AU3037497A - Composite material tubular equipment produced by winding of weft-unbalanced wov en fabric on a compressible mandrel - Google Patents

Composite material tubular equipment produced by winding of weft-unbalanced wov en fabric on a compressible mandrel Download PDF

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Publication number
AU3037497A
AU3037497A AU30374/97A AU3037497A AU3037497A AU 3037497 A AU3037497 A AU 3037497A AU 30374/97 A AU30374/97 A AU 30374/97A AU 3037497 A AU3037497 A AU 3037497A AU 3037497 A AU3037497 A AU 3037497A
Authority
AU
Australia
Prior art keywords
tube according
winding
fabric
tube
unbalanced
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU30374/97A
Inventor
Bernard Castagner
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of AU3037497A publication Critical patent/AU3037497A/en
Abandoned legal-status Critical Current

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Classifications

    • 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
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56Winding and joining, e.g. winding spirally
    • B29C53/58Winding and joining, e.g. winding spirally helically
    • B29C53/60Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56Winding and joining, e.g. winding spirally
    • B29C53/58Winding and joining, e.g. winding spirally helically
    • B29C53/581Winding and joining, e.g. winding spirally helically using sheets or strips consisting principally of plastics material
    • B29C53/582Winding and joining, e.g. winding spirally helically using sheets or strips consisting principally of plastics material comprising reinforcements, e.g. wires, threads
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/80Component parts, details or accessories; Auxiliary operations
    • B29C53/82Cores or mandrels
    • B29C53/821Mandrels especially adapted for winding and 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
    • B29C63/00Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • 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
    • B29K2105/0845Woven fabrics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2023/00Tubular articles
    • B29L2023/22Tubes or pipes, i.e. rigid

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Laminated Bodies (AREA)
  • Woven Fabrics (AREA)
  • Nonwoven Fabrics (AREA)
  • Storage Of Web-Like Or Filamentary Materials (AREA)
  • Moulding By Coating Moulds (AREA)

Description

1 TUBULAR ELEMENTS IN COMPOSITE MATERIALS OBTAINED BY WINDING AN UNBALANCED-WEAVE FABRIC ON A COMPRESSIBLE MANDREL 5 Numerous structural elements, in particular piles, posts or masts, are made from steel and, as a consequence, suffer from disadvantages such as: a) their significant weight and, in certain cases, the resultant problems in placing them; 10 b) their tendency to corrode due to the effects of air, water or the soil. c) the cost of their maintenance. In an attempt to overcome these disadvantages, such structural elements have been made from aluminium or 15 composite materials. Regarding such structural elements in composite materials, the technique that is generally employed consists in winding filaments of rovings. Structural elements such as piles, posts or masts should not only have good breaking strength characteristics but also 20 be highly rigid when subject to movements which tend to bend them. To achieve this, it is necessarily for the composite structure to take full advantage, firstly, of the tensile breaking and compressional strength of the fibers and, secondly, of the flexural modulus of the reinforcing fibers. 25 Thus, the major portion of the latter should be placed along the axis of the pile, post or mast. According to the invention, elongated structures such as piles, posts, masts, beams, are produced by winding, preferably helically, thermosetting-resin-impregnated glass 30 fabric impregnated with a a heat-setting resin such as an epoxy, polyester, or vinyl ester resin. According to the invention, these fabrics have an unbalanced weave, in other words have a higher percentage of filaments in the fill or woof than in the warp. Additionally, 35 their weave makes angular deformability possible thereby 4600\14606US.DOC - 13 novembre 1998- in/ 2 making it possible, according to the invention, to place the fill or woof filaments parallel to the X- X' axis of the structure. The originality of the design of these high bending 5 strength composite tubes of the invention will become clear from the description and corresponding technical justification. According to the invention, a tube is produced by helically winding a glass fabric in which the ratio warp/woof 10 is unbalanced, with c>t, where c is the percentage of the fiber placed in the warp and t is the percentage of fiber placed in the woof. The preferred values are between 10 and 25% for c and between 90 and 75% for t; this figure for modularity makes it possible, as a function of 15 diameter/thickness ratio, to ensure good resistance against radial buckling. According to the invention, the tube is built up from successive layers provided by forward and return helical winding. On the forward runs, helical winding is done at an 20 angle of B1 = (90 0 - ) with respect to the longitudinal axis and on the return run with an angle of B2 = (900 + a). According to the invention, helical winding is preferably carried out while giving the fabric an oblique slope of angle a (see FIG 1) so that the fill or woof 1 is parallel to the 25 longitudinal axis of the tube, the warp 2 having an angle a with respect to the circumferential plane 3; this arrangement improves flexural modulus. According to the invention, each layer is wound preferably by partially overlapping (see 6) successive turns 30 4, 5 (see FIG 2) . To avoid local excess thickness the width of offset 1 between two successive turns is such that L 35 n 4600\14606US.DOC - 13 novembre 1998 -2/7 3 where L is the width of the layer and n is an integer > 1. Without departing from the invention, helically winding is performed either with individual widths abuting as 5 indicated by reference 7 in FIG 3, or with alternating individual widths (see FIG 4). The individual widths 8 and 9 are placed during the first outward run. The individual widths 10 and 11 are placed during the first return run; the widths 12 and 13 during the second outward run. This latter 10 type of winding improves resistance to inter-layer shear stress. According to the invention, where winding is done with the turns abuting, the successive layers are preferably offset in order to decrease the effect of discontinuity 15 brought about by the individual widths. For example, in the case of a helical winding with abuting individual widths of width L and a number of layers q, the position of each layer (outward + return run) is offset by a space of width K such that 20 L K = m 25 where m is an integer > 1 and if possible with q m = r 30 r being an integer (see FIG 5). The individual widths 14 ,15, 16 are the widths for the first outward run and the individual widths 17,18 and 19 are the widths for the second outward run. 35 Even though the preferred fabric is a glass fabric it is possible, without a departing from the scope of the invention, to employ fabrics in carbon, aramide, or high 4600\14606US.DOC - 13 novembre 1998 - 3/7 4 strength polyethylene. It is also possible to employ hybrid fabrics, for example glass plus carbon. Without departing from the invention, the fabrics can be pre-impregnated with heat-setting resin. 5 Without departing from the invention, the fabrics employed can be pre-impregnated with thermoplastic resin. Without departing from the invention, the fabrics can be wound at the same time as a thermoplastic film and impregnated by melting plus compression. 10 Where it is desired to produce structural elements such as piles, posts or masts which are of considerable thickness, including cylindrical portions and having an unbalanced fiber reinforcement along the X-X' axis of the structural element, the presence of significant forces tending to clamp the 15 composite structure against the mandrel, after polymerization, has been observed; this phenomenon can make it difficult to remove the element from the mandrel and can create micro-cracking in the structure. In order to avoid these major disadvantages, according to 20 the invention, a smooth layer of a compressible material is placed on the mandrel after which the glass fabric is wound onto this compressible mandrel. According to the invention, the characteristics of compressability of the material will be such that it only 25 shows a slight deformability under the limited force of winding the fabric and it will absorb the contraction of the composite structure and only transmit a slight clamping force to the mandrel, thereby facilitating removal therefrom. The material chosen should have a low coefficient of friction. 30 According to the invention, the material is preferably a closed-cell polyethylene foam with a smooth polished skin. Without departing from the invention, another material having the above characteristics can be used, for example a flexible polyurethane foam. 4600\14606US.DOC - 13 novembre 1998 -4/7 5 According to the invention, in order to facilitate removal from the mandrel and preserve the internal surface state of the tube, the foam should be coated with a terpane film. 5 In the presence of flexural forces operating in a priviledged radial direction, oblong-shaped tubes are provided (see FIG 6) . This type of tube can for example be employed in the construction of breakwaters. Without departing from the invention, the tube can have a 10 sandwich structure (see FIG 7) constituted by two concentric tubes 20, 21 obtained by means of the invention and separated .: by a wall 22 in a material which is rigid in compression such as a rigid foam, a honeycomb structure, balsa, and so on. *** This makes it possible to make the tubes lighter and improves .15 rigidity. -0 Without departing from the invention, in order to improve 00 rigidity in the presence of bending forces acting along a preferred axis, the inner tube can be cylindrical and the outer tube oblong. 0 0 0O *0 0 S 0e 0 :0 4600\14606US.DOC - 13 novembre 1998 -5/7

Claims (7)

1.- A tube in a composite material characterised in that it is obtained by helically winding fabric in which the fill 5 or woof is unbalanced with respect to the warp
2.- The tube according to claim 1, characterised in that it is provided by inclining the fabric by an angle equal to the angle of helical winding. 10
3. - The tube according to one or several of claims 1 and .... 2, characterised in that the helical winding of the tube is performed with partial overlapping of successive turns. .15 4.- The tube according to one or several of claims 1 and 2, characterised in that individual widths are butt-jointed or alternate and successive layers thereof are offset in order to counterbalance discontinuities due to the individual widths. 20 **. 5.- The tube according to any one of the preceding claims, characterised in that the fabric employed is composed of fibers of a single type or of hybrid fibers. :25 6. - The tube according to any one of the preceding claims, characterised in that its profile is cylindrical or * 0 oblong. 0
7.- The tube according to any one of the preceding 30 claims, characterised in that it has a single-walled structure.
8.- The tube according to any one of the preceding claims, characterised in that it has a sandwich structure 4600\14606US.DOC - 13 november 1998 -6/7 7 that includes a material having high compression strength between two tubes.
9. - The tube according to any one of the above claims, 5 characterised in that its winding mandrel is covered with a layer of compressible material.
10. The tube according to claim 9, characterised in that the compressible material is a closed cell polyethylene foam. *. 0\ 14 0166S O 3n~ m19 -/
AU30374/97A 1996-05-23 1997-05-23 Composite material tubular equipment produced by winding of weft-unbalanced wov en fabric on a compressible mandrel Abandoned AU3037497A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9606537A FR2748964B1 (en) 1996-05-23 1996-05-23 TUBULAR EQUIPMENT IN COMPOSITE MATERIALS MADE BY WINDING UNBALANCED TISSUE ON A COMPRESSIBLE CHUCK
FR9606537 1996-05-23
PCT/FR1997/000909 WO1997044181A1 (en) 1996-05-23 1997-05-23 Composite material tubular equipment produced by winding of weft-unbalanced woven fabric on a compressible mandrel

Publications (1)

Publication Number Publication Date
AU3037497A true AU3037497A (en) 1997-12-09

Family

ID=9492471

Family Applications (1)

Application Number Title Priority Date Filing Date
AU30374/97A Abandoned AU3037497A (en) 1996-05-23 1997-05-23 Composite material tubular equipment produced by winding of weft-unbalanced wov en fabric on a compressible mandrel

Country Status (12)

Country Link
EP (1) EP0907494A1 (en)
JP (1) JP2000510779A (en)
KR (1) KR20000015809A (en)
CN (1) CN1219903A (en)
AU (1) AU3037497A (en)
BR (1) BR9709357A (en)
CA (1) CA2255860A1 (en)
FR (1) FR2748964B1 (en)
NO (1) NO985411L (en)
PL (1) PL330186A1 (en)
TR (1) TR199802381T2 (en)
WO (1) WO1997044181A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101103448B1 (en) * 2009-07-01 2012-01-09 경희대학교 산학협력단 Lane departure warning apparatus using laser
JP2011098523A (en) * 2009-11-06 2011-05-19 Ihi Corp Method of manufacturing case and the case
RU2445523C1 (en) * 2010-09-28 2012-03-20 Государственное образовательное учреждение высшего профессионального образования "Тихоокеанский государственный университет" Method of producing plain bearing
RU2445521C1 (en) * 2010-10-05 2012-03-20 Государственное образовательное учреждение высшего профессионального образования "Тихоокеанский государственный университет" Method of producing plain bearing
RU2445522C1 (en) * 2010-11-26 2012-03-20 Государственное образовательное учреждение высшего профессионального образования "Тихоокеанский государственный университет" Method of producing plain bearing
RU2485367C1 (en) * 2012-03-26 2013-06-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Тихоокеанский государственный университет" Manufacturing method of sliding bearing
JP6567530B2 (en) * 2013-09-11 2019-08-28 タタ、スティール、ユーケー、リミテッドTata Steel Uk Limited Tubular storage part for flywheel storage assembly and method for manufacturing the same
RU2540894C1 (en) * 2013-11-28 2015-02-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Тихоокеанский государственный университет" Sliding bearing manufacturing method
DE102017009839A1 (en) * 2017-07-12 2019-01-17 Oke Kunststofftechnik Gmbh & Co. Kg Method for producing a composite profile and composite profile
CN110815873A (en) * 2019-11-15 2020-02-21 核工业理化工程研究院 Method and device for treating surface of composite material cylinder
CN113232328B (en) * 2021-03-31 2022-05-06 成都飞机工业(集团)有限责任公司 Manufacturing method of composite material S-shaped air inlet duct cylinder based on 2.5D weaving

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3141052A (en) * 1960-09-19 1964-07-14 Jr Peter Labash Method of forming seamless hollow plastic shapes
DE1704632A1 (en) * 1967-02-24 1971-05-19 Bayer Ag Winding mandrel and process for the production of pipes made of glass fiber reinforced thermosetting plastics
DE2423223C3 (en) * 1974-05-14 1978-11-02 Troisdorfer Bau- Und Kunststoff Gmbh, 5210 Troisdorf Heatable winding drum made of steel for the manufacture of pipes and containers
US3969557A (en) * 1975-02-27 1976-07-13 Amf Incorporated Fiberglass vaulting pole
US3989562A (en) * 1975-03-10 1976-11-02 Pikaz, Inzenyrsky Podnik Container body
US4273601A (en) * 1977-10-31 1981-06-16 Structural Composites Industries, Inc. Method for the production of elongated resin impregnated filament composite structures
DE3929473A1 (en) * 1989-09-05 1991-03-07 Ch Polt I Angular winding of resin impregnated glass fabric - in which applicator trolley with roll of fabric moves sideways relative to rotating mandrel and has resin bath and fabric guides

Also Published As

Publication number Publication date
CA2255860A1 (en) 1997-11-27
PL330186A1 (en) 1999-04-26
CN1219903A (en) 1999-06-16
FR2748964B1 (en) 1998-08-07
FR2748964A1 (en) 1997-11-28
WO1997044181A1 (en) 1997-11-27
JP2000510779A (en) 2000-08-22
TR199802381T2 (en) 1999-06-21
BR9709357A (en) 1999-08-10
KR20000015809A (en) 2000-03-15
EP0907494A1 (en) 1999-04-14
NO985411L (en) 1998-11-23
NO985411D0 (en) 1998-11-20

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