WO2008118649A1 - Procédé pour lier une pellicule opposée à un noyau de composite de forme libre - Google Patents

Procédé pour lier une pellicule opposée à un noyau de composite de forme libre Download PDF

Info

Publication number
WO2008118649A1
WO2008118649A1 PCT/US2008/056840 US2008056840W WO2008118649A1 WO 2008118649 A1 WO2008118649 A1 WO 2008118649A1 US 2008056840 W US2008056840 W US 2008056840W WO 2008118649 A1 WO2008118649 A1 WO 2008118649A1
Authority
WO
WIPO (PCT)
Prior art keywords
core
recited
adhesive
freeform
composite
Prior art date
Application number
PCT/US2008/056840
Other languages
English (en)
Inventor
Ronald D. Jones
Gary S. Smrtic
William R. Smrtic
Original Assignee
Dynastrosi Laboratories, Inc.
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 Dynastrosi Laboratories, Inc. filed Critical Dynastrosi Laboratories, Inc.
Publication of WO2008118649A1 publication Critical patent/WO2008118649A1/fr

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • 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
    • B29C65/5057—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 positioned between the surfaces to be joined
    • 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
    • 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
    • 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
    • B29C66/114—Single butt joints
    • 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
    • B29C66/124—Tongue and groove joints
    • B29C66/1242—Tongue and groove joints comprising interlocking undercuts
    • B29C66/12423—Dovetailed interlocking undercuts
    • 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
    • B29C66/13—Single 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
    • B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • 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
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/23—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being multiple and parallel or being in the form of tessellations
    • B29C66/234—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being multiple and parallel or being in the form of tessellations said joint lines being in the form of tessellations
    • 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
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/24—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight
    • B29C66/242—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours
    • B29C66/2424—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain
    • B29C66/24243—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain forming a quadrilateral
    • B29C66/24244—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain forming a quadrilateral forming a rectangle
    • 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
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/24—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight
    • B29C66/242—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours
    • B29C66/2424—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain
    • B29C66/24243—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain forming a quadrilateral
    • B29C66/24244—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain forming a quadrilateral forming a rectangle
    • B29C66/24245—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain forming a quadrilateral forming a rectangle forming a square
    • 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
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/24—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight
    • B29C66/242—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours
    • B29C66/2424—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain
    • B29C66/24249—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain forming a specific polygon not provided for in B29C66/24241 - B29C66/24243
    • 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
    • B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
    • B29C66/3032—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined
    • B29C66/30325—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined making use of cavities belonging to at least one of the parts to be joined
    • 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
    • B29C66/53—Joining single elements to tubular articles, hollow articles or bars
    • B29C66/534—Joining single elements to open ends of tubular or hollow articles or to the ends of bars
    • B29C66/5346—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat
    • B29C66/53461—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat joining substantially flat covers and/or substantially flat bottoms to open ends of container bodies
    • 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
    • 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
    • B29C66/725—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 being hollow-walled or honeycombs
    • B29C66/7252—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 being hollow-walled or honeycombs hollow-walled
    • B29C66/72525—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 being hollow-walled or honeycombs hollow-walled comprising honeycomb cores
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00—Producing articles with hollow walls
    • B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/146—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/30—Auxiliary operations or equipment
    • 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
    • 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
    • B29C66/725—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 being hollow-walled or honeycombs
    • B29C66/7254—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 being hollow-walled or honeycombs honeycomb structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING 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
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING 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
    • B29K2309/00—Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
    • B29K2309/08—Glass
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • 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
    • B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608—Honeycomb structures

Definitions

  • Fused Deposition Modeling employs a combination heater/extrusion head operating under computer control to extrude beads or tows of viscous thermoplastic to produce a series of stacked and fused sectional planes.
  • stereo lithography a computer-controlled cold laser is used to cure photocurable epoxy held in a vat, one thin sectional layer at a time.
  • An exemplary composite article manufactured in accordance with the method of the present invention is generally comprised of a freeform- fabricated core to which multiple facing skins are bonded.
  • a tool path computer program is created from a three- dimensional computer-aided-design (3D-CAD) file specifying the geometry and dimensions of a composite core.
  • 3D-CAD computer-aided-design
  • This tool path program controls a freeform-fabrication machine that forms a solid part through the formation of successive layers of polymer, metal, or ceramic materials that are fused together.
  • the 3D-CAD file specifies not only the outer shape of the core, but also specifies the geometry and dimensions of the internal reinforcing structure, which may include hex cells, box cells, trusses, tetrahedral trusses, spheres, and/or arches. Furthermore, and more importantly, the 3D-CAD file specifies channels, receivers, openings, or other integral structural elements that are formed in the core to provide enhanced bonding between the facing skins and the freeform- fabricated core.
  • Figures 1A-1D are various views of an exemplary composite article 10 manufactured in accordance with the method of the present invention.
  • the composite article 10 is comprised of a freeform- fabricated core 12 to which a pair of facing skins 20, 22 are bonded.
  • the core 12 includes upper and lower (exterior) surface members 12a, 12b integral with and bounding an internal reinforcing structure 12c, which in this example, is comprised of an arrangement of hex cells, i.e., a honeycomb structure.
  • the upper and lower surface members 12a, 12b facilitate bonding of the facing skins 20, 22 to the core 12, as further described below.
  • the facing skins 20, 22 are made from a fiber- reinforced polymer material, and the bonding of the facing skins 20, 22 to the freeform- fabricated core 12 makes use of an adhesive film 30.
  • a network of adhesive flow channels 14 is formed in the upper and lower surface members 12a, 12b of the core 12.
  • Figure IB is a partial plan view of the core 12, illustrating the interconnected adhesive flow channels 14 in a grid pattern along the upper surface member 12a of the core 12.
  • Figure 1C is a partial side view of the core 12, illustrating the generally trapezoidal cross-section of the adhesive flow channels 14 in this example.
  • the facing skins 20, 22 are placed against the adhesive film 30 and the core 12. Then, the facing skins 20, 22 are cured to form a strong bond between the facing skins 20, 22 and the core 12.
  • the combination of the facing skins 20, 22 and the freeform-fabricated core 12 is referred to as a "composite lay-up," and the procedure for applying the facing skins 20, 22 to the exterior surface of the core 12 is referred to as the "lay- up.”
  • a vacuum is applied to the composite lay-up, effectively compressing the facing skins 20, 22 against the exterior surfaces of the freeform-fabricated core 12, and then the composite lay-up is cured. This is generally accomplished by subjecting the composite lay-up to a predetermined (higher than ambient) temperature for prescribed period of time while under vacuum pressure; however, some materials are able to cure at ambient atmospheric temperature and pressure.
  • the adhesive is drawn into and fills the interconnected adhesive flow channels 14 formed in the upper and lower surface members 12a, 12b of the core 12. Accordingly, there is an enhanced bond between the facing skins 20, 22 and the freeform-fabricated core 12.
  • Figures 2A-2D are various views of another exemplary composite article 110 manufactured in accordance with the method of the present invention.
  • the composite article 110 is again comprised of a freeform-fabricated core 112 to which a pair of facing skins 120, 122 are bonded through use of an adhesive film 130.
  • the core 112 again includes upper and lower (exterior) surface members 112a, 112b bounding an internal reinforcing structure 112c.
  • an interconnected network of adhesive flow channels 114 is again formed in the upper and lower surface members 112a, 112b of the core 112, similar to those channels described above with reference to Figures IA- ID.
  • generally rectangular openings 115 are also defined through the upper and lower surface members 112a, 112b of the core 112, each such opening 115 being bounded on four sides by the adhesive flow channels 114.
  • each of the upper and lower surface members 112a, 112b are best described as lattices.
  • Figure 2B is a partial plan view of the core 112, illustrating the interconnected adhesive flow channels 114 in a grid pattern along the upper surface member 112a of the core 112.
  • Figure 2C is a partial side view of the core 112, illustrating the generally trapezoidal cross-section of the adhesive flow channels 114 in this example.
  • the facing skins 120, 122 are placed against the adhesive film 130 and the core 112. Then, the facing skins 120, 122 are cured to form a strong bond between the facing skins 120, 122 and the core 112.
  • the adhesive is drawn into and fills the interconnected adhesive flow channels 114 formed in the upper and lower surface members 112a, 112b of the core 112. Accordingly, there again is an enhanced bond between the facing skins 120, 122 and the freeform-fabricated core 112.
  • Figures 3 A-3D are various views of another exemplary composite article 210 manufactured in accordance with the method of the present invention.
  • the composite article 210 is again comprised of a freeform-fabricated core 212 to which a pair of facing skins 220, 222 are bonded through use of an adhesive film 230.
  • the core 212 again includes upper and lower (exterior) surface members 212a, 212b bounding an internal reinforcing structure 212c.
  • multiple receivers 214 are formed in the upper and lower surface members 212a, 212b of the core 212.
  • Figure 3B is a partial plan view of the core 212, illustrating such receivers 214 along the upper surface member 212a of the core 212, and having generally circular upper and lower edges.
  • Figure 3C is a partial side view of the core 212, illustrating that the receivers 214 have a generally trapezoidal cross-section.
  • each receiver 214 can be characterized as being in the shape of a truncated cone.
  • the facing skins 220, 222 are cured to form a strong bond between the facing skins 220, 222 and the core 212.
  • the adhesive is drawn into and fills the receivers 214 formed in the upper and lower surface members 212a, 212b of the core 212. Accordingly, there again is an enhanced bond between the facing skins 220, 222 and the freeform- fabricated core 212.
  • FIG. 4C is a partial side view of the core 312, illustrating that the openings 314 are generally circular or ovular, and more importantly, are positioned near the upper portion of the internal reinforcing structure where the facing skins 320 is bonded to the core 312.
  • each of the walls of the cells of internal reinforcing structure 412c is designed with an enlarged edge portion 414 at the top and bottom thereof.
  • Figure 5B is a partial plan view of the core 412, illustrating such enlarged edge portions 414 along the upper surface of the cells of internal reinforcing structure 412c, which in this example, have a somewhat diamond-shaped cross-section.
  • Figure 5C is a partial side view of the core 412, again illustrating such enlarged edge portions 414.
  • similar enlarged edge portions may also be provided along the lower surface of the cells of internal reinforcing structure 412c.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

L'invention concerne un composé pour lier une pellicule opposée à un noyau de forme libre d'un article composite. De manière générale, ledit composé comporte les étapes consistant à fabriquer un noyau avec une machine de fabrication de formes libres, ledit noyau présentant une structure de renforcement interne muni d'une pluralité d'éléments structurels d'un seul tenant formée sur ou à proximité d'une surface du noyau ; appliquer un adhésif à la surface du noyau ; placer la pellicule opposée contre l'adhésif pour former un recouvrement composite ; et vulcaniser le recouvrement composite pour former l'article composite, l'adhésif passant à travers ou autour des éléments structurels d'un seul tenant et accentuant ainsi la liaison entre la pellicule opposée et le noyau de forme libre.
PCT/US2008/056840 2007-03-27 2008-03-13 Procédé pour lier une pellicule opposée à un noyau de composite de forme libre WO2008118649A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US69170407A 2007-03-27 2007-03-27
US11/691,704 2007-03-27

Publications (1)

Publication Number Publication Date
WO2008118649A1 true WO2008118649A1 (fr) 2008-10-02

Family

ID=39788910

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2008/056840 WO2008118649A1 (fr) 2007-03-27 2008-03-13 Procédé pour lier une pellicule opposée à un noyau de composite de forme libre

Country Status (1)

Country Link
WO (1) WO2008118649A1 (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016022449A1 (fr) * 2014-08-04 2016-02-11 3M Innovative Properties Company Système de finition pour composants imprimés en 3d
WO2017146284A1 (fr) * 2016-02-25 2017-08-31 기술융합협동조합 Procédé de fabrication d'une structure d'impression 3d par renfort et composite
CN108859145A (zh) * 2017-05-08 2018-11-23 波音公司 复合结构组件及其形成方法
CH714293A1 (fr) * 2017-11-01 2019-05-15 Griffes Consulting Sa Structure nid d'abeille.
WO2020012111A1 (fr) * 2018-07-10 2020-01-16 Safran Nacelles Procédé de fabrication d'un panneau composite
WO2020081645A1 (fr) 2018-10-16 2020-04-23 Divergent Technologies, Inc. Procédés et appareil de fabrication de panneaux optimisés et d'autres structures composites
DE102021101194A1 (de) 2021-01-21 2022-07-21 Siegfried Dreizler Wabensandwichanordnung, Wabenbildungselement und Verfahren zum Herstellen einer Wabensandwichanordnung
RU2800439C2 (ru) * 2018-07-10 2023-07-21 Сафран Насель Способ изготовления композитной панели

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6030483A (en) * 1996-09-10 2000-02-29 Wilson; Graeme Paul Method of forming laminates using a tessellated core
US6630093B1 (en) * 1999-08-21 2003-10-07 Ronald D. Jones Method for making freeform-fabricated core composite articles
US20060204714A1 (en) * 2004-09-01 2006-09-14 Hexcel Corporation Rubber-modified edge coating for honeycomb used in panels with composite face sheets

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6030483A (en) * 1996-09-10 2000-02-29 Wilson; Graeme Paul Method of forming laminates using a tessellated core
US6630093B1 (en) * 1999-08-21 2003-10-07 Ronald D. Jones Method for making freeform-fabricated core composite articles
US20060204714A1 (en) * 2004-09-01 2006-09-14 Hexcel Corporation Rubber-modified edge coating for honeycomb used in panels with composite face sheets

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016022449A1 (fr) * 2014-08-04 2016-02-11 3M Innovative Properties Company Système de finition pour composants imprimés en 3d
CN106687269A (zh) * 2014-08-04 2017-05-17 3M创新有限公司 用于3d打印部件的修整系统
EP3177445A4 (fr) * 2014-08-04 2018-03-07 3M Innovative Properties Company Système de finition pour composants imprimés en 3d
WO2017146284A1 (fr) * 2016-02-25 2017-08-31 기술융합협동조합 Procédé de fabrication d'une structure d'impression 3d par renfort et composite
CN108859145A (zh) * 2017-05-08 2018-11-23 波音公司 复合结构组件及其形成方法
CH714293A1 (fr) * 2017-11-01 2019-05-15 Griffes Consulting Sa Structure nid d'abeille.
WO2020012111A1 (fr) * 2018-07-10 2020-01-16 Safran Nacelles Procédé de fabrication d'un panneau composite
FR3083735A1 (fr) * 2018-07-10 2020-01-17 Safran Nacelles Procede de fabrication d’un panneau composite
RU2800439C2 (ru) * 2018-07-10 2023-07-21 Сафран Насель Способ изготовления композитной панели
US11840029B2 (en) 2018-07-10 2023-12-12 Safran Nacelles Method for manufacturing a composite panel
WO2020081645A1 (fr) 2018-10-16 2020-04-23 Divergent Technologies, Inc. Procédés et appareil de fabrication de panneaux optimisés et d'autres structures composites
CN111069598A (zh) * 2018-10-16 2020-04-28 戴弗根特技术有限公司 用于制造优化的板件和其它复合结构的方法和设备
EP3866998A4 (fr) * 2018-10-16 2022-08-03 Divergent Technologies, Inc. Procédés et appareil de fabrication de panneaux optimisés et d'autres structures composites
DE102021101194A1 (de) 2021-01-21 2022-07-21 Siegfried Dreizler Wabensandwichanordnung, Wabenbildungselement und Verfahren zum Herstellen einer Wabensandwichanordnung

Similar Documents

Publication Publication Date Title
WO2008118649A1 (fr) Procédé pour lier une pellicule opposée à un noyau de composite de forme libre
JP6505997B2 (ja) 幾何学形状充填材要素を有するラミネート複合角部充填材およびそれを形成する方法
US8642168B2 (en) Composite structure having reinforced core and method of making the same
US8512853B2 (en) Composite structure having reinforced core
JP6360672B2 (ja) 複合材径フィラーとその形成方法
EP2605902B1 (fr) Structures composites ayant des joints composite-métal et procédé pour leur fabrication
EP2406062B1 (fr) Reprise liée prévisible de structures composites à l'aide de pièces adaptées au besoin
US9566739B2 (en) Composite filler
JP2001253393A (ja) 複合材パネルおよびその製造方法
WO2004022319A1 (fr) Materiaux en nid d'abeilles ameliores destines a des applications aerospatiales
EP2070694B1 (fr) Panneau composite et son procédé de fabrication
EP2234793B1 (fr) Pièce constituée de matériau composite avec des zones d'épaisseur différente
JP5319538B2 (ja) 翼パネル構造
EP3769948B1 (fr) Structure composite dotée d'un élément de remplissage thermoplastique
JP5731392B2 (ja) 航空機の平面部材およびその製造方法
KR20160120270A (ko) 서로 교차하는 중공 보강 구조체들을 생산하기 위한 방법
US11458719B2 (en) Method for joining by bonding of parts, in particular composite parts having fibrous reinforcement
EP3231586B1 (fr) Structure dotée de structures unitaires assemblées
Falken et al. From development of multi-material skins to morphing flight hardware production
US20200384721A1 (en) Composite Panel Sandwich Structures with Integrated Joints
CN114889233B (zh) 一种轻型翼肋及其成型方法
JPH04244839A (ja) 炭素繊維強化複合材料の作製方法
Merlette Development of lightweight graphite/polyimide sandwich panels, phases 3, 4 and 5

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 08743844

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 08743844

Country of ref document: EP

Kind code of ref document: A1