WO2003045659A1 - Process for fabricating polypropylene sheet - Google Patents

Process for fabricating polypropylene sheet Download PDF

Info

Publication number
WO2003045659A1
WO2003045659A1 PCT/GB2002/004562 GB0204562W WO03045659A1 WO 2003045659 A1 WO2003045659 A1 WO 2003045659A1 GB 0204562 W GB0204562 W GB 0204562W WO 03045659 A1 WO03045659 A1 WO 03045659A1
Authority
WO
WIPO (PCT)
Prior art keywords
fibres
web
cooling
monolithic article
polymer
Prior art date
Application number
PCT/GB2002/004562
Other languages
French (fr)
Inventor
Ian Macmillan Ward
Peter John Hine
Original Assignee
Btg International Limited
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 to CA2465289A priority Critical patent/CA2465289C/en
Priority to AT02765109T priority patent/ATE502751T1/en
Priority to EP02765109A priority patent/EP1453647B1/en
Priority to US10/496,500 priority patent/US20040239002A1/en
Priority to DK02765109.0T priority patent/DK1453647T3/en
Priority to DE60239561T priority patent/DE60239561D1/en
Application filed by Btg International Limited filed Critical Btg International Limited
Priority to BRPI0214502-2A priority patent/BR0214502B1/en
Priority to AU2002329481A priority patent/AU2002329481A1/en
Priority to JP2003547140A priority patent/JP4756824B2/en
Publication of WO2003045659A1 publication Critical patent/WO2003045659A1/en
Priority to HK05101869.1A priority patent/HK1068846A1/en
Priority to US11/790,142 priority patent/US8021592B2/en

Links

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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/006Pressing and sintering powders, granules or 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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/003Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor characterised by the choice of material
    • 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
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/10Polymers of propylene
    • B29K2023/12PP, i.e. polypropylene
    • 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
    • B29K2105/25Solid
    • 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
    • B29K2223/00Use of polyalkenes or derivatives thereof as reinforcement
    • B29K2223/10Polymers of propylene
    • B29K2223/12PP, i.e. polypropylene
    • 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0077Yield strength; Tensile strength
    • 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0082Flexural strength; Flexion stiffness
    • 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0083Creep
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/24994Fiber embedded in or on the surface of a polymeric matrix

Definitions

  • The- present invention relates to polymer sheet materials made from oriented olefin polymer fibres or tapes, and in particular an improved process for making such materials.
  • the fibres may have been subjected to a prior crosslinking process, preferably an irradiation crosslinking process comprising irradiating the fibres with an ionising radiation in an inert environment containing alkylene or diene compounds, and then an annealing step comprising annealing the irradiated polymer at an elevated temperature, again in an inert environment containing alkyne or diene compounds.
  • a prior crosslinking process preferably an irradiation crosslinking process comprising irradiating the fibres with an ionising radiation in an inert environment containing alkylene or diene compounds
  • an annealing step comprising annealing the irradiated polymer at an elevated temperature, again in an inert environment containing alkyne or diene compounds.
  • the hot compacted materials are preferably cooled to ambient temperature under controlled conditions. Rapid cooling is less preferred. The most convenient technique is to allow the compacts to stand in the air until they have
  • the present invention provides a process for production of a monolithic article from a web of fibres of oriented polypropylene homopolymer or copolymer, comprising the steps of subjecting the web to elevated temperature and pressure sufficient to melt a proportion of the polymer and compact it, and then cooling the compacted web, wherein an accelerated rate of cooling is employed down to a lower temperature and in which said lower temperature is a predetermined amount below the recrystallisation temperature of the fibres.
  • the present invention provides a process for production of a monolithic article from a web of fibres of oriented polypropylene homopolymer or copolymer, comprising the steps of subjecting the web to elevated temperature and pressure sufficient to melt a proportion of the polymer and compact it, and then cooling the compacted web, wherein an accelerated rate of cooling is employed down to 100°C.
  • the fibres can be made by any suitable process, for example by solution or gel or melt forming, but most preferably by melt forming.
  • fibres of oriented polypropylene homopolymer or copolymer is used herein to denote all elongate elements which comprise polypropylene. They may be in the form of strands or filaments. They may be in the form of bands, ribbons or tapes, formed for example by initially slitting melt formed films. Whatever their form the fibres may be laid in a non-woven web for the process of the invention.
  • fibres may be formed into yarns comprising multiple fibres, or used in the form of a monofilament yarn.
  • the fibres are usually formed into a fabric by weaving or knitting.
  • the fibres may have been subjected to a crosslinking process, as described in WO 98/15397.
  • Woven fabrics may comprise only fibres in the form of strands or filaments, or they may comprise a mixture of fibres in the form of strands or filaments and fibres in the form of tapes. Most preferred are fabrics which are woven from flat tapes, as these have the best mechanical properties.
  • An accelerated rate of cooling in this specification means cooling under conditions such that heat is lost from the monolithic article more quickly than if it were cooled from the elevated temperature to a predetermined lower temperature below the recrystallisation temperature for the material, under ambient conditions, that is, in still air at ambient temperature, typically 20°C. That is, the monolithic article reaches the lower temperature more quickly than it would under ambient conditions. Cooling is not necessarily accelerated throughout the temperature range from the elevated temperature to the lower temperature. Suitably, however, an accelerated rate of cooling may be applied throughout the range from the elevated temperature down to the lower temperature.
  • the actual lower temperature is selected depending upon the recrystallisation temperature of the material being treated and should be one sufficiently below the recrystallisation temperature to ensure the material is prevented from recrystallising once the lower temperature has been reached. This may be achieved with a lower temperature as little as 10°C below the recrystallisation temperature when one employs temperature stabilisation techniques. However it will be appreciated that a greater temperature differential such as between 10°C and 20°C or between 10°C and 40°C or indeed greater may be employed to good effect. In the particular example discussed later herein the lower temperature for polypropylene was selected to be 100°C.
  • An accelerated rate of cooling may in principle be achieved by one or more of the following means:
  • the rate at which the compacted web is cooled is preferably at least 10°C per minute, preferably at least 30°C per minute, still more preferably at least 50°C per minute.
  • Particularly preferred is extremely rapid cooling of at least 100°C per minute, preferably at least 200°C per minute, and in the case of thin sheets in excess of 500°C per minute. These are average values applying to the entire cooling phase, from the elevated temperature to 100°C.
  • Very rapid rates of cooling may be termed quenching and may, indeed, be achieved by the traditional quenching method long used in the metallurgical art, of immersing the respective article in water.
  • the accelerated rate of cooling of the compacted web in accordance with the present invention only applies down to 100°C, which is significantly below the recrystallisation temperature.
  • the hot compaction process of the invention uses a compaction pressure not exceeding 10 MPa. It is also preferred that a single pressure is used throughout the hot compaction process. Most preferred pressures are between 1 and 7 MPa, particularly between 2 and 5 MPa. It is preferred that the hot compaction pressure is maintained during cooling.
  • the minimum temperature at which the fibres should be contacted is preferably that at which the leading edge of the endotherm, measured by Differential Scanning Calorimetry (DSC), of the constrained polymer fibres extrapolated to zero intersects the temperature axis.
  • DSC Differential Scanning Calorimetry
  • the temperature at which the fibres are compacted is no greater than the constrained peak temperature of melting at the ambient compaction pressure - i.e. the temperature of which the endotherm reaches it highest point.
  • the proportion of the fibres which is melted during the hot compaction process is generally between 10 and 50 percent by weight.
  • the fibres used in the present invention have a weight average molecular weight (M w ) in the range 100,000 to 800,000.
  • M w is in the range 250,000 to 450,000, for example 330,000 to 400,000.
  • M w is in the range 100,000 to 250,000, for example 150,000 to 220,000; M w being determined by the method described hereinafter. With such materials of lower M w the present invention provides a route to high yield stress and Young's modulus, yet should show a yield point rather than brittle failure.
  • the polymer is preferably a polypropylene homopolymer, but may be a copolymer comprising polypropylene. Generally any copolymer containing polypropylene such as those disclosed in WO 98/15397 may be used.
  • Compaction of the polypropylene may be carried out in an autoclave, or in a belt press or other apparatus in which the assembly is fed through a compaction zone where it is subjected to the required elevated temperature and pressure.
  • the process may be operated as a continuous or semi-continuous process. Cooling is preferably effected whilst the sheet is restrained against dimensional change, for example by being held under tension or by being still under a compaction pressure.
  • the belt press for example, the belt itself may be cooled (for example using air chilled by ice water) in the region immediately after the heating zone. In this way, it is possible to achieve cooling rates of up to 500°C per minute.
  • the monolithic article may be regarded as a polypropylene composite made up of a polypropylene matrix phase which was produced during the process, and a polypropylene fibre phase, a proportion of which may show selective surface melting, arising from the process.
  • the properties of both the matrix phase and the fibre phase are of significance in achieving a monolithic article of the required properties, and they may be defined, and studied, separately.
  • the Young's modulus of the matrix phase is at least 0.9 GPa, more preferably at least 1.2 GPa, more preferably at least 1.5 GPa, and most preferably at least 1.8 GPa.
  • the failure strength of the matrix phase is at least 20 MPa, more preferably at least 25 MPa, and most preferably at least 35 MPa.
  • the failure strain of the matrix phase is at least 5%.
  • the Young's modulus in the longitudinal direction (which may alternatively be called the draw or axial direction) of the fibre phase is at least 4 GPa, more preferably at least 6 GPa, and most preferably at least 8 GPa.
  • the failure strength in the longitudinal direction of the fibre phase is at least 250 MPa, more preferably at least 350 MPa, and most preferably at least 420 MPa.
  • the failure strain in the longitudinal direction of the fibre phase is at least
  • the effect of cooling rate was established by examining the cooling of a completely melted fabric, to simulate the melted matrix phase in a hot compacted sheet. It has been found that the properties of a hot compacted sheet are a combination of the properties of the original oriented fibres (the reinforcing phase), and the portion of the fibres which are melted (the matrix phase). Therefore by examining the properties of a melted fabric which has been cooled at different rates, it is possible to simulate the effect of cooling a hot compaction sheet at different rates.
  • the fabrics used were made from a number of different melt formed polypropylene homopolymers detailed in Table 1 below.
  • the reinforcement type indicates the type of fibre from which the fabric is woven.
  • M w and M n were measured by Rapra Technology Limited, of Shropshire, UK. Details of the testing are as follows:
  • the stress/strain behaviour of the above cooled films was measured using an RDP Howden servo-mechanical tensile testing machine.
  • the tensile tests on the compacted sheets and the melted films were carried out following ASTM D638 using a dumbbell shaped specimen. A nominal strain rate of 10 "3 s "1 was used for all the tests.
  • the sample strain during the tests was measured using a Messphysik video extensometer. Five samples were tested for each material at a temperature of 20 ⁇ 2°C and a relative humidity of 35 ⁇ 5%.
  • Typical stress-strain curves are shown in Figure 1, for each of the four polymer tests.
  • the results show that for all four polymers, the quenched samples were ductile and drew in a stable manner with the formation of a stable neck region. Strain for these samples was measured from the crosshead speed, rather than directly on the sample, for if the neck formed outside the measured region, the strain in the measurement region actually decreased.
  • the traces for the cooled and quenched samples have been displaced a small way along the x-axis simply in order to display each trace clearly.
  • the densities of the original oriented materials and the compacted sheets were measured using a density column.
  • the column was made from a mixture of digycidyl ether and isopropanol to give a density range of -890 to -930 kg m 3 .
  • the results are shown in Table 2.
  • the Young's Modulus was determined in the initial linear region of the stress strain curve following the guidelines of ASTM D638. The results are shown in Table 3 below.
  • Tables 2 and 3 show the density and Young's modulus of the various melted films. Both of these properties can be used as a measure of the crystallinity of the films, as one can attribute increases in either parameter with an increase in crystallinity. As the cooling rate is increased, the density and Young's modulus for each polymer type decreases. The cause is believed to be a decrease in crystallinity. Another result is an improvement in ductility.
  • the present invention is of benefit in situations where improved ductility (or related properties such as peel strength) is required. It is of particular benefit for polymers of lower M w , for example of M w 250,000 and below, since slow cooling regimes provide very brittle products, with such polymers.
  • Sheet samples were made using Polymer 1 cloths, and further sheet samples were made using Polymer 4 cloths.
  • the sheet samples were made of four layers of cloth, in a 0/90/90/0 lay-up (that is, the middle layers are orthogonal to the outer layers), and conditions were chosen to give a oriented fibre/matrix microstructure. In this way the central layers, where the peeling takes place, are in the same orientation, but overall the sheet samples have balanced properties.
  • Appropriate compaction conditions were chosen for the Polymer 1 and Polymer 4 samples. For Polymer 1 this was a compaction temperature of 182°C, a compaction pressure of 2.8 GPa, and a dwell time of 5 minutes.
  • the sheet samples were then tested for peel strength (interlayer adhesion).
  • the test was the T-Peel test (ASTM D1876). Samples for testing were 10mm wide and 100mm long and were tested using a crosshead speed of lOOmm/min. The testing was carried out parallel to the warp direction. Three samples were tested for each polymer and the results were averaged.
  • peel strength values for Polymer 4 are, as expected, higher than the values for Polymer 1.
  • the values for Polymer 4 are essentially the same for the fast and slow cooled samples. In contrast the fast cooled samples of Polymer 1 have a much higher peel strength value than the slow cooled samples.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Nonwoven Fabrics (AREA)
  • Reinforced Plastic Materials (AREA)
  • Laminated Bodies (AREA)
  • Wrappers (AREA)
  • Artificial Filaments (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Manufacture Of Macromolecular Shaped Articles (AREA)
  • Addition Polymer Or Copolymer, Post-Treatments, Or Chemical Modifications (AREA)

Abstract

A process for production of a monolithic article from a web of fibres of oriented polypropylene polymer, comprising the steps of subjecting the web to elevated temperature and pressure sufficient to melt a proportion of the polymer and compact it, and then cooling the compacted web, wherein an accelerated rate of cooling is employed down to 100°C. The process is of particular benefit when the weight average molecular weight (MW) of the fibres is 250,000 or below. The resultant articles have good stiffness and strength, yet with reasonable ductility. Similar articles cooled slowly are brittle.

Description

PROCESS FOR FABRICATING POLYPROPYLENE SHEET
The- present invention relates to polymer sheet materials made from oriented olefin polymer fibres or tapes, and in particular an improved process for making such materials.
In recent years, developments have been made in processes for compacting polyolefin fibres in order to make sheets of high stiffness and strength. Two-step compaction processes for melt-spun fibres employing high compaction pressures are well known. An example is disclosed in GB 2253420A, in which an assembly of fibres of an oriented polymer is hot compacted in a two-step process to form a sheet having good mechanical properties. The process involves an initial step in which the fibres are brought to and held at the compaction temperature whilst subject to a pressure sufficient to maintain the fibres in contact, and thereafter compacted at a high pressure (40-50 MPa) for a few seconds (the compaction pressure). In this process a proportion of the fibre surfaces, generally from 5 to 10 percent by weight, melt and subsequently recrystallise on cooling. This recrystallise phase binds the fibres together, resulting in good mechanical properties of the final sheet.
It is mentioned in GB 2253420A that the process can be applied to many types of oriented polymer including polyester and PEEK (polyether ether ketone) but that preferred polymers are oriented polyolefins. Polyethylene is the only polyolefin mentioned, and is used in all of the examples.
In WO 98/15397, an improvement to the above process is disclosed in which an assembly of melt-formed polyolefin fibres is maintained in intimate contact at elevated temperature sufficient to melt a proportion of the fibres, whilst being subjected to a compaction pressure of no greater than 10 MPa. This single-step, low- pressure process also produces products having excellent mechanical properties. If wished the fibres may have been subjected to a prior crosslinking process, preferably an irradiation crosslinking process comprising irradiating the fibres with an ionising radiation in an inert environment containing alkylene or diene compounds, and then an annealing step comprising annealing the irradiated polymer at an elevated temperature, again in an inert environment containing alkyne or diene compounds. In GB 2253420A it is stated that "the hot compacted materials are preferably cooled to ambient temperature under controlled conditions. Rapid cooling is less preferred. The most convenient technique is to allow the compacts to stand in the air until they have cooled to ambient temperature." The examples of GB 2253420A do not mention cooling rate.
In the examples of WO 98/15397 the compaction temperature and pressure were applied and the assembly was cooled under the compaction pressure to 100°C by passing a mixture of air and water through the heating platens. At this point the assembly was removed from the press and cooled to room temperature in air with no pressure applied. Cooling rate is not mentioned.
In Plastics, Rubber and Composites Processing and Applications, 1998, Vol 27, No. 4, pgs 167-171, specifically in relation to polyethylene it was stated that "the final cooling rate does not significantly affect the structure or properties of the final compacted sheet: quenched samples have been measured to have almost identical properties to slow cooled samples.."
Despite the above, we now have evidence to suggest that the cooling rate can have a significant effect on the final properties of compacted articles formed from fibres of oriented homopolymer or copolymer material.
In particular, we have discovered that unlike polyethylene, in the case of polypropylene the cooling rate has a significant effect on the final properties of the compacted sheet. Specifically, faster cooling rates result in the improvement of some properties, in particular ductility, and related properties such as peel strength.
Accordingly, the present invention provides a process for production of a monolithic article from a web of fibres of oriented polypropylene homopolymer or copolymer, comprising the steps of subjecting the web to elevated temperature and pressure sufficient to melt a proportion of the polymer and compact it, and then cooling the compacted web, wherein an accelerated rate of cooling is employed down to a lower temperature and in which said lower temperature is a predetermined amount below the recrystallisation temperature of the fibres.
In a particular aspect, the present invention provides a process for production of a monolithic article from a web of fibres of oriented polypropylene homopolymer or copolymer, comprising the steps of subjecting the web to elevated temperature and pressure sufficient to melt a proportion of the polymer and compact it, and then cooling the compacted web, wherein an accelerated rate of cooling is employed down to 100°C.
The fibres can be made by any suitable process, for example by solution or gel or melt forming, but most preferably by melt forming.
The term "fibres of oriented polypropylene homopolymer or copolymer" is used herein to denote all elongate elements which comprise polypropylene. They may be in the form of strands or filaments. They may be in the form of bands, ribbons or tapes, formed for example by initially slitting melt formed films. Whatever their form the fibres may be laid in a non-woven web for the process of the invention.
Alternatively they may be formed into yarns comprising multiple fibres, or used in the form of a monofilament yarn. The fibres are usually formed into a fabric by weaving or knitting. Optionally the fibres may have been subjected to a crosslinking process, as described in WO 98/15397. Woven fabrics may comprise only fibres in the form of strands or filaments, or they may comprise a mixture of fibres in the form of strands or filaments and fibres in the form of tapes. Most preferred are fabrics which are woven from flat tapes, as these have the best mechanical properties.
"An accelerated rate of cooling" in this specification means cooling under conditions such that heat is lost from the monolithic article more quickly than if it were cooled from the elevated temperature to a predetermined lower temperature below the recrystallisation temperature for the material, under ambient conditions, that is, in still air at ambient temperature, typically 20°C. That is, the monolithic article reaches the lower temperature more quickly than it would under ambient conditions. Cooling is not necessarily accelerated throughout the temperature range from the elevated temperature to the lower temperature. Suitably, however, an accelerated rate of cooling may be applied throughout the range from the elevated temperature down to the lower temperature.
The actual lower temperature is selected depending upon the recrystallisation temperature of the material being treated and should be one sufficiently below the recrystallisation temperature to ensure the material is prevented from recrystallising once the lower temperature has been reached. This may be achieved with a lower temperature as little as 10°C below the recrystallisation temperature when one employs temperature stabilisation techniques. However it will be appreciated that a greater temperature differential such as between 10°C and 20°C or between 10°C and 40°C or indeed greater may be employed to good effect. In the particular example discussed later herein the lower temperature for polypropylene was selected to be 100°C.
An accelerated rate of cooling may in principle be achieved by one or more of the following means:
contacting the compacted web with a fluid which is below ambient temperature - contacting the compacted web with a fluid which is a better thermal conductor than air at ambient temperature providing for relative movement between the compacted web and a fluid; most practicably, by impelling the fluid over the compacted web.
The rate at which the compacted web is cooled is preferably at least 10°C per minute, preferably at least 30°C per minute, still more preferably at least 50°C per minute. Particularly preferred is extremely rapid cooling of at least 100°C per minute, preferably at least 200°C per minute, and in the case of thin sheets in excess of 500°C per minute. These are average values applying to the entire cooling phase, from the elevated temperature to 100°C. Very rapid rates of cooling may be termed quenching and may, indeed, be achieved by the traditional quenching method long used in the metallurgical art, of immersing the respective article in water. The accelerated rate of cooling of the compacted web in accordance with the present invention only applies down to 100°C, which is significantly below the recrystallisation temperature.
It is preferred that the hot compaction process of the invention uses a compaction pressure not exceeding 10 MPa. It is also preferred that a single pressure is used throughout the hot compaction process. Most preferred pressures are between 1 and 7 MPa, particularly between 2 and 5 MPa. It is preferred that the hot compaction pressure is maintained during cooling.
The minimum temperature at which the fibres should be contacted is preferably that at which the leading edge of the endotherm, measured by Differential Scanning Calorimetry (DSC), of the constrained polymer fibres extrapolated to zero intersects the temperature axis. Preferably, the temperature at which the fibres are compacted is no greater than the constrained peak temperature of melting at the ambient compaction pressure - i.e. the temperature of which the endotherm reaches it highest point. The proportion of the fibres which is melted during the hot compaction process is generally between 10 and 50 percent by weight.
Preferably the fibres used in the present invention have a weight average molecular weight (Mw) in the range 100,000 to 800,000. In certain embodiments Mw is in the range 250,000 to 450,000, for example 330,000 to 400,000. In certain other embodiments Mwis in the range 100,000 to 250,000, for example 150,000 to 220,000; Mw being determined by the method described hereinafter. With such materials of lower Mw the present invention provides a route to high yield stress and Young's modulus, yet should show a yield point rather than brittle failure.
The polymer is preferably a polypropylene homopolymer, but may be a copolymer comprising polypropylene. Generally any copolymer containing polypropylene such as those disclosed in WO 98/15397 may be used.
Compaction of the polypropylene may be carried out in an autoclave, or in a belt press or other apparatus in which the assembly is fed through a compaction zone where it is subjected to the required elevated temperature and pressure. Thus, the process may be operated as a continuous or semi-continuous process. Cooling is preferably effected whilst the sheet is restrained against dimensional change, for example by being held under tension or by being still under a compaction pressure. In the case of a belt press for example, the belt itself may be cooled (for example using air chilled by ice water) in the region immediately after the heating zone. In this way, it is possible to achieve cooling rates of up to 500°C per minute.
The monolithic article may be regarded as a polypropylene composite made up of a polypropylene matrix phase which was produced during the process, and a polypropylene fibre phase, a proportion of which may show selective surface melting, arising from the process. The properties of both the matrix phase and the fibre phase are of significance in achieving a monolithic article of the required properties, and they may be defined, and studied, separately.
Preferably the Young's modulus of the matrix phase is at least 0.9 GPa, more preferably at least 1.2 GPa, more preferably at least 1.5 GPa, and most preferably at least 1.8 GPa.
Preferably the failure strength of the matrix phase is at least 20 MPa, more preferably at least 25 MPa, and most preferably at least 35 MPa.
Preferably the failure strain of the matrix phase is at least 5%.
Preferably the Young's modulus in the longitudinal direction (which may alternatively be called the draw or axial direction) of the fibre phase is at least 4 GPa, more preferably at least 6 GPa, and most preferably at least 8 GPa.
Preferably the failure strength in the longitudinal direction of the fibre phase is at least 250 MPa, more preferably at least 350 MPa, and most preferably at least 420 MPa.
Preferably the failure strain in the longitudinal direction of the fibre phase is at least
5%. EXAMPLE SET A
The effect of cooling rate was established by examining the cooling of a completely melted fabric, to simulate the melted matrix phase in a hot compacted sheet. It has been found that the properties of a hot compacted sheet are a combination of the properties of the original oriented fibres (the reinforcing phase), and the portion of the fibres which are melted (the matrix phase). Therefore by examining the properties of a melted fabric which has been cooled at different rates, it is possible to simulate the effect of cooling a hot compaction sheet at different rates.
The fabrics used were made from a number of different melt formed polypropylene homopolymers detailed in Table 1 below. The reinforcement type indicates the type of fibre from which the fabric is woven.
TABLE 1
Figure imgf000009_0001
Mw and Mn were measured by Rapra Technology Limited, of Shropshire, UK. Details of the testing are as follows:
Instrument Waters 150CV
Columns Plgel 2 x mixed bed-B, 30cn 10 microns
Solvent 1,2-dichlorobenzene with anti-oxidant
Flow-rate 1.0 ml/min (nominal)
Temperature 140°C (nominal) Detector refractive index and differential pressure
GPC system calibrated with polystyrene
Woven cloths made of each of the above polymers were completely melted by heating two layers of cloth in a hot press at 200°C. The pressure applied was 2.8 MPa, although since the samples were completely melted this was not critical. Cooling was achieved either by removing the sample and plunging it into water (quenching) or in the hot press by passing a coolant through the heated platens, after switching off the heating. Depending on the rate of cooling required 100% water, or air containing water droplets, was used as the coolant. In this example fast cooling in the press means a cooling rate of 20-30°C/min. The slowest cooling rate, l-2°C/min, was achieved by just switching off the heating and allowing the assembly to cool naturally in air.
Samples which were cooled in the press were removed from the press when the temperature had dropped to 100°C, which is 20°C below the crystallisation temperature measured by DSC. The cooling rate is therefore determined by the time taken to cool from the compaction temperature down to 100°C.
PHYSICAL PROPERTIES
Mechanical properties
The stress/strain behaviour of the above cooled films was measured using an RDP Howden servo-mechanical tensile testing machine. The tensile tests on the compacted sheets and the melted films were carried out following ASTM D638 using a dumbbell shaped specimen. A nominal strain rate of 10"3 s"1 was used for all the tests. The sample strain during the tests was measured using a Messphysik video extensometer. Five samples were tested for each material at a temperature of 20 ± 2°C and a relative humidity of 35 ± 5%.
Typical stress-strain curves are shown in Figure 1, for each of the four polymer tests. The results show that for all four polymers, the quenched samples were ductile and drew in a stable manner with the formation of a stable neck region. Strain for these samples was measured from the crosshead speed, rather than directly on the sample, for if the neck formed outside the measured region, the strain in the measurement region actually decreased. The traces for the cooled and quenched samples have been displaced a small way along the x-axis simply in order to display each trace clearly.
For the sample made using fast cooling differences in behaviour were seen. The lowest molecular weight polymer (Polymer 1, Graph 1) showed an initial linear region, with an increased slope compared to the quenched sample - indicating higher Young's modulus - then a yield point, again higher than the quenched sample, then rupture after 7-8% of elongation. This form of stress-strain behaviour is often termed necking-rupture. Two intermediate molecular weight samples (Polymers 2 and 3, Graphs 2 and 3) showed the formation of a neck but drawing did not stabilise and rupture occurred at -25% (0.25) strain. Only the highest molecular weight Polymer 4 (Graph 4) showed stable drawing following application of the fast cooling rate.
All the samples made by slow cooling showed necking-rupture or brittle behaviour. The failure strains of the original fibres were mostly between 10 and 20% (0.1 and 0.2): therefore if the matrix fails below this value then a hot compacted composite would see premature matrix failure before the reinforcing phase can reach full load carrying capacity, leading to premature delamination. It is seen that at the slowest cooling rate, none of the polymers reached this desired failure strain. In particular, the low molecular weight Polymer 1 showed brittle failure at a low stress.
It is clear that the cooling rate of the hot compaction process is a key process parameter, because it has a significant effect on the mechanical properties of the matrix phase, probably due to changes in crystallinity. The above results show that both quenching and fast cooling enhanced matrix ductility. As explained above, the greater the ductility of the matrix phase (and therefore the higher its failure strain) the better, in many situations, especially those in which the properties of hot compacted sheet are dominated by the matrix phase. These include interlayer adhesion (or peel strength) which depends mainly on the properties of the matrix, thermoformability where significant interlayer shear occurs (differential sliding between the layers), and normal tensile properties. Density
The densities of the original oriented materials and the compacted sheets were measured using a density column. The column was made from a mixture of digycidyl ether and isopropanol to give a density range of -890 to -930 kg m3. The results are shown in Table 2.
TABLE 2
Figure imgf000012_0001
Modulus
The Young's Modulus was determined in the initial linear region of the stress strain curve following the guidelines of ASTM D638. The results are shown in Table 3 below.
TABLE 3
Figure imgf000013_0001
Tables 2 and 3 show the density and Young's modulus of the various melted films. Both of these properties can be used as a measure of the crystallinity of the films, as one can attribute increases in either parameter with an increase in crystallinity. As the cooling rate is increased, the density and Young's modulus for each polymer type decreases. The cause is believed to be a decrease in crystallinity. Another result is an improvement in ductility.
The present invention is of benefit in situations where improved ductility (or related properties such as peel strength) is required. It is of particular benefit for polymers of lower Mw, for example of Mw 250,000 and below, since slow cooling regimes provide very brittle products, with such polymers.
EXAMPLE SET B
Peel Strength
Sheet samples were made using Polymer 1 cloths, and further sheet samples were made using Polymer 4 cloths. In each case the sheet samples were made of four layers of cloth, in a 0/90/90/0 lay-up (that is, the middle layers are orthogonal to the outer layers), and conditions were chosen to give a oriented fibre/matrix microstructure. In this way the central layers, where the peeling takes place, are in the same orientation, but overall the sheet samples have balanced properties. Appropriate compaction conditions were chosen for the Polymer 1 and Polymer 4 samples. For Polymer 1 this was a compaction temperature of 182°C, a compaction pressure of 2.8 GPa, and a dwell time of 5 minutes. For Polymer 4 this was a compaction temperature of 192°C, a compaction pressure of 2.8 GPa, and a compaction dwell time of 5 minutes. Slow cooling was achieved by switching off the heating and allowing the heating platens, containing the sheet sample, to cool in air (l-2°C/min). Fast cooling (35°C/min in this example) was achieved by passing water through the heating platens.
The sheet samples were then tested for peel strength (interlayer adhesion). The test was the T-Peel test (ASTM D1876). Samples for testing were 10mm wide and 100mm long and were tested using a crosshead speed of lOOmm/min. The testing was carried out parallel to the warp direction. Three samples were tested for each polymer and the results were averaged.
The results are shown in Table 4 below.
TABLE 4
Figure imgf000014_0001
It will be seen that the peel strength values for Polymer 4 are, as expected, higher than the values for Polymer 1. The values for Polymer 4 are essentially the same for the fast and slow cooled samples. In contrast the fast cooled samples of Polymer 1 have a much higher peel strength value than the slow cooled samples.

Claims

1. A process for production of a monolithic article from a web of fibres of oriented polypropylene homopolymer or copolymer, comprising the steps of subjecting the web to elevated temperature and pressure sufficient to melt a proportion of the polymer and compact it, and then cooling the compacted web, wherein an accelerated rate of cooling is employed down to a lower temperature and in which said lower temperature is a predetermined amount below the recrystallisation temperature of the fibres.
2. A process for production of a monolithic article from a web of fibres of oriented polypropylene homopolymer or copolymer, comprising the steps of subjecting the web to elevated temperature and pressure sufficient to melt a proportion of the polymer and compact it, and then cooling the compacted web, wherein an accelerated rate of cooling is employed down to 100°C.
3. A process as claimed in claim 1 or 2 wherein the compacted web is cooled at a mean rate of at least 10°C per minute, down to 100°C.
4. A process as claimed in claim 2 or 3 wherein the compacted web is cooled at a mean rate of at least 30°C per minute, down to 100°C.
5. A process as claimed in any preceding claim wherein the compaction pressure does not exceed 10 MPa.
6. A process as claimed in any preceding claim, wherein the fibres are melt formed fibres.
7. A process as claimed in any preceding claim wherein the weight average molecular weight (Mw) of the fibres is in the range 100,000 to 800,000.
8. A process as claimed in claim 7 wherein the weight average molecular weight (Mw) of the fibres is in the range 100,000 to 250,000.
9. A process as claimed in claim 8 wherein the weight average molecular weight (Mw) of the fibres is in the range 150,000 to 220,000.
10. A monolithic article manufactured by a process as claimed in any preceding claim, having a matrix phase of polymer which was produced by selective melting of the oriented phase during the process and an oriented fibre phase a fraction of which was melted during the process.
11. A monolithic article as claimed in claim 10 wherein the Young's modulus of the matrix phase is at least 0.9 GPa.
12. A monolithic article as claimed in claim 10 or 11 wherein the failure strength of the matrix phase is at least 20 MPa.
13. A monolithic article as claimed in claim 10, 11 or 12 wherein the failure strain of the matrix phase is at least 5%.
14. A monolithic article as claimed in any of claims 10 to 13 wherein the Young's modulus in the longitudinal direction of the oriented fibre phase is at least 4 GPa.
15. A monolithic article as claimed in any of claims 10 to 14 wherein the failure strength in the longitudinal direction of the oriented fibre phase is at least 250 MPa.
16. A monolithic article as claimed in any of claims 10 to 15 wherein the failure strain in the longitudinal direction of the oriented fibre phase is at least 5%.
17. A process of fabricating a monolithic article comprising polypropylene polymer or copolymer, or a monolithic article thus formed, substantially as hereinbefore described with particular reference to the accompanying examples.
PCT/GB2002/004562 2001-11-27 2002-10-08 Process for fabricating polypropylene sheet WO2003045659A1 (en)

Priority Applications (11)

Application Number Priority Date Filing Date Title
AT02765109T ATE502751T1 (en) 2001-11-27 2002-10-08 METHOD FOR PRODUCING A THIN PLATE FROM POLYPROPYLENE
EP02765109A EP1453647B1 (en) 2001-11-27 2002-10-08 Process for fabricating polypropylene sheet
US10/496,500 US20040239002A1 (en) 2001-11-27 2002-10-08 Process for fabricating polypropylene sheet
DK02765109.0T DK1453647T3 (en) 2001-11-27 2002-10-08 Process for producing polypropylene sheet
DE60239561T DE60239561D1 (en) 2001-11-27 2002-10-08 METHOD FOR PRODUCING A THIN PLATE OF POLYPROPYLENE
CA2465289A CA2465289C (en) 2001-11-27 2002-10-08 Process for fabricating polypropylene sheet
BRPI0214502-2A BR0214502B1 (en) 2001-11-27 2002-10-08 A process for producing a monolithic article from a oriented polypropylene homopolymer or copolymer fiber network.
AU2002329481A AU2002329481A1 (en) 2001-11-27 2002-10-08 Process for fabricating polypropylene sheet
JP2003547140A JP4756824B2 (en) 2001-11-27 2002-10-08 Secondary processing of polypropylene sheet
HK05101869.1A HK1068846A1 (en) 2001-11-27 2005-03-03 Process for fabricating polypropylene sheet
US11/790,142 US8021592B2 (en) 2001-11-27 2007-04-24 Process for fabricating polypropylene sheet

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0128405.8 2001-11-27
GBGB0128405.8A GB0128405D0 (en) 2001-11-27 2001-11-27 Process for fabricating polyolefin sheet

Related Child Applications (2)

Application Number Title Priority Date Filing Date
US10496500 A-371-Of-International 2002-10-08
US11/790,142 Continuation US8021592B2 (en) 2001-11-27 2007-04-24 Process for fabricating polypropylene sheet

Publications (1)

Publication Number Publication Date
WO2003045659A1 true WO2003045659A1 (en) 2003-06-05

Family

ID=9926542

Family Applications (2)

Application Number Title Priority Date Filing Date
PCT/GB2002/004562 WO2003045659A1 (en) 2001-11-27 2002-10-08 Process for fabricating polypropylene sheet
PCT/GB2002/004572 WO2003045660A1 (en) 2001-11-27 2002-10-08 Process for fabricating polypropylene sheet

Family Applications After (1)

Application Number Title Priority Date Filing Date
PCT/GB2002/004572 WO2003045660A1 (en) 2001-11-27 2002-10-08 Process for fabricating polypropylene sheet

Country Status (13)

Country Link
US (4) US20040239002A1 (en)
EP (2) EP1453647B1 (en)
JP (2) JP4949608B2 (en)
AT (2) ATE526137T1 (en)
AU (2) AU2002329481A1 (en)
BR (2) BR0214502B1 (en)
CA (2) CA2466832C (en)
DE (1) DE60239561D1 (en)
DK (2) DK1458538T3 (en)
ES (2) ES2363212T3 (en)
GB (1) GB0128405D0 (en)
HK (2) HK1068846A1 (en)
WO (2) WO2003045659A1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7294384B2 (en) 2005-09-27 2007-11-13 Milliken & Company Moldable construction incorporating bonding interface
US7294383B2 (en) 2005-09-27 2007-11-13 Milliken & Company Moldable construction incorporation non-olefin bonding interface
US7378359B2 (en) 2005-09-27 2008-05-27 Eleazer Howell B Moldable fibrous construction incorporating non-woven layers
US7892379B2 (en) 2006-09-11 2011-02-22 Milliken & Company Moldable fabric with unidirectional tape yarns
US8021592B2 (en) 2001-11-27 2011-09-20 Propex Operating Company Llc Process for fabricating polypropylene sheet
US8052913B2 (en) 2003-05-22 2011-11-08 Propex Operating Company Llc Process for fabricating polymeric articles
US9643382B2 (en) 2013-05-06 2017-05-09 Milliken & Company Fiber reinforced structural element

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
MXPA04002446A (en) 2001-09-26 2004-07-23 Baxter Int Preparation of submicron sized nanoparticles via dispersion and solvent or liquid phase removal.
US8676509B2 (en) 2001-11-13 2014-03-18 Dako Denmark A/S System for tracking biological samples
BRPI0516389A (en) 2004-10-22 2008-09-02 Dow Global Technologies Inc process to form a conformed three-dimensional article and apparatus
DK2100073T3 (en) * 2006-12-06 2010-05-31 Shell Int Research Use of a composite material as a barrier under cryogenic conditions
DK2693159T3 (en) * 2007-11-01 2018-03-12 Dsm Ip Assets Bv Plate of material and process for its manufacture
DE102008011303B4 (en) * 2008-02-27 2013-06-06 Siemens Aktiengesellschaft Operating method for a cooling line for cooling a rolling stock with temperature-separated cooling to a final enthalpy value
JP5850686B2 (en) * 2011-09-26 2016-02-03 積水化学工業株式会社 Manufacturing method of resin molded product and resin molded product
DE102014203235A1 (en) 2014-02-24 2015-08-27 Mahle International Gmbh Air conditioner, in particular for a motor vehicle and method for producing a component of an air conditioner
WO2016198097A1 (en) 2015-06-09 2016-12-15 Müller Textil GmbH Composite tent tarpaulin and tent arrangement
KR101713714B1 (en) 2015-06-29 2017-03-22 현대자동차주식회사 Thermoplastic resin composite and preparation method thereof
JP6097367B2 (en) * 2015-10-02 2017-03-15 積水化学工業株式会社 Manufacturing method of resin molded product and resin molded product
CA3237007A1 (en) 2021-11-08 2023-05-11 Liqiu Chu Polypropylene composite material having melting point gradient structure, preparation method therefor and system and use thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3962205A (en) * 1973-03-06 1976-06-08 National Research Development Corporation Polymer materials
US3997386A (en) * 1974-05-31 1976-12-14 Mitsubishi Jukogyo Kabushiki Kaisha Method for bonding thermoplastic high molecular weight materials
US4642153A (en) * 1983-05-31 1987-02-10 Allen Industries, Inc. Method and apparatus for making a sheet of material
WO1988009406A1 (en) * 1987-05-21 1988-12-01 Automotive Investment Co. Molding process using polypropylene strands and fabric fibers to produce article
US4948661A (en) * 1987-07-10 1990-08-14 C. H. Masland & Sons Glossy finish fiber reinforced molded product and processes of construction
GB2253420A (en) * 1991-03-07 1992-09-09 British Tech Group Polymeric materials
WO1998015397A2 (en) * 1996-10-04 1998-04-16 University Of Leeds Innovations Limited Method for compacting olefin fibres

Family Cites Families (86)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB397656A (en) * 1932-07-22 1933-08-31 Gen Electric Co Ltd Improvements in the manufacture of thermionic cathodes for electric discharge devices
US3017834A (en) * 1943-08-28 1962-01-23 Robert H Park Magnetic detecting device
US3231650A (en) * 1960-03-11 1966-01-25 Phillips Petroleum Co Non-woven polyolefin fabrics and method of preparing same
US3367926A (en) * 1964-03-25 1968-02-06 Dow Chemical Co Modification of crystalline structure of crystallizable high polymers
JPS462192Y1 (en) 1967-11-06 1971-01-25
US3689597A (en) * 1970-06-26 1972-09-05 Hercules Inc Polyphase compositions and process for their preparation
US3947537A (en) * 1971-07-16 1976-03-30 Exxon Research & Engineering Co. Battery separator manufacturing process
DE2404479A1 (en) * 1973-02-12 1974-08-15 Fmc Corp HIGH MODULE COPOLYESTER FIBER YARN
GB1469526A (en) * 1973-03-06 1977-04-06 Nat Res Dev Polymer materials
US3884521A (en) * 1973-09-24 1975-05-20 Moore Alvin E Light-weight, durable, land-traversing vehicle
FR2246587B1 (en) * 1973-10-03 1978-08-11 Nat Res Dev
JPS5112870A (en) 1974-07-15 1976-01-31 Furukawa Electric Co Ltd HORIOREFUINHAIGOBUTSUNO SEIKEIHOHO
JPS5419027B2 (en) 1974-09-26 1979-07-12
US4048364A (en) * 1974-12-20 1977-09-13 Exxon Research And Engineering Company Post-drawn, melt-blown webs
JPS5237875A (en) 1975-09-19 1977-03-24 Chisso Corp Manufacture of unwoven molded sheet
GB1568964A (en) * 1975-11-05 1980-06-11 Nat Res Dev Oriented polymer materials
US4013816A (en) * 1975-11-20 1977-03-22 Draper Products, Inc. Stretchable spun-bonded polyolefin web
US4091140A (en) * 1976-05-10 1978-05-23 Johnson & Johnson Continuous filament nonwoven fabric and method of manufacturing the same
DE2634537C3 (en) * 1976-07-31 1980-08-14 Ruhrchemie Ag, 4200 Oberhausen Process for the production of molded articles from polyolefins with molecular weights of at least 1 million
US4285748A (en) * 1977-03-11 1981-08-25 Fiber Industries, Inc. Selfbonded nonwoven fabrics
US4228118A (en) * 1977-11-03 1980-10-14 Monsanto Company Process for producing high tenacity polyethylene fibers
US4191718A (en) * 1977-12-19 1980-03-04 Ford Motor Company Thick section compression molded composites
US4234536A (en) * 1978-09-27 1980-11-18 Thiel Alfons W Method for the manufacture of thin-walled shaped articles of crystalline thermoplastic material
US4413110A (en) * 1981-04-30 1983-11-01 Allied Corporation High tenacity, high modulus polyethylene and polypropylene fibers and intermediates therefore
US4384016A (en) 1981-08-06 1983-05-17 Celanese Corporation Mutiaxially oriented high performance laminates comprised of uniaxially oriented sheets of thermotropic liquid crystal polymers
US4454270A (en) * 1981-12-14 1984-06-12 Ethyl Corporation Method and composition for preventing or suppressing discoloration in polyolefins
US4551296A (en) * 1982-03-19 1985-11-05 Allied Corporation Producing high tenacity, high modulus crystalline article such as fiber or film
US4403012A (en) * 1982-03-19 1983-09-06 Allied Corporation Ballistic-resistant article
US4455273A (en) * 1982-09-30 1984-06-19 Allied Corporation Producing modified high performance polyolefin fiber
US4483727A (en) * 1983-02-07 1984-11-20 Celanese Corporation High modulus polyethylene fiber bundles as reinforcement for brittle matrices
US5135804A (en) * 1983-02-18 1992-08-04 Allied-Signal Inc. Network of polyethylene fibers
EP0116845B1 (en) 1983-02-18 1989-12-20 AlliedSignal Inc. Consolidation of polyethylene fibrous networks
JPS6059172A (en) * 1983-09-09 1985-04-05 東洋紡績株式会社 Crosslinked polyethylene fiber
GB8332952D0 (en) 1983-12-09 1984-01-18 Ward I M Polymer irradiation
US4551293A (en) * 1984-03-05 1985-11-05 Jamak, Inc. Method of forming spark plug boots
ATE54094T1 (en) * 1984-04-13 1990-07-15 Nat Res Dev PROCESSES FOR DEFORMING IN THE SOLID STATE.
US4568581A (en) * 1984-09-12 1986-02-04 Collins & Aikman Corporation Molded three dimensional fibrous surfaced article and method of producing same
US4654262A (en) * 1985-04-10 1987-03-31 Itt Corporation Polyolefin resin surface preparation
DE3516425A1 (en) * 1985-05-08 1986-11-13 Bayer Ag, 5090 Leverkusen METHOD FOR PRODUCING MOLDED BODIES AND FILMS FROM THERMOTROPICAL POLYMERS, AND MOLDED BODIES AND FILMS PRODUCED THEREFORE
GB8513345D0 (en) * 1985-05-28 1985-07-03 Busm Co Ltd Gauge control of heat-softenable material
US4607640A (en) * 1985-11-18 1986-08-26 Mccusker Leroy H Athletic/industrial brassiere with protective inserts
US4931230A (en) * 1986-05-08 1990-06-05 Minnesota Mining And Manufacturing Company Method for preparing radiation resistant polypropylene articles
US4786348A (en) * 1987-01-05 1988-11-22 E. I. Du Pont De Nemours And Company Method of making transparent oriented sheets
CA1323301C (en) 1987-06-05 1993-10-19 Alan I. Faden Thyrotropin-releasing hormone analogs in cns injury
US4990204A (en) * 1987-10-27 1991-02-05 The Dow Chemical Company Improved spunbonding of linear polyethylenes
NL8801195A (en) 1988-05-06 1989-12-01 Stamicarbon BALLISTIC STRUCTURE.
JPH07103507B2 (en) 1988-08-23 1995-11-08 ユニチカ株式会社 Nonwoven fabric made of heat-bondable long fibers
NL8900475A (en) 1989-02-25 1990-09-17 Stamicarbon A PROCESS FOR MANUFACTURING PRODUCTS CONTAINING POLYALKEN FIBERS.
CA2011182C (en) 1989-04-07 1993-12-07 Thomas I. Insley Sorbent, impact resistant container
US5006390A (en) * 1989-06-19 1991-04-09 Allied-Signal Rigid polyethylene reinforced composites having improved short beam shear strength
NL8902194A (en) 1989-08-31 1991-03-18 Stamicarbon FABRIC OF THERMOPLASTIC AND CONTINUOUS REINFORCEMENT FIBER.
US5200131A (en) * 1990-04-09 1993-04-06 Mitsui Toatsu Chemicals, Inc. Method for molding syndiotactic polypropylene
US5032339A (en) * 1990-07-19 1991-07-16 E. I. Du Pont De Nemours And Company Process for shaping fiber reinforced thermoplastic articles
NL9002590A (en) 1990-11-28 1992-06-16 Stamicarbon MULTILAYER, ANTI-BALLISTIC STRUCTURE.
US5628946A (en) * 1991-03-07 1997-05-13 British Technology Group Limited Process for producing polymeric materials
US5244482A (en) * 1992-03-26 1993-09-14 The University Of Tennessee Research Corporation Post-treatment of nonwoven webs
NL9200625A (en) 1992-04-03 1993-11-01 Dsm Nv NON-WOVEN POLYOLEFINE FIBER LAYER FOR USE IN A LAYERED ANTIBALLISTIC STRUCTURE.
JPH0687185A (en) * 1992-07-22 1994-03-29 Mitsui Toatsu Chem Inc Laminated molding
US5514448A (en) 1992-07-22 1996-05-07 Mitsui Toatsu Chemicals, Inc. Laminated molding
US5654045A (en) 1992-12-21 1997-08-05 Hoechst Celanese Corp. Multiaxially reinforced LCP sheet
BE1007230A3 (en) 1993-06-23 1995-04-25 Dsm Nv COMPOSITE JOB mutually parallel fibers in a matrix.
JP2602166B2 (en) 1993-07-12 1997-04-23 近藤 弘康 Heat-resistant nonwoven fabric and method for producing the same
US5324576A (en) * 1993-08-25 1994-06-28 Minnesota Mining And Manufacturing Company Polyolefin meltblown elastic webs
FR2719553B1 (en) * 1994-05-04 1996-07-26 Eurocopter France Anti-torque device with rear rotor and shrouded stator for helicopter.
JP3226709B2 (en) * 1994-05-06 2001-11-05 帝人株式会社 Aramid-polyester laminate, intermediate material thereof and methods for producing them
US5573824A (en) * 1994-05-11 1996-11-12 Texas Instruments High strength, high modulus continuous polymeric material for durable, impact resistant applications
US5688426A (en) * 1995-06-07 1997-11-18 The Boeing Company Hybrid metal webbed composite beam
NL1000598C2 (en) 1995-06-20 1996-12-23 Dsm Nv Anti-ballistic molded part and a method of manufacturing the molded part.
NL1001415C2 (en) 1995-10-13 1997-04-15 Dsm Nv Anti-ballistic molded part.
GB9600800D0 (en) * 1996-01-15 1996-03-20 British Tech Group Compacted biomaterials
US20020031652A1 (en) * 1996-01-15 2002-03-14 Ward Ian Macmillan Compacted biomaterials
NL1003405C2 (en) 1996-06-24 1998-01-07 Dsm Nv Anti-ballistic molded part.
GB9620692D0 (en) * 1996-10-04 1996-11-20 Vantage Polymers Limited Olefin polymers
GB9620691D0 (en) * 1996-10-04 1996-11-20 Vantage Polymers Limited Olefin polymers
US6132657A (en) * 1998-06-29 2000-10-17 Polyeitan Composites Ltd. Process for producing polymeric materials
NL1010399C1 (en) 1998-10-26 2000-04-27 Dsm Nv Method for manufacturing a molded part.
US6191123B1 (en) * 1999-03-19 2001-02-20 Parker Hughes Institute Organic-arsenic compounds
US6482343B1 (en) * 1999-06-28 2002-11-19 Polyeitan Composites Ltd. Polymeric materials and process for producing same
DE10017493B4 (en) 2000-04-07 2009-02-26 Daimler Ag Method for producing a component with an internal tissue
GB0111287D0 (en) * 2001-05-09 2001-06-27 Amoco Detschland Gmbh Polyolefin sheet
GB0114669D0 (en) * 2001-06-15 2001-08-08 Btg Int Ltd Amorphous polymer articles
GB0128405D0 (en) 2001-11-27 2002-01-16 Btg Int Ltd Process for fabricating polyolefin sheet
US7082731B2 (en) * 2002-09-03 2006-08-01 Murray Patz Insulated concrete wall system
NL1021805C2 (en) 2002-11-01 2004-05-06 Dsm Nv Method for the manufacture of an antiballistic molding.
JP2007520371A (en) 2004-01-01 2007-07-26 ディーエスエム アイピー アセッツ ビー.ブイ. Bulletproof articles
JP2007517959A (en) 2004-01-07 2007-07-05 ディーエスエム アイピー アセッツ ビー.ブイ. Method for manufacturing curved object

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3962205A (en) * 1973-03-06 1976-06-08 National Research Development Corporation Polymer materials
US3997386A (en) * 1974-05-31 1976-12-14 Mitsubishi Jukogyo Kabushiki Kaisha Method for bonding thermoplastic high molecular weight materials
US4642153A (en) * 1983-05-31 1987-02-10 Allen Industries, Inc. Method and apparatus for making a sheet of material
WO1988009406A1 (en) * 1987-05-21 1988-12-01 Automotive Investment Co. Molding process using polypropylene strands and fabric fibers to produce article
US4948661A (en) * 1987-07-10 1990-08-14 C. H. Masland & Sons Glossy finish fiber reinforced molded product and processes of construction
GB2253420A (en) * 1991-03-07 1992-09-09 British Tech Group Polymeric materials
WO1998015397A2 (en) * 1996-10-04 1998-04-16 University Of Leeds Innovations Limited Method for compacting olefin fibres

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8021592B2 (en) 2001-11-27 2011-09-20 Propex Operating Company Llc Process for fabricating polypropylene sheet
US8052913B2 (en) 2003-05-22 2011-11-08 Propex Operating Company Llc Process for fabricating polymeric articles
US8268439B2 (en) 2003-05-22 2012-09-18 Propex Operating Company, Llc Process for fabricating polymeric articles
US8871333B2 (en) 2003-05-22 2014-10-28 Ian MacMillan Ward Interlayer hot compaction
US9403341B2 (en) 2003-05-22 2016-08-02 Propex Operating Company Llc Interlayer hot compaction
US10850479B2 (en) 2003-05-22 2020-12-01 Canco Hungary Investment Ltd. Process for fabricating polymeric articles
US7294384B2 (en) 2005-09-27 2007-11-13 Milliken & Company Moldable construction incorporating bonding interface
US7294383B2 (en) 2005-09-27 2007-11-13 Milliken & Company Moldable construction incorporation non-olefin bonding interface
US7300691B2 (en) 2005-09-27 2007-11-27 Milliken & Company Moldable construction incorporating non-olefin bonding interface
US7378359B2 (en) 2005-09-27 2008-05-27 Eleazer Howell B Moldable fibrous construction incorporating non-woven layers
US7892379B2 (en) 2006-09-11 2011-02-22 Milliken & Company Moldable fabric with unidirectional tape yarns
US9643382B2 (en) 2013-05-06 2017-05-09 Milliken & Company Fiber reinforced structural element

Also Published As

Publication number Publication date
WO2003045660A1 (en) 2003-06-05
BR0214500A (en) 2004-11-09
CA2465289C (en) 2011-01-11
HK1068846A1 (en) 2005-05-06
ES2373311T3 (en) 2012-02-02
ES2363212T3 (en) 2011-07-27
US20050064163A1 (en) 2005-03-24
US20100178486A1 (en) 2010-07-15
JP2005510636A (en) 2005-04-21
EP1458538B1 (en) 2011-09-28
CA2466832A1 (en) 2003-06-05
EP1453647A1 (en) 2004-09-08
DE60239561D1 (en) 2011-05-05
BR0214502B1 (en) 2012-10-30
ATE526137T1 (en) 2011-10-15
JP4949608B2 (en) 2012-06-13
DK1458538T3 (en) 2012-01-02
EP1458538A1 (en) 2004-09-22
BR0214500B1 (en) 2012-02-07
US8021592B2 (en) 2011-09-20
JP4756824B2 (en) 2011-08-24
AU2002334122A1 (en) 2003-06-10
EP1453647B1 (en) 2011-03-23
BR0214502A (en) 2004-11-09
CA2465289A1 (en) 2003-06-05
US20070196634A1 (en) 2007-08-23
JP2005510635A (en) 2005-04-21
ATE502751T1 (en) 2011-04-15
US20040239002A1 (en) 2004-12-02
HK1069559A1 (en) 2005-05-27
DK1453647T3 (en) 2011-05-09
GB0128405D0 (en) 2002-01-16
AU2002329481A1 (en) 2003-06-10
CA2466832C (en) 2010-11-16

Similar Documents

Publication Publication Date Title
US8021592B2 (en) Process for fabricating polypropylene sheet
Hine et al. The hot compaction of high modulus melt-spun polyethylene fibres
US20210008850A1 (en) Process for Fabricating Polymeric Articles
Goutianos et al. Failure mechanisms in unidirectional self-reinforced biobased composites based on high stiffness PLA fibres
Ye et al. Mode I interlaminar fracture of co-mingled yarn based glass/polypropylene composites
Wang et al. Properties of polypropylene single-polymer composites produced by the undercooling melt film stacking method
Ye et al. Interlaminar fracture of commingled-fabric-based GF/PET composites
EP1479498A1 (en) Process for fabricating polymeric articles

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NO NZ OM PH PL PT RO RU SD SE SG SI SK SL TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR IE IT LU MC NL PT SE SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
WWE Wipo information: entry into national phase

Ref document number: 2465289

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 2003547140

Country of ref document: JP

WWE Wipo information: entry into national phase

Ref document number: 2002765109

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 10496500

Country of ref document: US

WWP Wipo information: published in national office

Ref document number: 2002765109

Country of ref document: EP