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GB2010446A - Composite Tubular Element - Google Patents

Composite Tubular Element

Info

Publication number
GB2010446A
GB2010446A GB7846904A GB7846904A GB2010446A GB 2010446 A GB2010446 A GB 2010446A GB 7846904 A GB7846904 A GB 7846904A GB 7846904 A GB7846904 A GB 7846904A GB 2010446 A GB2010446 A GB 2010446A
Authority
GB
United Kingdom
Prior art keywords
fibers
core
layers
layer
give
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
GB7846904A
Other versions
GB2010446B (en
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.)
ExxonMobil Technology and Engineering Co
Original Assignee
Exxon Research and Engineering Co
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
Priority claimed from US05/856,615 external-priority patent/US4131701A/en
Application filed by Exxon Research and Engineering Co filed Critical Exxon Research and Engineering Co
Publication of GB2010446A publication Critical patent/GB2010446A/en
Application granted granted Critical
Publication of GB2010446B publication Critical patent/GB2010446B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00—Layered products having a non-planar shape
    • B32B1/08—Tubular products
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/02—Layered products essentially comprising sheet glass, or glass, slag, or like fibres in the form of fibres or filaments
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
    • B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
    • 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
    • F16C3/00—Shafts; Axles; Cranks; Eccentrics
    • F16C3/02—Shafts; Axles
    • F16C3/023—Shafts; Axles made of several parts, e.g. by welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • B32B2260/023—Two or more layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/101—Glass fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/10—Fibres of continuous length
    • B32B2305/18—Fabrics, textiles
    • B32B2305/188—Woven fabrics
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2311/00—Metals, their alloys or their compounds
    • B32B2311/24—Aluminium
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2313/00—Elements other than metals
    • B32B2313/04—Carbon
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2315/00—Other materials containing non-metallic inorganic compounds not provided for in groups B32B2311/00 - B32B2313/04
    • B32B2315/08—Glass
    • B32B2315/085—Glass fiber cloth or fabric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2597/00—Tubular articles, e.g. hoses, pipes
    • 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
    • F16C3/00—Shafts; Axles; Cranks; Eccentrics
    • F16C3/02—Shafts; Axles
    • F16C3/026—Shafts made of fibre reinforced resin

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Textile Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Laminated Bodies (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

Conventional structures for use as, for example, drive shafts or rotors are generally of solid metal. A lighter weight structure, having at least equal transmission properties, could give better fuel efficiency. One tubular structure of the invention is constructed from a metal tube 25; an adhesive 19; layers 26 and 28 of resin-impregnated carbon, or graphite, fibers; and interposed layers 27 and 24 of woven fiberglass. The fibers 22 of layer 26 are at an angle of from 5 DEG to 20 DEG with respect to the axis of core 25. The fibers 20 of layer 28 are at the corresponding angle, but of opposite hand orientation. The layers are shaped such that when wrapped around the core 25 the thickness of the total wrap increases from each end of the core to a maximum in its central portion. The wrapped article is heat cured to give the final composite structure. <IMAGE>
GB7846904A 1977-12-02 1978-12-01 Composite tubular element and methods for making same Expired GB2010446B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/856,615 US4131701A (en) 1977-05-27 1977-12-02 Composite tubular elements

Publications (2)

Publication Number Publication Date
GB2010446A true GB2010446A (en) 1979-06-27
GB2010446B GB2010446B (en) 1982-02-17

Family

ID=25324081

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7846904A Expired GB2010446B (en) 1977-12-02 1978-12-01 Composite tubular element and methods for making same

Country Status (6)

Country Link
JP (1) JPS5479337A (en)
CA (1) CA1098329A (en)
DE (1) DE2852033A1 (en)
FR (1) FR2410758A1 (en)
GB (1) GB2010446B (en)
IT (1) IT1100449B (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0040492A2 (en) * 1980-05-21 1981-11-25 Mitsubishi Rayon Co., Ltd. Moulding material for fibre reinforced plastic tubes
DE3108318A1 (en) * 1980-06-26 1982-01-21 Avco Corp., 06830 Greenwich, Conn. CONSTRUCTION OF A DRIVE SHAFT FROM A METAL COMPOSITE BODY AND METHOD FOR PRODUCING THE SAME
FR2516859A3 (en) * 1981-11-26 1983-05-27 Lerc Lab Etudes Rech Chim Double-tapered fibre reinforced plastics mast - thickest at point of greatest stress, used for wind surf board
GB2138921A (en) * 1983-04-16 1984-10-31 Brd Co Ltd Shafts
FR2600013A1 (en) * 1986-06-11 1987-12-18 Volkswagen Ag TORSION ELEMENT, CONSISTING OF OVERLAPPED FIBER STRATES
WO1999062704A1 (en) * 1998-06-05 1999-12-09 Exxon Research And Engineering Company Composite pipe structures having improved containment and axial strength
US6581644B1 (en) 1997-04-04 2003-06-24 Exxonmobil Research And Engineering Company Composite pipe structure having improved containment and axial strength
DE102007036436A1 (en) * 2007-08-02 2009-02-05 Benteler Automobiltechnik Gmbh hybrid wave

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4272971A (en) * 1979-02-26 1981-06-16 Rockwell International Corporation Reinforced tubular structure
CA1154042A (en) * 1979-07-12 1983-09-20 Frank H. Doyal Fiber-reinforced tubular spring
SE424218B (en) * 1980-10-31 1982-07-05 Fiber Mech TRANSMISSION SYSTEM
DE3341077C2 (en) * 1983-11-12 1996-11-14 Volkswagen Ag Cardan shaft, in particular drive shaft for wheels of a motor vehicle
DE3822417A1 (en) * 1987-07-15 1989-01-26 Man Technologie Gmbh Shaft for transmitting torsional forces
DE3943535C2 (en) * 1989-06-24 1994-11-24 Gkn Automotive Ag Connection arrangement
DE19806827A1 (en) * 1998-02-18 1999-08-19 Trw Automotive Electron & Comp Connection between a support and a plate element
DE102014200351B4 (en) 2014-01-10 2018-09-06 Magna Exteriors Gmbh Method for producing tubular components from fiber composite materials
US20200309186A1 (en) 2019-03-29 2020-10-01 Goodrich Corporation Hybrid composite drive shaft and a method of making

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3651661A (en) * 1970-02-02 1972-03-28 United Aircraft Corp Composite shaft with integral end flange
US3969557A (en) * 1975-02-27 1976-07-13 Amf Incorporated Fiberglass vaulting pole
US4089190A (en) * 1976-04-14 1978-05-16 Union Carbide Corporation Carbon fiber drive shaft

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0040492A2 (en) * 1980-05-21 1981-11-25 Mitsubishi Rayon Co., Ltd. Moulding material for fibre reinforced plastic tubes
EP0040492A3 (en) * 1980-05-21 1984-07-11 Mitsubishi Rayon Co., Ltd. Moulding material for fibre reinforced plastic tubes
DE3108318A1 (en) * 1980-06-26 1982-01-21 Avco Corp., 06830 Greenwich, Conn. CONSTRUCTION OF A DRIVE SHAFT FROM A METAL COMPOSITE BODY AND METHOD FOR PRODUCING THE SAME
FR2516859A3 (en) * 1981-11-26 1983-05-27 Lerc Lab Etudes Rech Chim Double-tapered fibre reinforced plastics mast - thickest at point of greatest stress, used for wind surf board
GB2138921A (en) * 1983-04-16 1984-10-31 Brd Co Ltd Shafts
FR2600013A1 (en) * 1986-06-11 1987-12-18 Volkswagen Ag TORSION ELEMENT, CONSISTING OF OVERLAPPED FIBER STRATES
US6581644B1 (en) 1997-04-04 2003-06-24 Exxonmobil Research And Engineering Company Composite pipe structure having improved containment and axial strength
WO1999062704A1 (en) * 1998-06-05 1999-12-09 Exxon Research And Engineering Company Composite pipe structures having improved containment and axial strength
DE102007036436A1 (en) * 2007-08-02 2009-02-05 Benteler Automobiltechnik Gmbh hybrid wave

Also Published As

Publication number Publication date
GB2010446B (en) 1982-02-17
IT7830480A0 (en) 1978-12-01
DE2852033A1 (en) 1979-06-07
DE2852033C2 (en) 1988-06-09
FR2410758B1 (en) 1984-11-23
CA1098329A (en) 1981-03-31
JPS6245412B2 (en) 1987-09-26
IT1100449B (en) 1985-09-28
FR2410758A1 (en) 1979-06-29
JPS5479337A (en) 1979-06-25

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Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PE20 Patent expired after termination of 20 years

Effective date: 19981130