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GB1551223A - Tubular members - Google Patents

Tubular members

Info

Publication number
GB1551223A
GB1551223A GB1828175A GB1828175A GB1551223A GB 1551223 A GB1551223 A GB 1551223A GB 1828175 A GB1828175 A GB 1828175A GB 1828175 A GB1828175 A GB 1828175A GB 1551223 A GB1551223 A GB 1551223A
Authority
GB
United Kingdom
Prior art keywords
tubular members
tubular
members
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.)
Expired
Application number
GB1828175A
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.)
High Temperature Engineers Ltd
Original Assignee
High Temperature Engineers Ltd
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 High Temperature Engineers Ltd filed Critical High Temperature Engineers Ltd
Priority to GB1828175A priority Critical patent/GB1551223A/en
Priority to FR7612559A priority patent/FR2309453A2/en
Priority to IT2283576A priority patent/IT1059040B/en
Priority to DE19762619257 priority patent/DE2619257A1/en
Publication of GB1551223A publication Critical patent/GB1551223A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
    • F16C7/02—Constructions of connecting-rods with constant length
    • F16C7/026—Constructions of connecting-rods with constant length made of fibre reinforced resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56—Winding and joining, e.g. winding spirally
    • B29C53/58—Winding and joining, e.g. winding spirally helically
    • B29C53/583—Winding and joining, e.g. winding spirally helically for making tubular articles with particular features
    • B29C53/585—Winding and joining, e.g. winding spirally helically for making tubular articles with particular features the cross-section varying along their axis, e.g. tapered, with ribs, or threads, with socket-ends
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H81/00—Methods, apparatus, or devices for covering or wrapping cores by winding webs, tapes, or filamentary material, not otherwise provided for
    • 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
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L33/00—Arrangements for connecting hoses to rigid members; Rigid hose-connectors, i.e. single members engaging both hoses
    • F16L33/22—Arrangements for connecting hoses to rigid members; Rigid hose-connectors, i.e. single members engaging both hoses with means not mentioned in the preceding groups for gripping the hose between inner and outer parts

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
GB1828175A 1975-05-01 1975-05-01 Tubular members Expired GB1551223A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB1828175A GB1551223A (en) 1975-05-01 1975-05-01 Tubular members
FR7612559A FR2309453A2 (en) 1975-05-01 1976-04-28 METHOD AND APPARATUS FOR WINDING A BAND OF FLEXIBLE MATERIAL ON A CYLINDRICAL CHUCK WITH TRUNCONIC ENDS
IT2283576A IT1059040B (en) 1975-05-01 1976-04-29 TUBULAR ORGAN REINFORCED BY A REINFORCEMENT WRAPPED
DE19762619257 DE2619257A1 (en) 1975-05-01 1976-04-30 TUBULAR COMPONENT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1828175A GB1551223A (en) 1975-05-01 1975-05-01 Tubular members

Publications (1)

Publication Number Publication Date
GB1551223A true GB1551223A (en) 1979-08-30

Family

ID=10109778

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1828175A Expired GB1551223A (en) 1975-05-01 1975-05-01 Tubular members

Country Status (4)

Country Link
DE (1) DE2619257A1 (en)
FR (1) FR2309453A2 (en)
GB (1) GB1551223A (en)
IT (1) IT1059040B (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0237046A3 (en) * 1986-03-12 1988-06-08 Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. Connection fitting for axially initiating load and pressure forces in bars of fiber composite
DE4029008C1 (en) * 1990-09-13 1991-10-31 Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt Ev, 5300 Bonn, De
DE4135695A1 (en) * 1991-10-25 1993-04-29 Deutsche Forsch Luft Raumfahrt ROD WITH A TUBULAR WALL OF FIBER COMPOSITE MATERIAL AND CONNECTING ELEMENT SIDED ON either side
US8205315B2 (en) 2006-11-01 2012-06-26 Tyee Aircraft Composite tube assemblies and methods of forming the same
EP3193029A1 (en) * 2016-01-12 2017-07-19 Crompton Technology Group Limited Composite tubular structure
EP4045802B1 (en) * 2019-10-14 2024-12-04 Avtechtyee, Inc. Methods for forming a composite tube assembly and composite tube assembly comprising slotted joints

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2371598A2 (en) * 1976-11-19 1978-06-16 Dassault Avions Connecting rod for aircraft controls - has metal bushes bonded to conical ends of rods formed of carbon fibre embedded in synthetic resin
DE2855570C2 (en) * 1978-12-22 1985-06-20 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Rod-shaped component
FR2446180A1 (en) * 1979-01-15 1980-08-08 Aerospatiale METHOD FOR PRODUCING A CONTROL OR TRANSMISSION OF EFFORTS AND CONNECTING ROD THUS OBTAINED
DE2926493C2 (en) * 1979-06-30 1982-09-09 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8000 München Strut for longitudinal pull and pressure
FR2469604A1 (en) * 1979-11-08 1981-05-22 Rech Meca Appliquee CONNECTING ROD OR THE LIKE HAVING A HOLLOW BODY
FR2469605A1 (en) * 1979-11-08 1981-05-22 Rech Meca Appliquee CONNECTING ROD OR SIMILAR OBJECT
DE2951629C2 (en) * 1979-12-21 1985-03-14 Felten & Guilleaume Energietechnik GmbH, 5000 Köln Drive shaft made of fiber-reinforced plastic, with a lost mandrel and tightly wound end pieces
FR2496836A1 (en) * 1980-12-23 1982-06-25 Maschf Augsburg Nuernberg Ag Lightweight strut for framework or machine - has inner and outer tubes with glass fibre reinforced layers between end caps
US5318374A (en) * 1992-09-23 1994-06-07 The Boeing Company Composite tube structure
US8157469B2 (en) * 2006-11-22 2012-04-17 The Boeing Company Composite structural member and method for producing the same
FR2942163B1 (en) * 2009-01-21 2016-04-15 Conseil & Technique PIECE OF COMPOSITE MATERIAL, ROD IN COMPOSITE MATERIAL AND METHOD OF MANUFACTURING THE SAME
DE102015213308B4 (en) * 2015-07-15 2019-03-14 Thyssenkrupp Ag Vibration damper with carbon fiber damper tube with threaded adapter for motor vehicle
DE102016102643B3 (en) * 2016-02-15 2017-05-11 Stefan OGINSKI Rod-shaped assembly with Umkrempelung and method for producing the rod-shaped assembly and use of a shell of fabric layer to form the Umkrempelung
DE102017001133A1 (en) 2017-02-07 2018-08-09 Liebherr-Components Kirchdorf GmbH Cylinder-piston device with at least one inner tube and at least one outer tube
US20250283504A1 (en) * 2024-03-08 2025-09-11 AvtechTyee, Inc. 3d printed linkage

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2837456A (en) * 1952-02-29 1958-06-03 Kellogg M W Co Filament wound container
US2848133A (en) * 1954-10-28 1958-08-19 Einar M Ramberg Pressure vessels and methods of making such vessels
US3571878A (en) * 1968-07-01 1971-03-23 Teledyne Inc Industrial rolls
GB1319235A (en) * 1969-07-18 1973-06-06 Dowty Rotol Ltd Devices of fibrous-reinforced plastics material
GB1330313A (en) * 1970-09-23 1973-09-19 British Aircraft Corp Ltd Composite structures
US3725981A (en) * 1970-10-07 1973-04-10 Boeing Co Joint construction and method of fabrication
NL7212295A (en) * 1971-09-18 1973-03-20
FR2343918A1 (en) * 1976-03-10 1977-10-07 Dassault Avions Connecting rod for aircraft controls - has metal bushes bonded to conical ends of rods formed of carbon fibre embedded in synthetic resin

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0237046A3 (en) * 1986-03-12 1988-06-08 Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. Connection fitting for axially initiating load and pressure forces in bars of fiber composite
DE4029008C1 (en) * 1990-09-13 1991-10-31 Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt Ev, 5300 Bonn, De
DE4135695A1 (en) * 1991-10-25 1993-04-29 Deutsche Forsch Luft Raumfahrt ROD WITH A TUBULAR WALL OF FIBER COMPOSITE MATERIAL AND CONNECTING ELEMENT SIDED ON either side
US8205315B2 (en) 2006-11-01 2012-06-26 Tyee Aircraft Composite tube assemblies and methods of forming the same
EP3193029A1 (en) * 2016-01-12 2017-07-19 Crompton Technology Group Limited Composite tubular structure
EP4045802B1 (en) * 2019-10-14 2024-12-04 Avtechtyee, Inc. Methods for forming a composite tube assembly and composite tube assembly comprising slotted joints

Also Published As

Publication number Publication date
IT1059040B (en) 1982-05-31
FR2309453A2 (en) 1976-11-26
DE2619257A1 (en) 1976-11-11

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Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed