FR2720795A1 - Straight bars for transmitting longitudinal forces based on reinforced composite materials. - Google Patents
Straight bars for transmitting longitudinal forces based on reinforced composite materials. Download PDFInfo
- Publication number
- FR2720795A1 FR2720795A1 FR9506450A FR9506450A FR2720795A1 FR 2720795 A1 FR2720795 A1 FR 2720795A1 FR 9506450 A FR9506450 A FR 9506450A FR 9506450 A FR9506450 A FR 9506450A FR 2720795 A1 FR2720795 A1 FR 2720795A1
- Authority
- FR
- France
- Prior art keywords
- bars
- fibers
- sleeve
- axis
- partial
- 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.)
- Granted
Links
- 239000011208 reinforced composite material Substances 0.000 title description 3
- 239000003733 fiber-reinforced composite Substances 0.000 claims abstract description 7
- 239000000463 material Substances 0.000 claims abstract description 7
- 238000005304 joining Methods 0.000 claims abstract description 3
- 239000000835 fiber Substances 0.000 claims description 47
- 239000004744 fabric Substances 0.000 claims description 8
- 239000006260 foam Substances 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 239000011159 matrix material Substances 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 4
- 238000004804 winding Methods 0.000 claims description 4
- 239000002131 composite material Substances 0.000 claims description 3
- 229920003002 synthetic resin Polymers 0.000 claims description 3
- 239000000057 synthetic resin Substances 0.000 claims description 3
- 238000005452 bending Methods 0.000 claims description 2
- 230000000284 resting effect Effects 0.000 claims 2
- 238000005520 cutting process Methods 0.000 claims 1
- 238000005192 partition Methods 0.000 claims 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 4
- 239000004917 carbon fiber Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
- F16C7/02—Constructions of connecting-rods with constant length
- F16C7/026—Constructions of connecting-rods with constant length made of fibre reinforced resin
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
- B29C65/5028—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being textile in woven or non-woven form
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5042—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like covering both elements to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—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
- B29C66/1142—Single butt to butt joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—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
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/522—Joining tubular articles
- B29C66/5221—Joining tubular articles for forming coaxial connections, i.e. the tubular articles to be joined forming a zero angle relative to each other
-
- 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
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/522—Joining tubular articles
- B29C66/5229—Joining tubular articles involving the use of a socket
-
- 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
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/526—Joining bars
- B29C66/5261—Joining bars for forming coaxial connections, i.e. the bars to be joined forming a zero angle relative to each other
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—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
- B29C66/63—Internally supporting the article during joining
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/228—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being stacked in parallel layers with fibres of adjacent layers crossing at substantial angles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B7/00—Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
-
- 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
- B29C2793/00—Shaping techniques involving a cutting or machining operation
- B29C2793/009—Shaping techniques involving a cutting or machining operation after shaping
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
- B29C65/5021—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being multi-layered
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
-
- 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
- B29C66/73—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 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
- B29C66/739—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 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
- B29C66/7392—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 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
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- 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
- 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
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0809—Fabrics
- B29K2105/0827—Braided fabrics
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- 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
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/10—Cords, strands or rovings, e.g. oriented cords, strands or rovings
- B29K2105/101—Oriented
- B29K2105/108—Oriented arranged in parallel planes and crossing at substantial angles
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- 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
- B29K2307/00—Use of elements other than metals as reinforcement
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- 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
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- 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
- B29L2031/06—Rods, e.g. connecting rods, rails, stakes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
- F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
Barre droite transmettant des forces longitudinales composée de deux ou plusieurs barres partielles coaxiales (4, 6) qui sont respectivement reliées par un manchon (16) en les assemblant bout à bout. L'objectif de l'invention est un moyen pour assembler de façon simple des barres individuelles à base de matériaux composites renforcés avec des fibres avec une grande résistance à la flexion et une paroi mince en barres de grande longueur au moyen d'un raccord par manchon sans écart important de rigidité.Straight bar transmitting longitudinal forces composed of two or more coaxial partial bars (4, 6) which are respectively connected by a sleeve (16) by joining them end to end. The object of the invention is a means for simply assembling individual bars based on fiber-reinforced composite materials with high flexural strength and a thin wall in long bars by means of a connector by sleeve without significant difference in rigidity.
Description
! "Barres droites de transmission de forces longitudinales à base de! "Straight bars of longitudinal force transmission based on
matériaux composites renforcés" La présente invention concerne une barre droite transmettant des forces longitudinales qui se compose de deux ou plusieurs barres partielles coaxiales qui sont respectivement reliées par un manchon en les assemblant reinforced composite materials "The present invention relates to a straight bar transmitting longitudinal forces which consists of two or more coaxial partial bars which are respectively connected by a sleeve by assembling them
bout à bout.end to end.
Par DE 1 871 814 El, on sait relier des tuyaux métalliques en les assemblant bout à bout par un manchon enfilé sur les extrémités lisses des tuyaux et empiétant sur l'emplacement du joint, manchon qui est relié par collage aux extrémités des tuyaux. Pour les conduites en cuivre, on sait By DE 1 871 814 El, it is known to connect metal pipes by assembling them end to end by a sleeve threaded on the smooth ends of the pipes and encroaching on the location of the joint, sleeve which is connected by gluing to the ends of the pipes. For copper pipes, we know
faire la jonction entre les extrémités des tuyaux et le manchon par brasure. join the ends of the pipes and the sleeve by brazing.
Par DE 38 18 066 A1, on sait relier entre eux des tuyaux en carbone ou graphite sur un plan coaxial par collage. Les tuyaux sont alors munis à By DE 38 18 066 A1, we know how to connect carbon or graphite pipes to each other on a coaxial plane by gluing. The pipes are then fitted to
l'avant de cônes qui s'emboîtent et collés entre eux sur les faces des cônes. the front of cones that fit together and glued together on the faces of the cones.
Une manchette en fibres de carbone imprégnée d'un thermoplastique est étirée sur l'extrémité extérieure de la fente conique. La manchette est alors A carbon fiber cuff impregnated with a thermoplastic is stretched over the outer end of the conical slot. The cuff is then
enroulée de préférence sur les tuyaux. preferably wound on the pipes.
Par DE 23 26 628, on connaît un raccord fait de coques de manchon collées pour tuyaux et éléments tubulaires. Les parties d'arête juxtaposées des coques de manchon conçues de facon rigide sont agencées de telle manière qu'elles se chevauchent pour agrandir la surface d'adhérence du DE 23 26 628 discloses a connector made of glued sleeve shells for pipes and tubular elements. The juxtaposed edge portions of the rigidly designed sleeve shells are arranged so that they overlap to enlarge the adhesion surface of the
point de jonction.junction point.
Des barres d'une grande résistance à la flexion à base de matériaux composites renforcés avec des fibres avec une paroi mince sont des matériaux idéals pour des constructions allégées, notamment dans les secteurs de l'aéronautique et de l'astronautique. Avec de telles barres, on peut fabriquer par exemple des treillis à trois dimensions avec un faible poids comme ceux décrits dans DE 42 30 857. Dans l'aéronautique et l'astronautique, on exige de telles poutres avec de grandes longueurs, par exemple des longueurs supérieures à 10 m. Des barres de cette longueur avec des diamètres de l'ordre de 20 mm ne peuvent être fabriquées en un seul bloc qu'avec de gros moyens en appareillage. Un problème est alors en particulier le durcissement dans la position rectiligne nécessaire. Des barres plus courtes avec des longueurs allant jusqu'à 6 m peuvent être fabriquées de façon avantageuse avec la haute précision exigée. De telles barres ne peuvent être utilisées avec des structures portantes de grande longueur que si elles peuvent être assemblées en barres de longueur assez grande avec de faibles écarts de rigidité. L'assemblage de barres de longueur assez courte en barres de longueur assez grande peut entraîner par exemple des avantages au niveau de la technique de fabrication même pour la fabrication Bars of high flexural strength based on fiber-reinforced composite materials with a thin wall are ideal materials for lightweight constructions, particularly in the aeronautics and astronautics sectors. With such bars, it is possible, for example, to make three-dimensional lattices with a low weight such as those described in DE 42 30 857. In aeronautics and astronautics, such beams are required with great lengths, for example lengths greater than 10 m. Bars of this length with diameters of the order of 20 mm can only be produced in a single block with large equipment. A problem then is in particular the hardening in the rectilinear position required. Shorter bars with lengths up to 6 m can be manufactured advantageously with the high precision required. Such bars can only be used with very long load-bearing structures if they can be assembled into fairly long bars with small stiffness differences. The assembly of bars of fairly short length into bars of fairly large length can, for example, lead to advantages in terms of manufacturing technique even for manufacturing
de poutres en treillis.of truss beams.
L'objectif de l'invention est un moyen pour assembler de façon simple des barres individuelles à base de matériaux composites renforcés avec des fibres avec une grande résistance à la flexion et une paroi mince en barres de grande longueur au moyen d'un raccord par manchon sans écart The object of the invention is a means for simply assembling individual bars based on fiber-reinforced composite materials with high flexural strength and a thin wall in long bars by means of a connector by sleeve without gap
important de rigidité.important stiffness.
Ce problème est résolu par un assemblage composé de deux ou plusieurs barres partielles coaxiales qui sont respectivement reliées par un manchon en les assemblant bout à bout, caractérisé en ce que on prévoit comme barres partielles des barres très résistantes à la flexion à base de matériaux composites renforcés avec des fibres, avec une paroi mince, au point de jonction, on colle comme manchon à l'extérieur un manchon de liaison à paroi mince, fendu le long d'une génératrice parallèle à l'axe, à base de matériaux composites renforcés avec des fibres, qui présente une couche intérieure à base de fibres unidirectionnelles, parallèles à l'axe et réparties à la périphérie, dont la rigidité correspond pour l'essentiel à la rigidité de la couche des fibres unidirectionnelles, transmettant les forces longitudinales, des forces partielles et qui présente à l'extérieur sur la couche intérieure à base de fibres unidirectionnelles un enroulement de fibres avec des fibres se croisant par rapport à l'axe sous un angle supérieur à 20 et à l'extérieur, sur le manchon de liaison, un tuyau en tissu de fibres à base de fibres à haute résistance est stratifié dans une matrice de résine synthétique, tuyau qui s'étend des deux côtés sur les extrémités du manchon de liaison et est stratifié dans les zones dépassant à l'extérieur sur This problem is solved by an assembly composed of two or more coaxial partial bars which are respectively connected by a sleeve by joining them end to end, characterized in that there are provided as partial bars bars very resistant to bending based on composite materials reinforced with fibers, with a thin wall, at the junction point, a bonding sleeve with a thin wall, split along a generatrix parallel to the axis, based on reinforced composite materials, is bonded to the outside with fibers, which has an inner layer based on unidirectional fibers, parallel to the axis and distributed at the periphery, the rigidity of which corresponds essentially to the rigidity of the layer of unidirectional fibers, transmitting the longitudinal forces, partial forces and which presents on the outside on the inner layer based on unidirectional fibers a winding of fiber s with fibers crossing with respect to the axis at an angle greater than 20 and on the outside, on the connecting sleeve, a hose made of high-strength fiber-based fiber fabric is laminated in a resin matrix synthetic, pipe that extends on both sides over the ends of the connecting sleeve and is laminated in the areas protruding outside on
les barres partielles.partial bars.
Des barres assemblées selon l'invention peuvent être utilisées comme barres de longeron pour les structures porteuses très étendues. Cependant, les barres peuvent être utilisées également dans des tiges de commande transmettant des forces de traction et de pression dans lesquelles ces barres sont guidées radialement par des logements appropriés et sont donc Bars assembled according to the invention can be used as spar bars for very wide load-bearing structures. However, the bars can also be used in control rods transmitting traction and pressure forces in which these bars are guided radially by suitable housings and are therefore
à l'abri de contraintes de flambage. free from buckling stress.
La réalisation de la barre en plusieurs parties rendue possible par The realization of the bar in several parts made possible by
l'assemblage peut présenter également des avantages lors du montage. assembly can also have advantages during assembly.
Avec une barre selon l'invention, les éléments de barre à raccorder peuvent être aussi par exemple des éléments de barre qui sont réalisés à une extrémité avec des éléments de raccordement. De tels éléments de barre réalisés avec des éléments de raccordement peuvent être fabriqués pratiquement en continu par exemple dans des longueurs assez courtes avec des éléments de raccordement disposés des deux côtés, comme il est décrit dans DE 41 35 695 A1. De telles longueurs de barre réalisées avec des éléments de raccordement peuvent alors être raccordées ultérieurement, par exemple également sur une structure porteuse réalisée avec les barres With a bar according to the invention, the bar elements to be connected can also be for example bar elements which are produced at one end with connecting elements. Such bar elements produced with connection elements can be produced practically continuously, for example in fairly short lengths with connection elements arranged on both sides, as described in DE 41 35 695 A1. Such bar lengths produced with connection elements can then be subsequently connected, for example also on a support structure produced with the bars.
transversales et les barres diagonales. transverse and diagonal bars.
Avec des assemblages selon l'invention, on peut également relier entre elles des sections partielles de telles structures porteuses, ce qui permet d'escompter des allégements de montage avec des structures porteuses très étirées en longueur. Ceci peut être aussi un avantage dans les cas o il With assemblies according to the invention, it is also possible to connect partial sections of such load-bearing structures to one another, which makes it possible to discount assembly reliefs with load-bearing structures very stretched in length. This can also be an advantage in cases where it
n'y a pas de problème en ce qui concerne la fabrication de barres. there is no problem when it comes to making bars.
Un avantage important réside dans le faible poids et le faible volume de An important advantage is the low weight and low volume of
l'assemblage en liaison avec une forte capacité de charge de l'assemblage. the assembly in conjunction with a high load capacity of the assembly.
L'invention est illustrée par exemple sur le dessin et décrite ci- dessous The invention is illustrated for example in the drawing and described below
dans le détail à l'aide du dessin. in detail using the drawing.
La figure 1 montre en coupe longitudinale un assemblage entre deux Figure 1 shows in longitudinal section an assembly between two
barres partielles au moyen d'un manchon de liaison extérieur. partial bars by means of an external connecting sleeve.
La figure 2 montre un manchon de liaison en vue latérale. Figure 2 shows a connecting sleeve in side view.
La figure 3 montre le manchon de liaison selon la figure 2 vu de l'avant gauche. La figure 4 montre le manchon de liaison dans un état déplié pour le montage. La barre représentée sur la figure 1 est composée de deux barres partielles 4, 6 coaxiales ou plus qui sont représentées ici sous la forme de barres à paroi mince et sont reliées assemblées bout à bout. Une liaison entre deux barres partielles coaxiales est représentée sur la figure 1. Les Figure 3 shows the connecting sleeve according to Figure 2 seen from the front left. Figure 4 shows the connecting sleeve in an unfolded state for mounting. The bar shown in Figure 1 is composed of two partial bars 4, 6 or more coaxial which are shown here in the form of thin-walled bars and are connected assembled end to end. A connection between two coaxial partial bars is shown in Figure 1. The
parois des barres partielles 4,6 sont en plastiques renforcés avec des fibres. walls of the partial bars 4,6 are made of plastic reinforced with fibers.
Comme fibre, on peut utiliser de façon connue de la fibre de verre, de la fibre de carbone ou de la fibre plastique très résistante. Elles doivent présenter au moins une couche faite de fibres unidirectionnelles qui s'étendent parallèlement à l'axe 10 de la barre et absorbent les forces de traction et de pression. Cette couche de fibres unidirectionnelles est masquée par une couche de fibres avec des fibres se croisant sous un angle par rapport à l'axe 10, de préférence avec un angle supérieur à 20 par rapport à l'axe 10. Ces deux couches de fibres, pour lesquelles on peut utiliser également des fibres différentes, sont enrobées dans une matrice de résine synthétique et forment ensemble dans une construction composite renforcée avec des fibres, le corps de barre 12 tubulaire. La paroi tubulaire repose de façon connue, dans l'exemple de réalisation représenté, sur un noyau en mousse résistant à la pression qui est réalisé de telle sorte qu'il présente une grande résistance à la déformation dans le sens transversal à As the fiber, glass fiber, carbon fiber or very strong plastic fiber can be used in known manner. They must have at least one layer made of unidirectional fibers which extend parallel to the axis 10 of the bar and absorb the tensile and pressure forces. This layer of unidirectional fibers is masked by a layer of fibers with fibers crossing at an angle relative to the axis 10, preferably with an angle greater than 20 relative to the axis 10. These two layers of fibers, for which different fibers can also be used, are coated in a matrix of synthetic resin and together form in a fiber reinforced composite construction, the tubular bar body 12. The tubular wall rests in a known manner, in the embodiment shown, on a pressure-resistant foam core which is produced in such a way that it has a high resistance to deformation in the transverse direction to
I'axe 10.Axis 10.
Les barres peuvent cependant être réalisées également sans noyau et être fabriquées par exemple selon la technique d'enroulement connue ou également sous la forme de tuyaux soumis à une pultrusion. Les fibres transmettant les forces longitudinales peuvent également être les fibres d'une gaine tressée à base de fibres qui est disposée avec une grande extension avec un angle des fibres inférieur à +/- 15 par rapport à l'axe de The bars can however also be produced without a core and be produced for example according to the known winding technique or also in the form of pipes subjected to pultrusion. The fibers transmitting the longitudinal forces can also be the fibers of a braided fiber-based sheath which is arranged with a large extension with an angle of the fibers less than +/- 15 relative to the axis of
la barre.bar.
Au point de jonction, les deux barres partielles 4 et 6 sont séparées At the junction point, the two partial bars 4 and 6 are separated
transversalement à leur axe 10. Elles peuvent se toucher par leurs faces 14. transversely to their axis 10. They can touch each other by their faces 14.
Cependant, on prévoit de préférence un espace. However, a space is preferably provided.
Pour relier les deux barres partielles 4, 6, il est prévu un manchon de liaison 16 qui entoure les deux barres partielles à l'extérieur et s'appuie dans la zone de liaison et est collé à la face externe des barres partielles à relier. La longueur du manchon de liaison est choisie de telle façon que les extrémités de la barre sont recouvertes respectivement sur une zone L égale à au moins 2D. Sur le manchon de liaison 16, on stratifie un tuyau flexible à base de tissu en fibres 18, qui est de préférence en fibres de carbone et est enrobé dans une matrice de résine synthétique. Ce tuyau dépasse des extrémités du manchon de liaison respectivement sur une longueur L. Dans cette zone, la gaine tressée en fibres 18 est stratifiée sur la face externe des barres partielles. Le manchon de liaison 16 est un élément composite renforcé avec des fibres avec une couche 20 interne à base de fibres unidirectionnelles parallèles à l'axe et une couche 22 disposée au- dessus à base d'un treillis de fibres mince, par exemple une gaine tressée en fibres à base de fibres de verre. Comme résultat de la fabrication du manchon de liaison 16, on peut fabriquer une barre avec un noyau en mousse résistant à la pression et, disposées dessus, les deux couches de fibres mentionnées dans une technique composite avec renforcement par des fibres. A partir d'une telle barre, on peut détacher alors des longueurs en fonction de la longueur exigée du manchon de liaison. En partant de ces tronçons de barre, on vide alors le noyau en mousse 8. Le manchon de forme tubulaire ainsi formé est coupé le long d'une génératrice 24 parallèle à l'axe, puis déplié d'au moins 90 , mais de préférence de 180 , comme représenté sur la figure 4. Il se brise alors dans la couche des fibres unidirectionnelles principalement en face de la coupe de séparation 24. Les deux parties restent reliées à la façon d'une charnière par la couche de tissu 22 extérieure. L'emplacement de la rupture et donc de l'assemblage à la façon d'une charnière ne pose pas de problème. Pour la cohérence des fibres unidirectionnelles, on peut prévoir également un enroulement circonférentiel To connect the two partial bars 4, 6, a connecting sleeve 16 is provided which surrounds the two partial bars on the outside and is supported in the connection zone and is glued to the external face of the partial bars to be connected. The length of the connecting sleeve is chosen so that the ends of the bar are covered respectively over an area L equal to at least 2D. On the connecting sleeve 16, a flexible hose based on fiber fabric 18 is laminated, which is preferably made of carbon fibers and is coated in a matrix of synthetic resin. This pipe protrudes from the ends of the connecting sleeve respectively over a length L. In this zone, the braided fiber sheath 18 is laminated on the external face of the partial bars. The connecting sleeve 16 is a fiber-reinforced composite element with an internal layer 20 based on unidirectional fibers parallel to the axis and a layer 22 arranged above based on a thin fiber mesh, for example a sheath braided in fibers based on glass fibers. As a result of the manufacture of the connecting sleeve 16, it is possible to manufacture a bar with a core of pressure-resistant foam and, arranged thereon, the two layers of fibers mentioned in a composite technique with fiber reinforcement. From such a bar, one can then detach lengths depending on the required length of the connecting sleeve. Starting from these bar sections, the foam core 8 is then emptied. The tubular sleeve thus formed is cut along a generatrix 24 parallel to the axis, then unfolded by at least 90, but preferably of 180, as shown in FIG. 4. It then breaks in the layer of unidirectional fibers mainly in front of the separation cut 24. The two parts remain connected in the manner of a hinge by the outer layer of fabric 22. The location of the break and therefore of the assembly in the manner of a hinge poses no problem. For the consistency of the unidirectional fibers, a circumferential winding can also be provided
au lieu d'un tuyau en tissu.instead of a fabric pipe.
Après l'application de la colle sur la face externe des deux barres partielles 4, 6 et/ou la face interne du manchon de liaison 16, le manchon de liaison déplié peut être posé sur les barres partielles et recourbé à nouveau pour avoir la forme tubulaire initiale. Par un dimensionnement approprié du diamètre intérieur du manchon de liaison, on peut respecter alors une épaisseur de colle souhaitée. Le manchon de liaison 16 est réalisé de telle façon que la solidité des fibres unidirectionnelles de la couche de fibres 20 corresponde pour l'essentiel à la résistance longitudinale des deux After the adhesive has been applied to the external face of the two partial bars 4, 6 and / or the internal face of the connecting sleeve 16, the unfolded connecting sleeve can be placed on the partial bars and bent again to have the shape initial tubular. By an appropriate dimensioning of the internal diameter of the connecting sleeve, one can then respect a desired adhesive thickness. The connecting sleeve 16 is produced in such a way that the solidity of the unidirectional fibers of the layer of fibers 20 corresponds essentially to the longitudinal resistance of the two
barres partielles 4, 6.partial bars 4, 6.
Par le manchon de liaison 16, on fait coulisser un tronçon de tuyau en tissu 18 enfilé auparavant sur l'une des barres partielles 4, 6, à base de fibres à haute résistance, de préférence des fibres de carbone, et on le stratifie sur la face externe du manchon de liaison 16 et les zones L' Through the connecting sleeve 16, a section of fabric pipe 18 is slid previously slid over one of the partial bars 4, 6, based on high-strength fibers, preferably carbon fibers, and it is laminated on the external face of the connecting sleeve 16 and the zones L '
limitrophes des deux barres partielles 4, 6. bordering on the two partial bars 4, 6.
Le tuyau stratifié en tissu de fibres atténue les écarts de rigidité sur les The laminated fiber fabric pipe reduces the stiffness differences on the
deux extrémités du manchon de liaison. two ends of the connecting sleeve.
Des manchons de liaison comme ceux représentés sur les figures 2 à 4 peuvent être utilisés également pour la réparation en cas de dégâts matériels sur les barres en appliquant un manchon de liaison de longueur appropriée sur les tronçons endommagés. Dans le cas d'une réparation, on peut enlever également un tronçon très endommagé d'une barre et insérer alors une barre appropriée dans la barre endommagée au moyen de deux manchons de liaison. Dans le cas présent, on peut également insérer et Connecting sleeves like those shown in Figures 2 to 4 can also be used for repair in the event of material damage to the bars by applying a connecting sleeve of appropriate length to the damaged sections. In the case of a repair, a severely damaged section of a bar can also be removed and a suitable bar can then be inserted into the damaged bar by means of two connecting sleeves. In this case, you can also insert and
stratifier des tronçons appropriés de tuyau en tissu. laminate appropriate sections of fabric pipe.
Bien entendu, I'invention n'est pas limitée aux exemples de réalisation ci-dessus décrits et représentés, à partir desquels on pourra prévoir d'autres modes et d'autres formes de réalisation, sans pour autant sortir du cadre de l'invention. Of course, the invention is not limited to the examples of embodiment described and shown above, from which other modes and other embodiments can be provided, without going beyond the ambit of the invention. .
Claims (3)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4419691A DE4419691C1 (en) | 1994-06-04 | 1994-06-04 | Straight FRP bar for longitudinal load transmission |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2720795A1 true FR2720795A1 (en) | 1995-12-08 |
FR2720795B1 FR2720795B1 (en) | 1997-03-14 |
Family
ID=6519881
Family Applications (1)
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---|---|---|---|
FR9506450A Expired - Fee Related FR2720795B1 (en) | 1994-06-04 | 1995-05-31 | Straight bars for transmitting longitudinal forces based on reinforced composite materials. |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE4419691C1 (en) |
FR (1) | FR2720795B1 (en) |
GB (1) | GB2289928B (en) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
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US5915503A (en) * | 1995-11-16 | 1999-06-29 | The B.F. Goodrich Company | Brake rod having a bending mode coulomb damper |
EP0774595B1 (en) * | 1995-11-16 | 2002-05-08 | The B.F. Goodrich Company | Nested damping device with relative motion |
DE19645467A1 (en) * | 1996-11-05 | 1998-05-14 | Deutsch Zentr Luft & Raumfahrt | Force application device |
DE19703856A1 (en) * | 1997-02-03 | 1998-08-06 | Estebanez Eva Garcia | Joint filling method for forming steel joints in heavy machines, e.g. cranes |
DE19723112C1 (en) * | 1997-06-03 | 1999-06-02 | Ulrich Dipl Ing Rueger | Connection element for a glued connection between two or more bars |
DE19800911A1 (en) * | 1998-01-14 | 1999-07-22 | Deutsch Zentr Luft & Raumfahrt | Process for producing a heavy-duty rod and the rod produced by the method |
DE19958375C2 (en) * | 1999-12-06 | 2003-04-03 | Deutsch Zentr Luft & Raumfahrt | Force transmission device and method for connecting incompatible materials |
US6585298B2 (en) * | 2001-11-13 | 2003-07-01 | Flowtite Technology As | High-strength butt-wrap joint for reinforced plastic pipes |
DE202004002838U1 (en) * | 2004-02-20 | 2005-04-07 | Hans Riedmayer E K | Clip for preventing tensile rod or push rod from rotating, comprises forked head secured to clip part and to plastic insert for rod |
DE202008008653U1 (en) | 2008-06-24 | 2009-04-09 | First Composites Gmbh | Plastic multiprofile, in particular with a core |
US20100132880A1 (en) * | 2008-12-01 | 2010-06-03 | Kevin Patrick Kelleher | Composite honeycomb sandwich panel splicing |
CN101565989B (en) * | 2009-05-15 | 2011-04-06 | 同济大学 | Method for coaxially connecting FRP reinforcements by FRP connecting pipe and expansive cement |
DE102010001479A1 (en) * | 2010-02-02 | 2011-08-04 | Rieter Ingolstadt GmbH, 85055 | Thread guide rod for cross-wound bobbin manufactured textile machine, particularly open end spinning machine, has multiple tubular rod parts which are connected axially with each other by coupling elements |
GB2478768B (en) * | 2010-03-18 | 2013-01-30 | Marathon Belting Ltd | A fibrous structure and a method of manufacturing same |
FR2957844B1 (en) * | 2010-03-26 | 2012-05-18 | Messier Dowty Sa | METHOD FOR MANUFACTURING A MECHANICAL MEMBER IN COMPOSITE MATERIAL HAVING INCREASED MECHANICAL TENSION-COMPRESSION AND BENDING |
DE102011005329A1 (en) * | 2011-03-10 | 2012-09-13 | Sgl Carbon Se | Method and device for producing a fiber-reinforced composite material and in particular a tension member |
FR3006725B1 (en) * | 2013-06-05 | 2015-06-19 | Hutchinson | COMPOSITE ROD, ITS MANUFACTURING METHOD, AND AERONAUTICAL CEILING OR FLOOR STRUCTURE INCORPORATING IT. |
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DE2326628A1 (en) * | 1972-05-22 | 1973-12-06 | Lockheed Aircraft Corp | COUPLING MADE OF GLUED SLEEVES FOR TUBES AND TUBE-SHAPED LINKS |
DE3818066A1 (en) * | 1988-05-27 | 1989-12-07 | Sigri Gmbh | ADHESIVE CONNECTION OF CARBON OR GRAPHITE TUBES |
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DE2911330C2 (en) * | 1979-03-22 | 1984-03-22 | Siemens Ag, 1000 Berlin Und 8000 Muenchen | Connector for assembling hollow tubular frame racks |
DE3447990C2 (en) * | 1983-01-05 | 1990-06-28 | Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt Ev, 5300 Bonn, De | Connecting element |
DE3603712A1 (en) * | 1986-02-06 | 1987-08-13 | Ambros Stanelle | PIPE COUPLING |
DE4135695C2 (en) * | 1991-10-25 | 1993-10-28 | Deutsche Forsch Luft Raumfahrt | Rod with a tubular wall made of fiber composite material and connection element arranged on both sides |
DE4205834C1 (en) * | 1992-02-26 | 1993-06-03 | Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt E.V., 5300 Bonn, De | Framework of thin walled round fibre compound rods - has fibre compound joint plates connecting cross and diagonal bars to upright bars |
DE4330857C2 (en) * | 1992-09-17 | 1995-01-26 | Deutsche Forsch Luft Raumfahrt | Composite element with carbon fibers |
-
1994
- 1994-06-04 DE DE4419691A patent/DE4419691C1/en not_active Expired - Fee Related
-
1995
- 1995-05-04 GB GB9509053A patent/GB2289928B/en not_active Expired - Fee Related
- 1995-05-31 FR FR9506450A patent/FR2720795B1/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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DE2326628A1 (en) * | 1972-05-22 | 1973-12-06 | Lockheed Aircraft Corp | COUPLING MADE OF GLUED SLEEVES FOR TUBES AND TUBE-SHAPED LINKS |
DE3818066A1 (en) * | 1988-05-27 | 1989-12-07 | Sigri Gmbh | ADHESIVE CONNECTION OF CARBON OR GRAPHITE TUBES |
Also Published As
Publication number | Publication date |
---|---|
DE4419691C1 (en) | 1995-08-24 |
GB9509053D0 (en) | 1995-06-28 |
GB2289928B (en) | 1998-06-24 |
GB2289928A (en) | 1995-12-06 |
FR2720795B1 (en) | 1997-03-14 |
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