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 PDF

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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
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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
Application number
FR9506450A
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French (fr)
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FR2720795B1 (en
Inventor
Rainer Schutze
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Deutsches Zentrum fuer Luft und Raumfahrt eV
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Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C7/00Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
    • F16C7/02Constructions of connecting-rods with constant length
    • F16C7/026Constructions of connecting-rods with constant length made of fibre reinforced resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/50Joining 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
    • B29C65/5007Joining 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
    • B29C65/5028Joining 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/50Joining 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
    • B29C65/5042Joining 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint 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
    • B29C66/112Single lapped joints
    • B29C66/1122Single lap to lap joints, i.e. overlap joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint 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
    • B29C66/114Single butt joints
    • B29C66/1142Single butt to butt joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/52Joining tubular articles, bars or profiled elements
    • B29C66/522Joining tubular articles
    • B29C66/5221Joining tubular articles for forming coaxial connections, i.e. the tubular articles to be joined forming a zero angle relative to each other
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/52Joining tubular articles, bars or profiled elements
    • B29C66/522Joining tubular articles
    • B29C66/5229Joining tubular articles involving the use of a socket
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/52Joining tubular articles, bars or profiled elements
    • B29C66/526Joining bars
    • B29C66/5261Joining bars for forming coaxial connections, i.e. the bars to be joined forming a zero angle relative to each other
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/63Internally supporting the article during joining
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22Fibrous 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
    • B29C70/228Fibrous 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B7/00Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00Shaping techniques involving a cutting or machining operation
    • B29C2793/009Shaping techniques involving a cutting or machining operation after shaping
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/50Joining 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
    • B29C65/5007Joining 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
    • B29C65/5021Joining 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • B29C66/7212Fibre-reinforced materials characterised by the composition of the fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, 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
    • B29K2105/0809Fabrics
    • B29K2105/0827Braided fabrics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, 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
    • B29K2105/10Cords, strands or rovings, e.g. oriented cords, strands or rovings
    • B29K2105/101Oriented
    • B29K2105/108Oriented arranged in parallel planes and crossing at substantial angles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00Use of elements other than metals as reinforcement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2309/00Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
    • B29K2309/08Glass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/06Rods, e.g. connecting rods, rails, stakes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight 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)

REVENDICATIONS 1. Barre droite transmettant des forces longitudinales composée 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 (4,6;4',6') des barres très résistantes à la flexion à base de matériaux composites renforcés avec des fibres, avec une paroi mince, l0 au point de jonction, on colle comme manchon à l'extérieur un manchon de liaison (16) à paroi mince, fendu le long d'une génératrice (14) parallèle à l'axe, à base de matériaux composites renforcés avec des fibres, qui présente une couche (20) intérieure à base de fibres unidirectionnelles, parallèles à l'axe et réparties à la périphérie, dont la rigidité correspond pour I'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 (10) sous un angle supérieur à 20 et à l'extérieur, sur le manchon de liaison (16), un tuyau en tissu de fibres (18) 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 (16) et est stratifié dans les zones dépassant à  1. Straight bar transmitting longitudinal forces composed of two or more coaxial partial bars which are respectively connected by a sleeve by joining them end to end, characterized in that partial bars are provided (4,6; 4 ', 6') bars very resistant to bending on the basis of composite materials reinforced with fibers, with a thin wall, 10 at the junction point, a bonding sleeve (16) with a thin wall, split along a generator (14) parallel to the axis, based on fiber-reinforced composite materials, which has an inner layer (20) based on unidirectional fibers, parallel to the axis and distributed at the periphery, the rigidity 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 fibers unidirectional a winding of fibers with fibers crossing with respect to the axis (10) at an angle greater than 20 and outside, on the connecting sleeve (16), a fiber fabric pipe (18) to high strength fiber base is laminated in a synthetic resin matrix, pipe which extends on both sides over the ends of the connecting sleeve (16) and is laminated in the areas beyond l'extérieur sur les barres partielles.  the outside on the partial bars. 2. Barre selon la revendication 1 ou 2, caractérisée en ce que le manchon de liaison (16) présente une longueur égale à au moins 4D des  2. Bar according to claim 1 or 2, characterized in that the connecting sleeve (16) has a length equal to at least 4D of barres partielles.partial bars. 3. Procédé pour la fabrication d'un manchon de liaison pour barres selon la revendication 1, caractérisé en ce que, en partant d'une barre munie d'un noyau en mousse résistant à la pression avec un diamètre correspondant au diamètre extérieur des barres partielles (4,6) à relier et d'une paroi mince reposant dessus faite dans un matériau composite renforcé avec des fibres avec une couche, reposant sur le noyau en mousse, de fibres unidirectionnelles parallèles à l'axe et une couche extérieure avec des fibres se croisant sous un angle supérieur à 20 par rapport à l'axe de la barre, on enlève le noyau en mousse, on coupe la paroi du manchon ainsi constitué le long d'une génératrice parallèle à l'axe et on déplie le manchon de façon que la couche de fibres (20) unidirectionnelle se casse dans la zone située en face de la séparation (24) parallèlement aux  3. Method for manufacturing a connecting sleeve for bars according to claim 1, characterized in that, starting from a bar provided with a core of pressure-resistant foam with a diameter corresponding to the outside diameter of the bars partial (4,6) to be connected and a thin wall resting thereon made of a fiber-reinforced composite material with a layer, resting on the foam core, of unidirectional fibers parallel to the axis and an outer layer with fibers crossing at an angle greater than 20 relative to the axis of the bar, removing the foam core, cutting the wall of the sleeve thus formed along a generatrix parallel to the axis and unfolding the sleeve so that the unidirectional fiber layer (20) breaks in the area opposite the partition (24) parallel to the fibres unidirectionnelles.unidirectional fibers.
FR9506450A 1994-06-04 1995-05-31 Straight bars for transmitting longitudinal forces based on reinforced composite materials. Expired - Fee Related FR2720795B1 (en)

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DE4419691A DE4419691C1 (en) 1994-06-04 1994-06-04 Straight FRP bar for longitudinal load transmission

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FR2720795B1 FR2720795B1 (en) 1997-03-14

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Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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.

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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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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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