portion of the component contacting the hot parison 44 to “melt” so that a bond will develop between parison 44 and the mating component as the “hot” materials comprising parison 44 and the mating component solidify as they cool.
  • Means is provided for moving a component to mate with a portion of a hot parison 44 to cause a bond to be established between parison 44 and that component. As suggested, for example, in FIGS. 4 and 5, a fixture 60 is provided to carry inlet cup 26 into open mouth 62 of the inflated, hot, extruded parison 44 and hold inlet cup 26 in open mouth 62 until the plastics material comprising mount 38 of inlet cup 26 bonds to parison 44. After cooling has been completed, fixture 60 is withdrawn, leaving inlet cup 26 mated with inflated parison 44 as shown, for example, in FIG. 3.
  • In an illustrative embodiment, parison 44 is made of polyarylamide (PAA). Parison 44 could also be made of liquid crystalline polyethylene (LCP). PAA is suitable for blow-molding. LCP is a low-permeation material suitable for blow-molding. Exterior portions of mount 38 can be made of PAA, LCP, or some suitable material that bonds to PAA, LCP, or the material used to make parison 44.
  • In other embodiments, mount 38 of inlet cup 26 is made of polyethylene or a combination of polyethylene and acetal. It is within the scope of this disclosure to position inlet cup 26 as an insert in a mold 70 and draw a vacuum 72 using vacuum supply 74 through inlet cup 26 via openings formed in nozzle restrictor 40 to move parison 44 in direction 76 to mate inlet cup 26 to a parison in the mold as suggested diagrammatically in FIG. 6.
  • By mating and bonding a component such as inlet cup 26 to parison 44 while parison 44 is located in a closed mold 28, secondary processes are not needed to couple an inlet cup to a filler neck after the filler neck is removed from a mold. Inlet cup 26 is mated and bonded to parison 44 to yield a more robust joint or union between inlet cup 26 and parison 44. An o-ring seal between inlet cup 26 and filler neck 14 may or may not be needed.
  • A method of coupling a component to a fuel fill tube in accordance with the present disclosure comprises the steps of providing an elongated mold cavity 48 between a first mold die 51 mated to a second mold die 52, and using a vacuum 46 to draw a hot extruded parison 44 into elongated mold cavity 48 as suggested in FIG. 2. Hot extruded parison 44 is formed to include opposite first and second ends 47, 49 and a central passageway 54 extending therethrough between first and second ends 47, 49.
  • The present method further comprises the steps of blowing inflation air 50 through an opening 47′ formed in first end 47 into central passageway 54 to inflate hot extruded parison 44 while hot extruded parison 44 is located in elongated mold cavity 48 and mating a first filler neck component 26 to first end 47 of hot extruded parison 44 after inflation of hot extruded parison 44. It is also within the scope of the present disclosure to blow inflation air 50 through an opening 49′ formed in second end 49 to enlarge opening 47′ in first end 47 to receive first filler neck component 26 therein. The mating step occurs while parison material comprising hot extruded parison 44 that has been heated to a hot temperature above a melting point of component material comprising first filler neck component 26 to (1) transfer heat associated with hot extruded parison 44 to first filler neck component 26 to melt some of the component material included in first filler neck component 26 and (2) cause said some of the component material to mate with parison material in hot extruded parison 44 so that a bond develops between mating portions of hot extruded parison 44 and first filler neck component 26 as hot extruded parison 44 and first filler neck component 26 cool to anchor first filler neck component 26 to the parison 44.
  • The mating step further comprises the steps of mounting first filler neck component 26 on a fixture 60 and moving fixture 60 into central passageway 54 formed in hot extruded parison 44 through an opening 47′ formed in first end 47 of hot extruded parison 44 to deposit a portion of the first filler neck component 26 in the central passage to facilitate transfer of heat from parison material in hot extruded parison 44 to component material of first filler neck component 26′ located in central passageway 54 of hot extruded parison 44 as suggested in FIGS. 4 and 5. The mating step further comprises the step of separating fixture 60 from first filler neck component 26 after parison 44 and component materials have cooled and bonded to anchor first filler neck component 26 to parison 44.
  • The using step further comprises the steps of introducing a hot extruded parison 44 into elongated mold cavity 48 through a first cavity inlet 48′ formed in one end of elongated mold cavity 48 while first mold die 51 is mated to second mold die 52 and applying a vacuum 46 to hot extruded parison 44 through a second cavity inlet 48″ formed in an opposite end of elongated mold cavity 48 while first mold die 51 is mated to second mold die 52 to move hot extruded parison through elongated mold cavity 48 in a direction 55 toward second cavity inlet 48″ as suggested in FIG. 2. The applying step ends before the blowing step begins in an illustrative embodiment. Inflation air 50 is blown through first cavity inlet 48′ into central passageway 54 of hot extruded parison 44.
  • A second filler neck component 24 is mated to second end 49 of hot extruded parison 44 after inflation of hot extruded parison 44 as suggested in FIGS. 2 and 3. This mating step occurs while parison material comprising the hot extruded parison has been heated to a hot temperature above a melting point of component material comprising second filler neck component 24 to (1) transfer heat associated with hot extruded parison 44 to second filler neck component 24 to melt some of the component material included in second filler neck component 24 and (2) cause said some of the component material to mate with parison material in hot extruded parison 44 so that a bond develops between mating portions of hot extruded parison 44 and second filler neck component 24 as hot extruded parison 44 and second filler neck component 24 cool to anchor second filler neck component 24 to parison 44. It is within the scope of the present disclosure to blow inflation air 50 through opening 49′ formed in second end 49 of parison 44 to enlarge opening 49′ to receive second filler neck component 24 therein.

Claims (20)

1. A method of coupling a component to a fuel fill tube, the method comprising the steps of
providing an elongated mold cavity between a first mold die mated to a second mold die,
using a vacuum to draw a hot extruded parison into the elongated mold cavity, the hot extruded parison being formed to include opposite first and second ends and a central passageway extending therethrough between the first and second ends,
blowing inflation air into the central passageway to inflate the hot extruded parison while the hot extruded parison is located in the elongated mold cavity, and
mating a first filler neck component to the first end of the hot extruded parison after inflation of the hot extruded parison, while parison material comprising the hot extruded parison that has been heated to a hot temperature above a melting point of component material comprising the first filler neck component, to transfer heat associated with the hot extruded parison to the first filler neck component to melt some of the component material included in the first filler neck component and cause said some of the component material to mate with parison material in the first end of the hot extruded parison so that a bond develops between mating portions of the hot extruded parison and the first filler neck component as the hot extruded parison and the first filler neck component cool to anchor the first filler neck component to the first end of the parison.
2. The method of claim 1, further comprising the step of mating a second filler neck component to the second end of the hot extruded parison after inflation of the hot extruded parison, while parison material comprising the hot extruded parison that has been heated to a hot temperature above a melting point of component material comprising the second filler neck component, to transfer heat associated with the hot extruded parison to the second filler neck component to melt some of the component material included in the second filler neck component and cause said some of the component material to mate with parison material in the second end of the hot extruded parison so that a bond develops between mating portions of the hot extruded parison and the second filler neck component as the hot extruded parison and the second filler neck component cool to anchor the second filler neck component to the second end of the parison.
3. The method of claim 1, wherein the mating step further comprises the steps of mounting the first filler neck component on a fixture and moving the fixture into the central passageway formed in the hot extruded parison through an opening formed in the first end of the hot extruded parison to deposit a portion of the first filler neck component in the central passage to facilitate transfer of heat from parison material in the hot extruded parison to component material of the first filler neck component located in the central passageway of the hot extruded parison.
4. The method of claim 3, wherein the mating step further comprises the step of separating the fixture from the first filler neck component after the parison and component materials have cooled and bonded to anchor the first filler neck component to the parison.
5. The method of claim 1, wherein the using step further comprises the steps of introducing a hot extruded parison into the elongated mold cavity through a first cavity inlet formed in one end of the elongated mold cavity while the first mold die is mated to the second mold die and applying a vacuum to the hot extruded parison through a second cavity inlet formed in an opposite end of the elongated mold cavity while the first mold die is mated to the second mold die to move the hot extruded parison through the elongated mold cavity in a direction toward the second cavity inlet.
6. The method of claim 5, wherein the applying step ends before the blowing step begins and wherein inflation air is blown through the first cavity inlet into the central passageway of the hot extruded parison.
7. The method of claim 1, wherein each of the first and second mold dies include a half-round surface forming a boundary portion of the elongated mold cavity and wherein the inflation air expands the hot extruded parison in radially outwardly extending directions to mate with the half-round surfaces of the first and second mold dies while the first mold die is mated with the second mold die.
8. The method of claim 7, wherein the mating step further comprises the steps of mounting the first filler neck component on a fixture and moving the fixture into the central passageway formed in the hot extruded parison through an opening formed in the second end of the hot extruded parison to deposit a portion of the first filler neck in the central passage to facilitate transfer of heat from parison material in the hot extruded parison to component material of the first filler neck component located in the central passageway of the hot extruded parison.
9. The method of claim 8, wherein the mating step further comprises the step of separating the fixture from the first filler neck component after the parison and component materials have cooled and bonded to anchor the filler neck component to the parison.
10. A method of coupling a component to an element formed in a blow mold, the method comprising the steps of
providing a first component and
bonding the first component to a hot parison while the hot parison is located in a closed blow mold.
11. The method of claim 10, wherein the bonding step comprises the step of providing first and second mold dies lying in mating relation to one another and cooperating to form a portion of the closed blow mold and a mold cavity between the mold dies, the first and second mold dies each including a surface facing toward the hot parison and the other mold die, and the bonding step further comprises the steps of inflating the hot parison in radially outwardly extending directions to mate with the surfaces formed in the first and second mold dies and, while the parison is still hot, mating the first component with the hot parison to cause a portion of the first component contacting the hot parison to melt so that a bond develops between the hot parison and the first component as hot materials comprising the parison and the first component solidify as they cool.
12. The method of claim 1, wherein the bonding step further comprises providing means for moving the first component to mate with the hot parison to cause the bond to be established between the hot parison and the first component, the moving means carrying the first component into an open mouth of the inflated, hot parison and holding the first component in the open mouth until material comprising a mount of the first component bonds to the hot parison and, after a cooling has been completed, the moving means is withdrawn, leaving the first component mated to and bonded with the inflated parison.
13. The method of claim 12, wherein the first component is an inlet cup including a mount and a nozzle restrictor coupled to the mount and formed to include an aperture and exterior portions of the mount are made of a low-permeation material that bonds to a low-permeation material used to make the hot parison.
14. The method of claim 13, wherein the low-permeation material of the exterior portions of the mount and the low-permeation material used to make the hot parison includes liquid crystalline polyethylene.
15. The method of claim 10, wherein the bonding step comprises the step of providing first and second mold dies lying in mating relation to one another and cooperating to form a portion of the closed blow mold, and the bonding step further comprises the steps of drawing the hot parison using a vacuum through an elongated mold cavity defined by the first and second mold dies, and the bonding step further comprises the step of blowing inflation air into a central passageway formed in the hot parison to inflate the hot parison while the hot parison is deployed in the mold cavity, the inflation air expanding the hot parison in radially outwardly extending directions to mate with half-round surfaces formed in the first and second mold dies, and while the parison is hot, the first component is mated with the hot parison to cause a portion of the first component contacting the hot parison to melt so that a bond will develop between the hot parison and the first component as materials comprising the hot parison and the first component solidify as they cool.
16. The method of claim 15, wherein the materials comprising the hot parison and the first component include low-permeation materials suitable for blow-molding.
17. The method of claim 1, further comprising the step of providing a second component and wherein the bonding step comprises the step of providing first and second mold dies lying in mating relation to one another and cooperating to form a portion of the closed blow mold and a mold cavity therebetween, the first and second mold dies each including a surface facing toward the hot parison and the other mold die, and the bonding step further comprises the steps of inflating the hot parison in radially outwardly extending directions to mate with the surfaces formed in the first and second mold dies and, while the parison is hot, mating the first component with an upper end of the hot parison and mating the second component with a lower end of the hot parison to cause a portion of the first and second components contacting the hot parison to melt so that a bond develops between the hot parison and each of the first and second components as hot materials comprising the parison and the first and second components solidify as they cool.
18. The method of claim 17, wherein the first component is an inlet cup, the second component is an inlet check valve, and the materials comprising the hot parison, the inlet cup, and the inlet check valve include low-permeation materials suitable for blow molding and suitable for bonding the inlet cup and the inlet check valve to the hot pari son.
19. The method of claim 18, wherein the inlet cup is made of one or more of polyethylene and acetal, and the hot parison is made of liquid crystalline polyethylene.
20. The method of claim 1, wherein the bonding step comprises the step of providing first and second mold dies lying in mating relation to one another and cooperating to form a portion of the closed blow mold and a mold cavity between the mold dies, the first and second mold dies each including a surface facing toward the other mold die, and the bonding step further comprises the steps of positioning the first component as an insert in the closed blow mold and drawing a vacuum through the first component to mate the first component to the hot parison in the closed blow mold.
US11/276,148 2005-02-17 2006-02-15 Method of coupling a component to a fuel fill tube Abandoned US20060180959A1 (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070261752A1 (en) * 2006-04-13 2007-11-15 Stant Manufacturing Inc. Multiple-layer fluid fuel apparatus
GB2505053A (en) * 2012-06-21 2014-02-19 Mercury Plastics Inc Process for joining a fitting to a hollow extrusion
WO2014078259A1 (en) * 2012-11-16 2014-05-22 Illinois Tool Works Inc. Method for producing a blow moulded fuel filler system for a motor vehicle and fuel filler system for a motor vehicle
US8980161B2 (en) 2007-03-06 2015-03-17 Mercury Plastics, Inc. Method for making a reservoir
GB2486952B (en) * 2010-12-14 2016-04-06 Mercury Plastics Inc Method for making a reservoir

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202009001201U1 (en) * 2009-01-31 2009-05-20 Norma Germany Gmbh Tankstutzen
DE102009001968A1 (en) * 2009-03-30 2010-10-07 Geiger Automotive Gmbh Method and device for producing a plastic component and plastic component
US8413431B2 (en) * 2009-06-30 2013-04-09 Eaton Corporation Tank assembly
DE102013107978A1 (en) 2013-07-25 2015-01-29 Contitech Mgw Gmbh Method for producing a media line with an end piece for receiving a component of a coupling
JP6405508B2 (en) * 2013-11-25 2018-10-17 三桜工業株式会社 Fuel supply device and method of assembling the same
US9873320B2 (en) 2015-04-09 2018-01-23 Stant Usa Corp. Fuel tank pressure regulator
US9902258B2 (en) 2015-04-27 2018-02-27 Stant Usa Corp. Fuel tank pressure regulator
US10458366B2 (en) 2016-10-31 2019-10-29 Stant Usa Corp. Fuel tank pressure regulator
WO2018160698A1 (en) 2017-03-01 2018-09-07 Stant Usa Corp. Fuel tank fill pipe assembly
EP3385105B1 (en) * 2017-04-06 2019-04-03 Magna Steyr Fuel Systems GesmbH Refuelling device
US10794335B2 (en) 2018-06-01 2020-10-06 Stant Usa Corp. Fuel tank pressure regulator
CN111059366A (en) * 2018-10-16 2020-04-24 湖南易净环保科技有限公司 Continuous fiber reinforced thermoplastic pipeline and production method thereof
EP4081418A1 (en) 2020-02-14 2022-11-02 Stant USA Corp. Fuel tank pressure regulator

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4719072A (en) * 1984-05-08 1988-01-12 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Method for disposing inner insert in blow molding
US4730652A (en) * 1984-11-06 1988-03-15 Proprietary Technology, Inc. Automotive fuel filler system
US4865799A (en) * 1987-06-18 1989-09-12 Abc Group Method for aligning extruded parison into sepentine-shaped mold cavity
US5308427A (en) * 1992-09-28 1994-05-03 Ford Motor Company Method for fastening plastic articles
US6508275B1 (en) * 2000-03-15 2003-01-21 Salflex Polymers Ltd. Flexible fuel filler pipe
US6589620B1 (en) * 1999-12-18 2003-07-08 Delphi Technologies, Inc. Fuel permeation resistant fuel tank
US6746560B1 (en) * 1998-11-13 2004-06-08 Hoover Materials Handling Group Inc. Blow molding appurtenances to a container

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2929707B2 (en) * 1990-11-14 1999-08-03 日産自動車株式会社 Plastic fuel tank
FR2674933B1 (en) * 1991-04-05 1993-06-11 Caoutchouc Manuf Plastique PROCESS FOR CONTINUOUSLY PRODUCING A FLEXIBLE TUBULAR STRUCTURE COMPRISING A SINGLE-LAYERED SHEET OF MICROMETRIC THICKNESS AND FLEXIBLE TUBULAR STRUCTURES PRODUCED ACCORDING TO THIS PROCESS.
US5759329A (en) * 1992-01-06 1998-06-02 Pilot Industries, Inc. Fluoropolymer composite tube and method of preparation
DE4405409C1 (en) 1994-02-21 1995-08-24 Rasmussen Gmbh Fuel hose
US5568828A (en) * 1994-11-30 1996-10-29 Stant Manufacturing Inc. Fuel-delivery control system
US6170535B1 (en) * 1998-11-17 2001-01-09 Salflex Polymers Ltd. Multi-layer conduit
US6056029A (en) * 1999-03-03 2000-05-02 Stant Manufacturing Inc. Fuel-Transfer system
US20010029994A1 (en) 2000-03-23 2001-10-18 Brown Gregory P. Fuel tank valve apparatus
US6555243B2 (en) * 2000-06-09 2003-04-29 Ems-Chemie Ag Thermoplastic multilayer composites
JP4179528B2 (en) 2001-05-23 2008-11-12 株式会社デンソー Secondary battery inspection method
US7147001B2 (en) 2004-03-26 2006-12-12 Stant Manufacturing Inc. Fuel-transfer system
JP4489558B2 (en) * 2004-10-25 2010-06-23 三桜工業株式会社 Multi-layer resin tube

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4719072A (en) * 1984-05-08 1988-01-12 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Method for disposing inner insert in blow molding
US4730652A (en) * 1984-11-06 1988-03-15 Proprietary Technology, Inc. Automotive fuel filler system
US4865799A (en) * 1987-06-18 1989-09-12 Abc Group Method for aligning extruded parison into sepentine-shaped mold cavity
US5308427A (en) * 1992-09-28 1994-05-03 Ford Motor Company Method for fastening plastic articles
US6746560B1 (en) * 1998-11-13 2004-06-08 Hoover Materials Handling Group Inc. Blow molding appurtenances to a container
US6589620B1 (en) * 1999-12-18 2003-07-08 Delphi Technologies, Inc. Fuel permeation resistant fuel tank
US6508275B1 (en) * 2000-03-15 2003-01-21 Salflex Polymers Ltd. Flexible fuel filler pipe

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070261752A1 (en) * 2006-04-13 2007-11-15 Stant Manufacturing Inc. Multiple-layer fluid fuel apparatus
US8980161B2 (en) 2007-03-06 2015-03-17 Mercury Plastics, Inc. Method for making a reservoir
GB2486952B (en) * 2010-12-14 2016-04-06 Mercury Plastics Inc Method for making a reservoir
GB2505053A (en) * 2012-06-21 2014-02-19 Mercury Plastics Inc Process for joining a fitting to a hollow extrusion
GB2505053B (en) * 2012-06-21 2018-09-05 Mercury Plastics Inc Method for making a reservoir
WO2014078259A1 (en) * 2012-11-16 2014-05-22 Illinois Tool Works Inc. Method for producing a blow moulded fuel filler system for a motor vehicle and fuel filler system for a motor vehicle
US20150290864A1 (en) * 2012-11-16 2015-10-15 Illinois Tool Works Inc. Method for producing a blow moulded fuel filler system for a motor vehicle and fuel filler system for a motor vehicle

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EP1693179A2 (en) 2006-08-23
EP1693179A3 (en) 2008-02-13

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