EP3348684A1 - Carbon fiber manufacturing method and carbon fiber manufacturing apparatus - Google Patents

Carbon fiber manufacturing method and carbon fiber manufacturing apparatus Download PDF

Info

Publication number
EP3348684A1
EP3348684A1 EP17000054.1A EP17000054A EP3348684A1 EP 3348684 A1 EP3348684 A1 EP 3348684A1 EP 17000054 A EP17000054 A EP 17000054A EP 3348684 A1 EP3348684 A1 EP 3348684A1
Authority
EP
European Patent Office
Prior art keywords
carbon fiber
plasma
module
fiber manufacturing
chamber
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
EP17000054.1A
Other languages
German (de)
French (fr)
Other versions
EP3348684B1 (en
Inventor
Chih-Yung Wang
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.)
UHT Unitech Co Ltd
Original Assignee
UHT Unitech Co 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 UHT Unitech Co Ltd filed Critical UHT Unitech Co Ltd
Priority to EP17000054.1A priority Critical patent/EP3348684B1/en
Publication of EP3348684A1 publication Critical patent/EP3348684A1/en
Application granted granted Critical
Publication of EP3348684B1 publication Critical patent/EP3348684B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01FCHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F9/00Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
    • D01F9/08Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
    • D01F9/12Carbon filaments; Apparatus specially adapted for the manufacture thereof
    • D01F9/14Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
    • D01F9/32Apparatus therefor
    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01DMECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
    • D01D10/00Physical treatment of artificial filaments or the like during manufacture, i.e. during a continuous production process before the filaments have been collected
    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01FCHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F9/00Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
    • D01F9/08Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
    • D01F9/12Carbon filaments; Apparatus specially adapted for the manufacture thereof
    • D01F9/14Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
    • D01F9/20Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M2101/00Chemical constitution of the fibres, threads, yarns, fabrics or fibrous goods made from such materials, to be treated
    • D06M2101/40Fibres of carbon

Definitions

  • the present invention relates to a carbon fiber manufacturing technique, and more particularly to a carbon fiber manufacturing method and a carbon fiber manufacturing apparatus which can greatly improve the sizing quality of a carbon fiber and effectively reduce the cost of the carbon fiber production equipment and the working time.
  • Carbon fibers are classified into carbon fibers or graphite fibers according to their carbon contents, which have excellent mechanical properties and electrical properties and can be widely used in various applications.
  • a conventional carbon fiber is achieved by bundling precursor fibers, such as polyacrylonitrile fibers, to form a carbon fiber precursor fiber bundle, and then the carbon fiber precursor fiber bundle is calcined (high-temperature carbonization) to form the carbon fiber.
  • PAN polyacrylonitrile
  • the carbon fiber precursor fiber bundles are heated to form carbon fibers or graphite fibers by different heating apparatuses according to the application of the carbon fibers.
  • the carbon content of the fibers of graphite fibers is 90% or more, forming a two-dimensional carbocyclic planar net structure and a graphite layer structure having parallel layers.
  • the results show that the crystalline region of a high-strength carbon fiber is composed of 5-6 graphite layers, and the crystalline region of a high-strength and high-modulus carbon fiber is composed of 10-20 graphite layers. Theoretically and practically, it is pointed out that the larger the crystalline thickness of the graphite layer is, the higher the tensile modulus of the carbon fiber is.
  • the surface of the carbon fiber after the high-temperature carbonization step is usually coated with a layer of oiling agent (a resin oiling agent is generally used, it is called as a sizing step) before it leaves the factory.
  • the layer of oiling agent is used to protect the fiber from breakage due to friction in the subsequent step to affect the overall quality of the carbon fiber.
  • the surfaces of untreated carbon fibers adsorb impurities thereon. Since these impurities are present between the surface of the carbon fiber and the resin oiling agent, the adhesion between the carbon fiber and the resin oiling agent is insufficient, and the purpose of protecting the fiber cannot be achieved
  • the surface of the carbon fiber is excessively finely formed due to high-temperature sintering, and there are few functional groups on the surface.
  • the fiber and the resin oiling agent cannot be bonded fully in the sizing step.
  • a heat treatment or electrolysis technique can be applied to the surface treatment of the fiber after the high-temperature carbonization step, and then the sizing step is performed in order to improve the bonding of the fiber and the resin oiling agent.
  • the surface treatment of the carbon fiber is performed by means of heat treatment
  • the carbon fiber is treated at a temperature in the range of 500°C to 800°C for 1-10 minutes.
  • a relatively long period of time is required.
  • the heat treatment is always performed with a large number of fibers at a time, so it is difficult to control the processing quality.
  • the surface treatment of the carbon fiber is performed by means of electrolysis, at least one drying process is required before the surface of the fiber is coated with the oiling agent. This also takes more time.
  • a change of the electrolyte may affect the processing quality. Even the surface of the fiber may have depositions.
  • the primary object of the present invention is to provide a carbon fiber manufacturing method which can greatly improve the sizing quality of a carbon fiber and effectively reduce the cost of the carbon fiber production equipment and the working time.
  • the carbon fiber manufacturing method of the present invention comprises providing a raw material step, providing a carbon fiber precursor fiber bundle; performing a high-temperature carbonization step, the carbon fiber precursor fiber bundle being heated to form a carbon fiber having a predetermined carbon content; performing a plasma surface treatment step, a plasma gas flow with a predetermined power being provided to act on the carbon fiber at a predetermined time so that a surface of the carbon fiber is formed with a plasma-modified configuration; performing a sizing step, the plasma-modified configuration being coated with a resin oiling agent; and performing a drying step, the resin oiling agent coated on the plasma-modified configuration being processed with drying so that the resin oiling agent is firmly adhered to the surface of the carbon fiber.
  • the surface of the carbon fiber is roughened and provided with functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent and the carbon fiber in the subsequent sizing step so as to improve the sizing quality of the carbon fiber greatly.
  • the structure of the carbon fiber is more stable and reliable.
  • the plasma surface treatment belongs to a dry-type and fast surface treatment technique to effectively reduce the cost of the carbon fiber production equipment and the working time.
  • the carbon fiber precursor fiber bundle is guided into a chamber.
  • the chamber is formed with at least one microwave field concentration area therein, and is provided with a gas supply assembly to supply an inert gas and a microwave generating assembly to supply a high-frequency microwave.
  • the electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle passing through the microwave field concentration area.
  • the chamber is provided with at least one pair of microwave-sensitive materials.
  • the microwave-sensitive materials are one of graphite, carbide, magnetic compound, nitride, and ionic compound or a combination thereof.
  • the inert gas is nitrogen, argon, helium, or a combination thereof.
  • the frequency of the high-frequency microwave is in the range of 300-30,000 MHz, and its microwave power density is in the range of 1-1000kW/m3.
  • the chamber is an elliptic chamber.
  • the chamber is a flat panel chamber.
  • the plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • an atmospheric plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • a low-pressure plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • a microwave plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • a glow plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • the carbon fiber precursor fiber bundle has a surface not processed with a pre-oxidation treatment.
  • the carbon fiber precursor fiber bundle has a surface processed with a pre-oxidation treatment in advance.
  • the resin oiling agent is a thermosetting resin oiling agent.
  • the resin oiling agent is a thermoplastic resin oiling agent.
  • the carbon content of the carbon fiber is in the range of 80%-90%.
  • the carbon fiber manufacturing apparatus of the present invention comprises a feeding module, a receiving module, a high-temperature carbonization module, a plasma surface treatment module, and a sizing module.
  • the receiving module is disposed in the vicinity of the feeding module.
  • the feeding module and the receiving module constitute a carbon fiber drag route.
  • the high-temperature carbonization module is disposed at the carbon fiber drag route and located between the feeding module and the receiving module for heating the carbon fiber drag route.
  • the plasma surface treatment module is disposed at the carbon fiber drag route and located between the high-temperature carbonization module and the receiving module for supplying a plasma gas flow to the carbon fiber drag route.
  • the sizing module is disposed at the carbon fiber drag route and located between the plasma surface treatment module and the receiving module for coating a resin oiling agent on the surface of a carbon fiber.
  • the carbon fiber manufacturing apparatus of the present invention can be operated in the integrated operation of the feeding module, the high-temperature carbonization module, the plasma surface treatment module, the sizing module, and the receiving module.
  • a carbon fiber precursor fiber bundle released from the feeding module is sequentially processed at a predetermined speed to perform the steps of high-temperature carbonization, plasma surface treatment, sizing, and so on, in a relatively more active and reliable manner.
  • the carbon fiber precursor fiber bundle is heated to form the carbon fiber, and then the surface of the carbon fiber is formed with the resin oiling agent.
  • the surface of the carbon fiber is roughened and provided with functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent and the carbon fiber in the subsequent sizing procedure so as to improve the sizing quality of the carbon fiber greatly.
  • the structure of the carbon fiber is more stable and reliable.
  • the plasma surface treatment belongs to a dry-type and fast surface treatment technique to effectively reduce the cost of the carbon fiber production equipment and the working time.
  • the high-temperature carbonization module has a chamber for the carbon fiber drag route or the carbon fiber precursor fiber bundle to pass therethrough.
  • the chamber is formed with at least one microwave field concentration area and supplies an inert gas and a high-frequency microwave. Under the protection of the inert gas atmosphere, the electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle passing through the microwave field concentration area.
  • the high-temperature carbonization module has a chamber for the carbon fiber drag route or the carbon fiber precursor fiber bundle to pass therethrough.
  • the chamber is formed with at least one microwave field concentration area and provided with a gas supply assembly to supply an inert gas and a microwave generating assembly to supply a high-frequency microwave.
  • the electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle passing through the microwave field concentration area.
  • the plasma surface treatment module is provided with at least one plasma generator.
  • the plasma surface treatment module is provided with at least one plasma generator located at upper and lower positions of the carbon fiber drag route, respectively.
  • the chamber is an elliptic chamber.
  • the chamber is an elliptic chamber, and the chamber is provided with at least one pair of microwave-sensitive materials.
  • the chamber is a flat plate chamber.
  • the chamber is a flat plate chamber, and the chamber is provided with at least one pair of microwave-sensitive materials.
  • the plasma generator is able to generate the plasma gas flow having a power in the range of 100-10000 Watts.
  • the plasma generator is able to generate an atmospheric plasma gas flow having a power in a range of 100-10000 Watts.
  • the plasma generator is able to generate a low-pressure plasma gas flow having a power in the range of 100-10000 Watts.
  • the plasma generator is able to generate a microwave plasma gas flow having a power in the range of 100-10000 Watts.
  • the plasma generator is able to generate a glow plasma gas flow having a power in the range of 100-10000 Watts.
  • the sizing module is provided with at least one reservoir.
  • the carbon fiber manufacturing apparatus further comprises a drying module.
  • the drying module is disposed at the carbon fiber drag route between the sizing module and the receiving module for the resin oiling agent to be adhered to the surface of the carbon fiber firmly.
  • the surface of the carbon fiber can be roughened and provided with the functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent and the carbon fiber in the subsequent sizing step.
  • the structure of the carbon fiber is more stable and reliable.
  • the microwave focusing heating way the same apparatus can be applied to a carbon fiber precursor fiber bundle whose surface has not been processed with a pre-oxidation treatment or a carbon fiber precursor fiber bundle whose surface has been processed with a pre-oxidation treatment in advance.
  • the apparatus can be used to produce general carbon fibers or high modulus carbon fibers (graphite fibers) so as reduce the cost of the carbon fiber production equipment and the working time effectively.
  • the present invention discloses a carbon fiber manufacturing method which can greatly improve the sizing quality of carbon fibers and effectively reduce the cost of the carbon fiber production equipment and the working time.
  • the carbon fiber manufacturing method of the present invention comprises providing a raw material step, performing a high-temperature carbonization step, performing a plasma surface treatment step, and performing a sizing step.
  • the carbon fiber manufacturing method further comprises performing a drying step after the sizing step. Referring to FIG. 1 through FIG. 5 , the steps are described in details as below.
  • a carbon fiber precursor fiber bundle is provided to be processed to form a carbon fiber.
  • the carbon fiber precursor fiber bundle may be formed of rayon, poly vinyl alcohol, vinylidene chloride, polyacrylonitrile (PAN), pitch, and the like.
  • the surface of the carbon fiber precursor fiber bundle may have not been processed with a pre-oxidation treatment or have been processed with a pre-oxidation treatment in advance.
  • the carbon fiber precursor fiber bundle is heated to form the carbon fiber having a predetermined carbon content.
  • the carbon fiber precursor fiber bundle 70A is guided into a chamber 31 of a high-temperature carbonization module 30.
  • the chamber 31 is formed with at least one microwave field concentration area 311 therein, and is provided with a gas supply assembly 32 to supply an inert gas and a microwave generating assembly 33 to supply a high-frequency microwave.
  • the electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle 70A passing through the microwave field concentration area 311, enabling the carbon fiber precursor fiber bundle to form the carbon fiber 70B having a predetermined carbon content.
  • the carbon content of the carbon fiber 70B is in the range of 80%-90%.
  • a plasma gas flow with a predetermined power is provided to act on the carbon fiber 70B at a predetermined time, such that the surface of the carbon fiber 70B is formed with a plasma-modified configuration 71, shown in FIG. 3 , which is rougher or has more functional groups relative to the carbon fiber precursor fiber bundle 70A.
  • the plasma-modified configuration 71 on the surface of the carbon fiber 70B is coated with a resin oiling agent 80, so that the surface of the carbon fiber 70B has the resin oiling agent 80, as shown in FIG. 4 .
  • the resin oiling agent 80 is coated on the surface of the carbon fiber 70B by soaking or immersing.
  • the resin oiling agent 80 may be a thermosetting resin oiling agent or a thermoplastic resin oiling agent.
  • a drying treatment is applied to the resin oiling agent 80 coated on the plasma-modified configuration 71 so that the resin oiling agent 80 is firmly adhered to the surface of the carbon fiber 70B.
  • the drying treatment is carried out by ultraviolet irradiation, cooling, drying or air-drying for the resin oiling agent to be bonded to the surface of the carbon fiber.
  • an atmospheric plasma gas flow, a low-pressure plasma gas flow, a microwave plasma gas flow, or a glow plasma gas flow with a power of 100-10000 watts may be used to act on the carbon fiber 10B for 10-1000 milliseconds. Since the plasma gas flow contains particles having energy, the impurities that originally adhere to the surface of the carbon fiber 10B can be broken to form small molecules by the impact of the plasma gas flow through the physical reaction (collision) of the plasma gas flow, and then the small molecules are blown away from the surface of the carbon fiber 70B by the air flow, so that the surface of the carbon fiber 70B is clean.
  • the resin oiling agent 80 can be completely in contact with the carbon fiber 70B to increase the bonding effect.
  • the impact of the plasma gas flow will also form the plasma-modified configuration 71 on the surface of the carbon fiber 70B.
  • the plasma-modified configuration 71 is rougher relative to the carbon fiber precursor fiber bundle 70A, and is further formed with pores.
  • the surface of the carbon fiber 70B is roughened or formed with the pores, which is beneficial to increase the contact area between the resin oiling agent 80 and the carbon fiber 70B in the subsequent sizing step.
  • the resin oiling agent 80 penetrates into the pores, and the resin oiling agent 80 is anchored between the pores to form an anchor effect to enhance the bonding effect of the resin oiling agent 80 and the carbon fiber 70B.
  • the plasma gas flow also makes the surface of the carbon fiber 70B generate a chemical reaction at the same time, so that at least one functional group (such as -OH, -N, etc.) is added to the surface of the carbon fiber 70B.
  • the surface tension of the surface of the carbon fiber 70B is increased due to the presence of the functional group, which is beneficial to improve the wetting effect for the resin oiling agent 80 to be coated on the carbon fiber 70B. That is, the contact angle of the resin oiling agent 80 to the carbon fiber 70B becomes small, so that the resin oiling agent 80 can be quickly or instantaneously coated on the carbon fiber 70B, and the speed of the sizing step is increased, thereby accelerating the overall production speed of the carbon fiber 70B.
  • the presence of the functional group such as the OH group reacts with the resin oiling agent 80, such as epoxy resin (Epoxy), to generate hydrogen bonding, thereby increasing the bonding effect.
  • the surface of the carbon fiber 70B is roughened and provided with functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent 80 and the carbon fiber 70B in the subsequent sizing step so as to improve the sizing quality of the carbon fiber 70B greatly.
  • the structure of the carbon fiber is more stable and reliable.
  • the plasma surface treatment belongs to a dry-type and fast surface treatment technique to effectively reduce the cost of the carbon fiber production equipment and the working time.
  • the foregoing inert gas may be nitrogen, argon, helium, or a combination thereof.
  • the frequency of the high-frequency microwave may be in the range of 300-30,000 MHz, and its microwave power density may be in the range of 1-1000kW/m3.
  • the chamber 31 of the high-temperature carbonization module 30 may be an elliptic chamber, or the chamber 31 may be a flat plate chamber as shown in FIG. 5 .
  • the chamber 31 is provided with a pair of microwave-sensitive materials 34 therein, thereby enhancing the focusing effect on the microwave field in order to further accelerate the high-temperature carbonization process.
  • the microwave-sensitive materials 34 may be one of graphite, carbide, magnetic compound, nitride, and ionic compound or a combination thereof.
  • the carbonization of the carbon fiber is enhanced rapidly and more crystalline carbons are formed and stacked, which leads to the formation of larger graphite crystalline molecules, namely, larger graphite crystalline thickness, while deriving a higher microwave induction heating effect is derived.
  • Such a cycle generates an autocatalytic reaction, enabling the carbon fiber to be rapidly heated to the graphitization temperature (1500- 3000°C), and carbon atoms are reconstructed and rearranged more rapidly to form a graphite layer.
  • the same apparatus can be applied to a carbon fiber precursor fiber bundle whose surface has not been processed with a pre-oxidation treatment or a carbon fiber precursor fiber bundle whose surface has been processed with a pre-oxidation treatment in advance. It is only necessary to adjust the microwave power for the production, the apparatus can be used to produce general carbon fibers (1000-1500°C) or high modulus carbon fibers (graphite fibers).
  • an object to be tested that the resin oiling agent after the drying step is firmly adhered to the surface of the carbon fiber, and the treatment conditions in the plasma surface treatment step are shown in Table 1 below: Table 1: the conditions of the plasma surface treatment plasma gas consumption N 2 200 L/min CDA 0.4 L/min plasma gas amount 200.4 L/min plasma power 0 ⁇ 1000 W plasma surface treatment time 0.025 ⁇ 0.100 sec. carbon fiber yarn width 7 mm yarn per unit time receiving capacity 0.28 J/s distance 1 mm
  • the ILSS strength (interlayer bonding force) was measured for an object to be tested in an environment of a temperature of 23°C and a humidity of 50% RH by using an INSTRON measuring machine according to ASTM 2344, and the results are shown in Table 2 below: Table 2: the relationship between the plasma surface treatment power (W), the processing time (sec.), and the interlayer bonding force (MPa) (epoxy resin used as the resin oiling agent) of PAN carbon fiber 12K.
  • the carbon fiber without the plasma surface treatment the interlayer bonding force of the object to be tested is only 70MPa.
  • the processing time is 0.075 seconds and the plasma power is increased from the untreated (0W, without plasma power) to 1000W, the interlayer bonding force is increased from 70MPa to 89MPa. That is, the interlayer bonding force is increased to 127%.
  • FIG. 6a shows a SEM image of the object to be tested without the plasma treatment.
  • FIG. 6b shows a SEM image of the object to be tested with the plasma treatment.
  • the SEM image of the object to be tested without the plasma surface treatment illustrates a void H between the resin oiling agent 80 and the carbon fiber 70B because the surface of the carbon fiber 70B is smooth and doesn't have functional groups.
  • the void H causes a decrease in the strength of the object to be tested. That is to say, the bonding force between the carbon fiber and the resin oiling agent is insufficient for protecting the fiber.
  • the SEM image of the object to be tested with the plasma surface treatment illustrates that there is no void between the resin oiling agent 80 and the carbon fiber 70B because the surface of the carbon fiber 70B is rough and has functional groups (such as -OH, -N, etc.).
  • the resin oiling agent 80 and the carbon fiber 70B are bonded tightly, so that the strength of the object to be tested is enhanced. That is, the adhesion between the carbon fiber and the resin oiling agent is enhanced, so that the purpose of protecting the fiber can be achieved.
  • the present invention further discloses a carbon fiber manufacturing apparatus which can greatly improve the sizing quality of carbon fibers and effectively reduce the cost of the carbon fiber production equipment and the working time.
  • the carbon fiber manufacturing apparatus of the present invention comprises a feeding module 10, a receiving module 20, a high-temperature carbonization module 30, a plasma surface treatment module 40, and a sizing module 50.
  • the feeding module 10 is to perform the step of providing a raw material in the carbon fiber manufacturing method, and is used to supply a carbon fiber precursor fiber bundle 70A to be processed into a carbon fiber 70B.
  • the receiving module 20 is disposed in the vicinity of the feeding module 10, and corresponds to the feeding module 10 to constitute a carbon fiber drag route.
  • the receiving module 20 includes a yarn winding assembly 21 to receive the carbon fiber 70B.
  • the yarn winding assembly 21 performs a drag action on the carbon fiber 70B to be received.
  • the high-temperature carbonization module 30 is to perform the high-temperate carbonization step in the carbon fiber manufacturing method.
  • the high-temperature carbonization module 30 is disposed at the carbon fiber drag route between the feeding module 10 and the receiving module 20 for heating the carbon fiber precursor fiber bundle 70A, enabling the carbon fiber precursor fiber bundle 70A to become the carbon fiber 70B having a predetermined carbon content.
  • the plasma surface treatment module 40 is to perform the plasma surface treatment step in the carbon fiber manufacturing method.
  • the plasma surface treatment module 40 is disposed at the carbon fiber drag route between the high-temperature carbonization module 30 and the receiving module 20 to provide a plasma gas flow with a predetermined power to act on the carbon fiber 70B, such that the surface of the carbon fiber 70B is formed with a plasma-modified configuration 71 which is rougher or has more functional groups relative to the carbon fiber precursor fiber bundle 70A.
  • the sizing module 50 is to perform the sizing step in the carbon fiber manufacturing method.
  • the sizing module 50 is disposed at the carbon fiber drag route between the plasma surface treatment module 40 and the receiving module 20 for the plasma-modified configuration 71 on the surface of the carbon fiber 70B to be coated with a resin oiling agent 80.
  • the sizing module 50 is provided with at least one reservoir 51 for storing the resin oiling agent 80.
  • the carbon fiber manufacturing apparatus of the present invention may further comprise a drying module 60.
  • the drying module 60 is to perform the drying step in the carbon fiber manufacturing method.
  • the drying module 60 is disposed at the carbon fiber drag route between the sizing module 50 and the receiving module 20 for the resin oiling agent 80 to be firmly adhered to the surface of the carbon fiber 70B.
  • the drying module 60 is provided with at least one blast furnace 61 to generate hot blast.
  • the carbon fiber manufacturing apparatus of the present invention can be operated in the integrated operation of the feeding module 10, the high-temperature carbonization module 30, the plasma surface treatment module 40, the sizing module 50, and the receiving module 20.
  • the carbon fiber precursor fiber bundle 70A released from the feeding module 10 is sequentially processed at a predetermined speed to perform the steps of high-temperature carbonization, plasma surface treatment, sizing, and so on, in a relatively more active and reliable manner.
  • the carbon fiber precursor fiber bundle 70A is heated to form the carbon fiber 70B, and then the surface of the carbon fiber 70B is formed with the resin oiling agent 80.
  • the plasma surface treatment module 40 is provided with at least one plasma generator 41 for generating a plasma gas flow.
  • the plasma surface treatment module 40 is provided with at least one plasma generator 41 disposed at the upper and lower positions of the carbon fiber drag route respectively for generating a plasma gas flow to act on the surface of the carbon fiber 70B.
  • the surface of the carbon fiber can be roughened and provided with the functional groups by the plasma surface treatment step, which is beneficial to enhance the interface bonding of the resin oiling agent and the carbon fiber in the subsequent sizing step.
  • the structure of the carbon fiber is more stable and reliable to improve the quality of the carbon fiber, thereby accelerating the overall production speed of the carbon fiber.
  • the microwave focusing heating way the same apparatus can be applied to a carbon fiber precursor fiber bundle whose surface has not been processed with a pre-oxidation treatment or a carbon fiber precursor fiber bundle whose surface has been processed with a pre-oxidation treatment in advance.
  • the apparatus can be used to produce general carbon fibers or high modulus carbon fibers (graphite fibers) so as reduce the cost of the carbon fiber production equipment and the working time effectively.

Abstract

A carbon fiber manufacturing method and a carbon fiber manufacturing apparatus are provided. A carbon fiber precursor fiber bundle (70A) is performed with a high-temperature carbonization step to form a carbon fiber (70B), and then the carbon fiber (70B) is performed with a plasma surface treatment so that the surface of the carbon fiber (70B) is formed with a plasma-modified configuration (71) which is relatively rougher. Finally, the surface of the carbon fiber (70B) is coated with a resin oiling agent (80) to obtain the carbon fiber (70B) having the resin oiling agent (80) thereon. Particularly, through a plasma surface treatment step, the surface of the carbon fiber (70B) is roughened and provided with functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent (80) and the carbon fiber (70B). The structure of the carbon fiber (70B) is more stable and reliable. The cost of the carbon fiber production equipment and the working time can be reduced effectively.

Description

    FIELD OF THE INVENTION
  • The present invention relates to a carbon fiber manufacturing technique, and more particularly to a carbon fiber manufacturing method and a carbon fiber manufacturing apparatus which can greatly improve the sizing quality of a carbon fiber and effectively reduce the cost of the carbon fiber production equipment and the working time.
  • BACKGROUND OF THE INVENTION
  • Carbon fibers are classified into carbon fibers or graphite fibers according to their carbon contents, which have excellent mechanical properties and electrical properties and can be widely used in various applications. A conventional carbon fiber is achieved by bundling precursor fibers, such as polyacrylonitrile fibers, to form a carbon fiber precursor fiber bundle, and then the carbon fiber precursor fiber bundle is calcined (high-temperature carbonization) to form the carbon fiber.
  • There are various precursor fibers of carbon fibers on the market, such as rayon, poly vinyl alcohol, vinylidene chloride, polyacrylonitrile (PAN), pitch, and the like. In general, polyacrylonitrile (PAN) is used as the raw material of carbon fibers. The manufacturing steps are generally as follows: PAN raw material (precursor fiber) → pre-oxidation → high-temperature carbonization → surface treatment → sizing.
  • In the carbonization step, the carbon fiber precursor fiber bundles are heated to form carbon fibers or graphite fibers by different heating apparatuses according to the application of the carbon fibers. In principle, the carbon content of the fibers of graphite fibers is 90% or more, forming a two-dimensional carbocyclic planar net structure and a graphite layer structure having parallel layers. The results show that the crystalline region of a high-strength carbon fiber is composed of 5-6 graphite layers, and the crystalline region of a high-strength and high-modulus carbon fiber is composed of 10-20 graphite layers. Theoretically and practically, it is pointed out that the larger the crystalline thickness of the graphite layer is, the higher the tensile modulus of the carbon fiber is.
  • On the other hand, the surface of the carbon fiber after the high-temperature carbonization step is usually coated with a layer of oiling agent (a resin oiling agent is generally used, it is called as a sizing step) before it leaves the factory. The layer of oiling agent is used to protect the fiber from breakage due to friction in the subsequent step to affect the overall quality of the carbon fiber. The surfaces of untreated carbon fibers adsorb impurities thereon. Since these impurities are present between the surface of the carbon fiber and the resin oiling agent, the adhesion between the carbon fiber and the resin oiling agent is insufficient, and the purpose of protecting the fiber cannot be achieved
  • Furthermore, in the high-temperature carbonization step, the surface of the carbon fiber is excessively finely formed due to high-temperature sintering, and there are few functional groups on the surface. As a result, the fiber and the resin oiling agent cannot be bonded fully in the sizing step. It is known that a heat treatment or electrolysis technique can be applied to the surface treatment of the fiber after the high-temperature carbonization step, and then the sizing step is performed in order to improve the bonding of the fiber and the resin oiling agent.
  • However, when the surface treatment of the carbon fiber is performed by means of heat treatment, the carbon fiber is treated at a temperature in the range of 500°C to 800°C for 1-10 minutes. A relatively long period of time is required. Besides, the heat treatment is always performed with a large number of fibers at a time, so it is difficult to control the processing quality. When the surface treatment of the carbon fiber is performed by means of electrolysis, at least one drying process is required before the surface of the fiber is coated with the oiling agent. This also takes more time. Moreover, a change of the electrolyte may affect the processing quality. Even the surface of the fiber may have depositions.
  • Accordingly, the inventor of the present invention has devoted himself based on his many years of practical experiences to solve these problems.
  • SUMMARY OF THE INVENTION
  • In view of the problems of the prior art, the primary object of the present invention is to provide a carbon fiber manufacturing method which can greatly improve the sizing quality of a carbon fiber and effectively reduce the cost of the carbon fiber production equipment and the working time.
  • In order to achieve the forgoing object, the carbon fiber manufacturing method of the present invention comprises providing a raw material step, providing a carbon fiber precursor fiber bundle; performing a high-temperature carbonization step, the carbon fiber precursor fiber bundle being heated to form a carbon fiber having a predetermined carbon content; performing a plasma surface treatment step, a plasma gas flow with a predetermined power being provided to act on the carbon fiber at a predetermined time so that a surface of the carbon fiber is formed with a plasma-modified configuration; performing a sizing step, the plasma-modified configuration being coated with a resin oiling agent; and performing a drying step, the resin oiling agent coated on the plasma-modified configuration being processed with drying so that the resin oiling agent is firmly adhered to the surface of the carbon fiber.
  • In the carbon fiber manufacturing method of the present invention, through the plasma surface treatment step, the surface of the carbon fiber is roughened and provided with functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent and the carbon fiber in the subsequent sizing step so as to improve the sizing quality of the carbon fiber greatly. The structure of the carbon fiber is more stable and reliable. The plasma surface treatment belongs to a dry-type and fast surface treatment technique to effectively reduce the cost of the carbon fiber production equipment and the working time.
  • Preferably, in the high-temperature carbonization step, the carbon fiber precursor fiber bundle is guided into a chamber. The chamber is formed with at least one microwave field concentration area therein, and is provided with a gas supply assembly to supply an inert gas and a microwave generating assembly to supply a high-frequency microwave. Under the protection of the inert gas atmosphere, the electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle passing through the microwave field concentration area.
  • Preferably, the chamber is provided with at least one pair of microwave-sensitive materials.
  • Preferably, the microwave-sensitive materials are one of graphite, carbide, magnetic compound, nitride, and ionic compound or a combination thereof.
  • Preferably, the inert gas is nitrogen, argon, helium, or a combination thereof.
  • Preferably, the frequency of the high-frequency microwave is in the range of 300-30,000 MHz, and its microwave power density is in the range of 1-1000kW/m3.
  • Preferably, the chamber is an elliptic chamber.
  • Alternatively, the chamber is a flat panel chamber.
  • Preferably, in the plasma surface treatment step, the plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • Alternatively, in the plasma surface treatment step, an atmospheric plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • Alternatively, in the plasma surface treatment step, a low-pressure plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • Alternatively, in the plasma surface treatment step, a microwave plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • Alternatively, in the plasma surface treatment step, a glow plasma gas flow with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
  • Preferably, the carbon fiber precursor fiber bundle has a surface not processed with a pre-oxidation treatment.
  • Alternatively, the carbon fiber precursor fiber bundle has a surface processed with a pre-oxidation treatment in advance.
  • Preferably, the resin oiling agent is a thermosetting resin oiling agent.
  • Alternatively, the resin oiling agent is a thermoplastic resin oiling agent.
  • Preferably, the carbon content of the carbon fiber is in the range of 80%-90%.
  • In order to achieve the forgoing object, the carbon fiber manufacturing apparatus of the present invention comprises a feeding module, a receiving module, a high-temperature carbonization module, a plasma surface treatment module, and a sizing module. The receiving module is disposed in the vicinity of the feeding module. The feeding module and the receiving module constitute a carbon fiber drag route. The high-temperature carbonization module is disposed at the carbon fiber drag route and located between the feeding module and the receiving module for heating the carbon fiber drag route. The plasma surface treatment module is disposed at the carbon fiber drag route and located between the high-temperature carbonization module and the receiving module for supplying a plasma gas flow to the carbon fiber drag route. The sizing module is disposed at the carbon fiber drag route and located between the plasma surface treatment module and the receiving module for coating a resin oiling agent on the surface of a carbon fiber.
  • Thereby, the carbon fiber manufacturing apparatus of the present invention can be operated in the integrated operation of the feeding module, the high-temperature carbonization module, the plasma surface treatment module, the sizing module, and the receiving module. A carbon fiber precursor fiber bundle released from the feeding module is sequentially processed at a predetermined speed to perform the steps of high-temperature carbonization, plasma surface treatment, sizing, and so on, in a relatively more active and reliable manner. The carbon fiber precursor fiber bundle is heated to form the carbon fiber, and then the surface of the carbon fiber is formed with the resin oiling agent. Particularly, through the plasma surface treatment module, the surface of the carbon fiber is roughened and provided with functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent and the carbon fiber in the subsequent sizing procedure so as to improve the sizing quality of the carbon fiber greatly. The structure of the carbon fiber is more stable and reliable. The plasma surface treatment belongs to a dry-type and fast surface treatment technique to effectively reduce the cost of the carbon fiber production equipment and the working time.
  • Preferably, the high-temperature carbonization module has a chamber for the carbon fiber drag route or the carbon fiber precursor fiber bundle to pass therethrough. The chamber is formed with at least one microwave field concentration area and supplies an inert gas and a high-frequency microwave. Under the protection of the inert gas atmosphere, the electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle passing through the microwave field concentration area.
  • Preferably, the high-temperature carbonization module has a chamber for the carbon fiber drag route or the carbon fiber precursor fiber bundle to pass therethrough. The chamber is formed with at least one microwave field concentration area and provided with a gas supply assembly to supply an inert gas and a microwave generating assembly to supply a high-frequency microwave. Under the protection of the inert gas atmosphere, the electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle passing through the microwave field concentration area. The plasma surface treatment module is provided with at least one plasma generator.
  • Preferably, the plasma surface treatment module is provided with at least one plasma generator located at upper and lower positions of the carbon fiber drag route, respectively.
  • Preferably, the chamber is an elliptic chamber.
  • Preferably, the chamber is an elliptic chamber, and the chamber is provided with at least one pair of microwave-sensitive materials.
  • Alternatively, the chamber is a flat plate chamber.
  • Alternatively, the chamber is a flat plate chamber, and the chamber is provided with at least one pair of microwave-sensitive materials.
  • Preferably, the plasma generator is able to generate the plasma gas flow having a power in the range of 100-10000 Watts.
  • Alternatively, the plasma generator is able to generate an atmospheric plasma gas flow having a power in a range of 100-10000 Watts.
  • Alternatively, the plasma generator is able to generate a low-pressure plasma gas flow having a power in the range of 100-10000 Watts.
  • Alternatively, the plasma generator is able to generate a microwave plasma gas flow having a power in the range of 100-10000 Watts.
  • Alternatively, the plasma generator is able to generate a glow plasma gas flow having a power in the range of 100-10000 Watts.
  • Preferably, the sizing module is provided with at least one reservoir.
  • Preferably, the carbon fiber manufacturing apparatus further comprises a drying module. The drying module is disposed at the carbon fiber drag route between the sizing module and the receiving module for the resin oiling agent to be adhered to the surface of the carbon fiber firmly.
  • Specifically, through plasma surface treatment, the surface of the carbon fiber can be roughened and provided with the functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent and the carbon fiber in the subsequent sizing step. The structure of the carbon fiber is more stable and reliable. By the microwave focusing heating way, the same apparatus can be applied to a carbon fiber precursor fiber bundle whose surface has not been processed with a pre-oxidation treatment or a carbon fiber precursor fiber bundle whose surface has been processed with a pre-oxidation treatment in advance. By simply adjusting the microwave power, the apparatus can be used to produce general carbon fibers or high modulus carbon fibers (graphite fibers) so as reduce the cost of the carbon fiber production equipment and the working time effectively.
  • BRIEF DESCRIPTION OF THE DRAWINGS
    • FIG. 1 is a flow diagram of a carbon fiber manufacturing method of the present invention;
    • FIG. 2 is a structural schematic view of a high-temperature carbonization module in accordance with an embodiment of the present invention;
    • FIG. 3 is a sectional schematic view of a carbon fiber after finishing a plasma surface treatment step of the present invention;
    • FIG. 4 is a sectional schematic view of a carbon fiber after finishing a sizing step of the present invention;
    • FIG. 5 is a structural schematic view of a high-temperature carbonization module in accordance with another embodiment of the present invention;
    • FIG. 6a illustrates a SEM image of an object to be tested without plasma treatment; and
    • FIG. 6b illustrates a SEM image of an object to be tested with the plasma treatment.
    • FIG. 7 is a structural schematic view of a carbon fiber manufacturing apparatus in accordance with a first embodiment of the present invention; and
    • FIG. 8 is a structural schematic view of a carbon fiber manufacturing apparatus in accordance with a second embodiment of the present invention.
    DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • Embodiments of the present invention will now be described, by way of example only, with reference to the accompanying drawings.
  • The present invention discloses a carbon fiber manufacturing method which can greatly improve the sizing quality of carbon fibers and effectively reduce the cost of the carbon fiber production equipment and the working time. As shown in FIG. 1, the carbon fiber manufacturing method of the present invention comprises providing a raw material step, performing a high-temperature carbonization step, performing a plasma surface treatment step, and performing a sizing step. The carbon fiber manufacturing method further comprises performing a drying step after the sizing step. Referring to FIG. 1 through FIG. 5, the steps are described in details as below.
  • In the step of providing the raw material, a carbon fiber precursor fiber bundle is provided to be processed to form a carbon fiber. In practice, the carbon fiber precursor fiber bundle may be formed of rayon, poly vinyl alcohol, vinylidene chloride, polyacrylonitrile (PAN), pitch, and the like. The surface of the carbon fiber precursor fiber bundle may have not been processed with a pre-oxidation treatment or have been processed with a pre-oxidation treatment in advance.
  • In the high-temperature carbonization step, the carbon fiber precursor fiber bundle is heated to form the carbon fiber having a predetermined carbon content. In practice, as shown in FIG. 2, the carbon fiber precursor fiber bundle 70A is guided into a chamber 31 of a high-temperature carbonization module 30. The chamber 31 is formed with at least one microwave field concentration area 311 therein, and is provided with a gas supply assembly 32 to supply an inert gas and a microwave generating assembly 33 to supply a high-frequency microwave. Under the protection of the inert gas atmosphere, the electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle 70A passing through the microwave field concentration area 311, enabling the carbon fiber precursor fiber bundle to form the carbon fiber 70B having a predetermined carbon content. The carbon content of the carbon fiber 70B is in the range of 80%-90%.
  • In the plasma surface treatment step, a plasma gas flow with a predetermined power is provided to act on the carbon fiber 70B at a predetermined time, such that the surface of the carbon fiber 70B is formed with a plasma-modified configuration 71, shown in FIG. 3, which is rougher or has more functional groups relative to the carbon fiber precursor fiber bundle 70A.
  • In the sizing step, the plasma-modified configuration 71 on the surface of the carbon fiber 70B is coated with a resin oiling agent 80, so that the surface of the carbon fiber 70B has the resin oiling agent 80, as shown in FIG. 4. In practice, the resin oiling agent 80 is coated on the surface of the carbon fiber 70B by soaking or immersing. The resin oiling agent 80 may be a thermosetting resin oiling agent or a thermoplastic resin oiling agent.
  • In the drying step, a drying treatment is applied to the resin oiling agent 80 coated on the plasma-modified configuration 71 so that the resin oiling agent 80 is firmly adhered to the surface of the carbon fiber 70B. In practice, the drying treatment is carried out by ultraviolet irradiation, cooling, drying or air-drying for the resin oiling agent to be bonded to the surface of the carbon fiber.
  • In the plasma surface treatment step, an atmospheric plasma gas flow, a low-pressure plasma gas flow, a microwave plasma gas flow, or a glow plasma gas flow with a power of 100-10000 watts may be used to act on the carbon fiber 10B for 10-1000 milliseconds. Since the plasma gas flow contains particles having energy, the impurities that originally adhere to the surface of the carbon fiber 10B can be broken to form small molecules by the impact of the plasma gas flow through the physical reaction (collision) of the plasma gas flow, and then the small molecules are blown away from the surface of the carbon fiber 70B by the air flow, so that the surface of the carbon fiber 70B is clean. In the sizing step, the resin oiling agent 80 can be completely in contact with the carbon fiber 70B to increase the bonding effect. In addition, the impact of the plasma gas flow will also form the plasma-modified configuration 71 on the surface of the carbon fiber 70B. The plasma-modified configuration 71 is rougher relative to the carbon fiber precursor fiber bundle 70A, and is further formed with pores. The surface of the carbon fiber 70B is roughened or formed with the pores, which is beneficial to increase the contact area between the resin oiling agent 80 and the carbon fiber 70B in the subsequent sizing step. The resin oiling agent 80 penetrates into the pores, and the resin oiling agent 80 is anchored between the pores to form an anchor effect to enhance the bonding effect of the resin oiling agent 80 and the carbon fiber 70B.
  • The plasma gas flow also makes the surface of the carbon fiber 70B generate a chemical reaction at the same time, so that at least one functional group (such as -OH, -N, etc.) is added to the surface of the carbon fiber 70B. In the sizing step, the surface tension of the surface of the carbon fiber 70B is increased due to the presence of the functional group, which is beneficial to improve the wetting effect for the resin oiling agent 80 to be coated on the carbon fiber 70B. That is, the contact angle of the resin oiling agent 80 to the carbon fiber 70B becomes small, so that the resin oiling agent 80 can be quickly or instantaneously coated on the carbon fiber 70B, and the speed of the sizing step is increased, thereby accelerating the overall production speed of the carbon fiber 70B. The presence of the functional group such as the OH group reacts with the resin oiling agent 80, such as epoxy resin (Epoxy), to generate hydrogen bonding, thereby increasing the bonding effect.
  • Thereby, in the carbon fiber manufacturing method of the present invention, through the plasma surface treatment step, the surface of the carbon fiber 70B is roughened and provided with functional groups, which is beneficial to enhance the interface bonding of the resin oiling agent 80 and the carbon fiber 70B in the subsequent sizing step so as to improve the sizing quality of the carbon fiber 70B greatly. The structure of the carbon fiber is more stable and reliable. The plasma surface treatment belongs to a dry-type and fast surface treatment technique to effectively reduce the cost of the carbon fiber production equipment and the working time.
  • Furthermore, the foregoing inert gas may be nitrogen, argon, helium, or a combination thereof. The frequency of the high-frequency microwave may be in the range of 300-30,000 MHz, and its microwave power density may be in the range of 1-1000kW/m3.
  • In the embodiment as shown in FIG. 2, the chamber 31 of the high-temperature carbonization module 30 may be an elliptic chamber, or the chamber 31 may be a flat plate chamber as shown in FIG. 5. As shown in FIG. 5, whatever the chamber 31 is, the chamber 31 is provided with a pair of microwave-sensitive materials 34 therein, thereby enhancing the focusing effect on the microwave field in order to further accelerate the high-temperature carbonization process. In practice, the microwave-sensitive materials 34 may be one of graphite, carbide, magnetic compound, nitride, and ionic compound or a combination thereof.
  • Due to the resonant effect of microwave heating, the carbonization of the carbon fiber is enhanced rapidly and more crystalline carbons are formed and stacked, which leads to the formation of larger graphite crystalline molecules, namely, larger graphite crystalline thickness, while deriving a higher microwave induction heating effect is derived. Such a cycle generates an autocatalytic reaction, enabling the carbon fiber to be rapidly heated to the graphitization temperature (1500- 3000°C), and carbon atoms are reconstructed and rearranged more rapidly to form a graphite layer.
  • In other words, the same apparatus can be applied to a carbon fiber precursor fiber bundle whose surface has not been processed with a pre-oxidation treatment or a carbon fiber precursor fiber bundle whose surface has been processed with a pre-oxidation treatment in advance. It is only necessary to adjust the microwave power for the production, the apparatus can be used to produce general carbon fibers (1000-1500°C) or high modulus carbon fibers (graphite fibers).
  • In a preferred embodiment, an object to be tested that the resin oiling agent after the drying step is firmly adhered to the surface of the carbon fiber, and the treatment conditions in the plasma surface treatment step are shown in Table 1 below: Table 1: the conditions of the plasma surface treatment
    plasma gas consumption N2 200 L/min
    CDA 0.4 L/min
    plasma gas amount 200.4 L/min
    plasma power 0∼1000 W
    plasma surface treatment time 0.025∼0.100 sec.
    carbon fiber yarn width 7 mm
    yarn per unit time receiving capacity 0.28 J/s
    distance 1 mm
  • The ILSS strength (interlayer bonding force) was measured for an object to be tested in an environment of a temperature of 23°C and a humidity of 50% RH by using an INSTRON measuring machine according to ASTM 2344, and the results are shown in Table 2 below: Table 2: the relationship between the plasma surface treatment power (W), the processing time (sec.), and the interlayer bonding force (MPa) (epoxy resin used as the resin oiling agent) of PAN carbon fiber 12K.
    plasma power (W) of surface treatment interlayer bonding force (ILSS)(MPa)
    0.025 sec. 0.075 sec. 0.100 sec.
    0(untreated) 70 70 70
    250 71 73 75
    500 73 76 81
    750 75 81 85
    900 79 86 88
    1000 83 89 91
  • As can be seen from Table 2, the carbon fiber without the plasma surface treatment, the interlayer bonding force of the object to be tested is only 70MPa. With an increase of the plasma power, for example, the processing time is 0.075 seconds and the plasma power is increased from the untreated (0W, without plasma power) to 1000W, the interlayer bonding force is increased from 70MPa to 89MPa. That is, the interlayer bonding force is increased to 127%.
  • In the sizing step, the epoxy resin is used as the resin oiling agent, and the carbon fiber is used as the carbon fiber 70B. FIG. 6a shows a SEM image of the object to be tested without the plasma treatment. FIG. 6b shows a SEM image of the object to be tested with the plasma treatment. As shown in FIG. 6a, the SEM image of the object to be tested without the plasma surface treatment illustrates a void H between the resin oiling agent 80 and the carbon fiber 70B because the surface of the carbon fiber 70B is smooth and doesn't have functional groups. The void H causes a decrease in the strength of the object to be tested. That is to say, the bonding force between the carbon fiber and the resin oiling agent is insufficient for protecting the fiber.
  • As shown in FIG. 6b, the SEM image of the object to be tested with the plasma surface treatment illustrates that there is no void between the resin oiling agent 80 and the carbon fiber 70B because the surface of the carbon fiber 70B is rough and has functional groups (such as -OH, -N, etc.). The resin oiling agent 80 and the carbon fiber 70B are bonded tightly, so that the strength of the object to be tested is enhanced. That is, the adhesion between the carbon fiber and the resin oiling agent is enhanced, so that the purpose of protecting the fiber can be achieved.
  • In order to implement the aforesaid carbon fiber manufacturing method, the present invention further discloses a carbon fiber manufacturing apparatus which can greatly improve the sizing quality of carbon fibers and effectively reduce the cost of the carbon fiber production equipment and the working time. As shown in FIG. 7, the carbon fiber manufacturing apparatus of the present invention comprises a feeding module 10, a receiving module 20, a high-temperature carbonization module 30, a plasma surface treatment module 40, and a sizing module 50.
  • The feeding module 10 is to perform the step of providing a raw material in the carbon fiber manufacturing method, and is used to supply a carbon fiber precursor fiber bundle 70A to be processed into a carbon fiber 70B.
  • The receiving module 20 is disposed in the vicinity of the feeding module 10, and corresponds to the feeding module 10 to constitute a carbon fiber drag route. The receiving module 20 includes a yarn winding assembly 21 to receive the carbon fiber 70B. The yarn winding assembly 21 performs a drag action on the carbon fiber 70B to be received.
  • The high-temperature carbonization module 30 is to perform the high-temperate carbonization step in the carbon fiber manufacturing method. The high-temperature carbonization module 30 is disposed at the carbon fiber drag route between the feeding module 10 and the receiving module 20 for heating the carbon fiber precursor fiber bundle 70A, enabling the carbon fiber precursor fiber bundle 70A to become the carbon fiber 70B having a predetermined carbon content.
  • The plasma surface treatment module 40 is to perform the plasma surface treatment step in the carbon fiber manufacturing method. The plasma surface treatment module 40 is disposed at the carbon fiber drag route between the high-temperature carbonization module 30 and the receiving module 20 to provide a plasma gas flow with a predetermined power to act on the carbon fiber 70B, such that the surface of the carbon fiber 70B is formed with a plasma-modified configuration 71 which is rougher or has more functional groups relative to the carbon fiber precursor fiber bundle 70A.
  • The sizing module 50 is to perform the sizing step in the carbon fiber manufacturing method. The sizing module 50 is disposed at the carbon fiber drag route between the plasma surface treatment module 40 and the receiving module 20 for the plasma-modified configuration 71 on the surface of the carbon fiber 70B to be coated with a resin oiling agent 80. The sizing module 50 is provided with at least one reservoir 51 for storing the resin oiling agent 80.
  • As shown in FIG. 8, the carbon fiber manufacturing apparatus of the present invention may further comprise a drying module 60. The drying module 60 is to perform the drying step in the carbon fiber manufacturing method. The drying module 60 is disposed at the carbon fiber drag route between the sizing module 50 and the receiving module 20 for the resin oiling agent 80 to be firmly adhered to the surface of the carbon fiber 70B. In practice, the drying module 60 is provided with at least one blast furnace 61 to generate hot blast.
  • Thereby, the carbon fiber manufacturing apparatus of the present invention can be operated in the integrated operation of the feeding module 10, the high-temperature carbonization module 30, the plasma surface treatment module 40, the sizing module 50, and the receiving module 20. The carbon fiber precursor fiber bundle 70A released from the feeding module 10 is sequentially processed at a predetermined speed to perform the steps of high-temperature carbonization, plasma surface treatment, sizing, and so on, in a relatively more active and reliable manner. The carbon fiber precursor fiber bundle 70A is heated to form the carbon fiber 70B, and then the surface of the carbon fiber 70B is formed with the resin oiling agent 80.
  • The plasma surface treatment module 40 is provided with at least one plasma generator 41 for generating a plasma gas flow. In an embodiment, the plasma surface treatment module 40 is provided with at least one plasma generator 41 disposed at the upper and lower positions of the carbon fiber drag route respectively for generating a plasma gas flow to act on the surface of the carbon fiber 70B.
  • Compared to the prior art, through the carbon fiber manufacturing method and the carbon fiber manufacturing apparatus of the present invention, the surface of the carbon fiber can be roughened and provided with the functional groups by the plasma surface treatment step, which is beneficial to enhance the interface bonding of the resin oiling agent and the carbon fiber in the subsequent sizing step. The structure of the carbon fiber is more stable and reliable to improve the quality of the carbon fiber, thereby accelerating the overall production speed of the carbon fiber. By the microwave focusing heating way, the same apparatus can be applied to a carbon fiber precursor fiber bundle whose surface has not been processed with a pre-oxidation treatment or a carbon fiber precursor fiber bundle whose surface has been processed with a pre-oxidation treatment in advance. By simply adjusting the microwave power, the apparatus can be used to produce general carbon fibers or high modulus carbon fibers (graphite fibers) so as reduce the cost of the carbon fiber production equipment and the working time effectively.
  • Although particular embodiments of the present invention have been described in detail for purposes of illustration, various modifications and enhancements may be made without departing from the spirit and scope of the present invention. Accordingly, the present invention is not to be limited except as by the appended claims.

Claims (25)

  1. A carbon fiber manufacturing method, comprising:
    providing a raw material step, providing a carbon fiber precursor fiber bundle (70A);
    performing a high-temperature carbonization step, the carbon fiber precursor fiber bundle (70A) being heated to form a carbon fiber (70B) having a predetermined carbon content;
    performing a plasma surface treatment step, a plasma gas flow with a predetermined power being provided to act on the carbon fiber (70B) at a predetermined time so that a surface of the carbon fiber (70B) is formed with a plasma-modified configuration (71);
    performing a sizing step, the plasma-modified configuration (71) being coated with a resin oiling agent (80); and
    performing a drying step, the resin oiling agent (80) coated on the plasma-modified configuration (71) being processed with drying so that the resin oiling agent (80) is firmly adhered to the surface of the carbon fiber (70B).
  2. The carbon fiber manufacturing method as claimed in claim 1, wherein in the high-temperature carbonization step, the carbon fiber precursor fiber bundle (70A) is guided into a chamber (31), the chamber (31) is formed with at least one microwave field concentration area (311) therein and is provided with a gas supply assembly (32) to supply an inert gas and a microwave generating assembly (33) to supply a high-frequency microwave, under the protection of the inert gas atmosphere, an electric field of the high-frequency microwave produces a sensing current to heat up and produce a high temperature quickly with the carbon fiber precursor fiber bundle (70A) passing through the microwave field concentration area (311).
  3. The carbon fiber manufacturing method as claimed in claim 2, wherein the chamber (31) is provided with at least one pair of microwave-sensitive materials (34).
  4. The carbon fiber manufacturing method as claimed in claim 3, wherein the microwave-sensitive materials (34) are one of graphite, carbide, magnetic compound, nitride, and ionic compound or a combination thereof.
  5. The carbon fiber manufacturing method as claimed in claim 2, wherein the inert gas is nitrogen, argon, helium, or a combination thereof.
  6. The carbon fiber manufacturing method as claimed in claim 2, wherein the frequency of the high-frequency microwave is in the range of 300-30,000 MHz, and its microwave power density is in the range of 1-1000kW/m3.
  7. The carbon fiber manufacturing method as claimed in claim 2, wherein the chamber (31) is an elliptic chamber.
  8. The carbon fiber manufacturing method as claimed in claim 2, wherein the chamber (31) is a flat panel chamber.
  9. The carbon fiber manufacturing method as claimed in claim 1, wherein in the plasma surface treatment step, the plasma gas flow, an atmospheric plasma gas flow, a low-pressure plasma gas flow, a microwave plasma gas flow, or a glow plasma gas flow with a power of 100-10000 watts acts on the carbon fiber (70B) for 10-1000 milliseconds.
  10. The carbon fiber manufacturing method as claimed in claim 1, wherein the carbon fiber precursor fiber bundle (70A) has a surface not processed with a pre-oxidation treatment.
  11. The carbon fiber manufacturing method as claimed in claim 1, wherein the carbon fiber precursor fiber bundle (70A) has a surface processed with a pre-oxidation treatment in advance.
  12. The carbon fiber manufacturing method as claimed in claim 1, wherein the resin oiling agent (80) is a thermosetting resin oiling agent.
  13. The carbon fiber manufacturing method as claimed in claim 1, wherein the resin oiling agent (80) is a thermoplastic resin oiling agent.
  14. The carbon fiber manufacturing method as claimed in claim 1, wherein the carbon content of the carbon fiber (70B) is in the range of 80%-90%.
  15. A carbon fiber manufacturing apparatus, comprising:
    a feeding module (10) and a receiving module (20), the receiving module (20) being disposed in the vicinity of the feeding module (10), the feeding module (10) and the receiving module (20) constituting a carbon fiber drag route;
    a high-temperature carbonization module (30), disposed at the carbon fiber drag route and located between the feeding module (10) and the receiving module (20) for heating the carbon fiber drag route;
    a plasma surface treatment module (40), disposed at the carbon fiber drag route and located between the high-temperature carbonization module (30) and the receiving module (20) for supplying a plasma gas flow to the carbon fiber drag route; and
    a sizing module (50), disposed at the carbon fiber drag route and located between the plasma surface treatment module (40) and the receiving module (20).
  16. The carbon fiber manufacturing apparatus as claimed in claim 15, wherein the high-temperature carbonization module (30) has a chamber (31), a gas supply assembly (32), and a microwave generating assembly (33), the carbon fiber drag route passes through the chamber (31), the gas supply assembly (32) is used to supply an inert gas, and the microwave generating assembly (33) is used to supply a high-frequency microwave.
  17. The carbon fiber manufacturing apparatus as claimed in claim 16, wherein the plasma surface treatment module (40) is provided with at least one plasma generator (41).
  18. The carbon fiber manufacturing apparatus as claimed in claim 16, wherein the plasma surface treatment module (40) is provided with at least one plasma generator (41) located at upper and lower positions of the carbon fiber drag route, respectively.
  19. The carbon fiber manufacturing apparatus as claimed in claim 16, wherein the chamber (31) is an elliptic chamber.
  20. The carbon fiber manufacturing apparatus as claimed in claim 19, wherein the chamber (31) is provided with at least one pair of microwave-sensitive materials (34).
  21. The carbon fiber manufacturing apparatus as claimed in claim 16, wherein the chamber (31) is a flat plate chamber.
  22. The carbon fiber manufacturing apparatus as claimed in claim 21, wherein the chamber is provided with at least one pair of microwave-sensitive materials (34).
  23. The carbon fiber manufacturing apparatus as claimed in claim 17, wherein the plasma generator is able to generate the plasma gas flow, an atmospheric plasma gas flow, a low-pressure plasma gas flow, a microwave plasma gas flow, or a glow plasma gas flow having a power in the range of 100-10000 watts.
  24. The carbon fiber manufacturing apparatus as claimed in claim 15, wherein the sizing module (50) is provided with at least one reservoir (51).
  25. The carbon fiber manufacturing apparatus as claimed in claim 15, further comprising a drying module (60), the drying module (60) being disposed at the carbon fiber drag route between the sizing module (50) and the receiving module (20).
EP17000054.1A 2017-01-12 2017-01-12 Carbon fiber manufacturing method and carbon fiber manufacturing apparatus Active EP3348684B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP17000054.1A EP3348684B1 (en) 2017-01-12 2017-01-12 Carbon fiber manufacturing method and carbon fiber manufacturing apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP17000054.1A EP3348684B1 (en) 2017-01-12 2017-01-12 Carbon fiber manufacturing method and carbon fiber manufacturing apparatus

Publications (2)

Publication Number Publication Date
EP3348684A1 true EP3348684A1 (en) 2018-07-18
EP3348684B1 EP3348684B1 (en) 2020-07-29

Family

ID=57984755

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17000054.1A Active EP3348684B1 (en) 2017-01-12 2017-01-12 Carbon fiber manufacturing method and carbon fiber manufacturing apparatus

Country Status (1)

Country Link
EP (1) EP3348684B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113338027A (en) * 2021-05-12 2021-09-03 北京化工大学 Surface treatment method of carbon fiber

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104342936A (en) * 2013-07-26 2015-02-11 永虹科技股份有限公司 Carbon-fiber surface oiling agent replacing method
US20160257797A1 (en) * 2012-02-28 2016-09-08 Ut-Battelle, Llc Method of improving adhesion of carbon fibers with a polymeric matrix

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160257797A1 (en) * 2012-02-28 2016-09-08 Ut-Battelle, Llc Method of improving adhesion of carbon fibers with a polymeric matrix
CN104342936A (en) * 2013-07-26 2015-02-11 永虹科技股份有限公司 Carbon-fiber surface oiling agent replacing method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113338027A (en) * 2021-05-12 2021-09-03 北京化工大学 Surface treatment method of carbon fiber

Also Published As

Publication number Publication date
EP3348684B1 (en) 2020-07-29

Similar Documents

Publication Publication Date Title
EP2679619B1 (en) Fiber reinforced composite material
US6514449B1 (en) Microwave and plasma-assisted modification of composite fiber surface topography
KR102461416B1 (en) Surface-treated carbon fiber, surface-treated carbon fiber strand, and manufacturing method therefor
CN1053170C (en) Process for a surface treatment of a glass fabric
EP2781538B1 (en) Fiber-reinforced composite material and process for producing fiber-reinforced composite material
US20180179696A1 (en) Carbon fiber manufacturing method
EP3348684B1 (en) Carbon fiber manufacturing method and carbon fiber manufacturing apparatus
US20180179697A1 (en) Carbon fiber manufacturing apparatus
JP2755431B2 (en) Carbon fiber reinforced carbon composite material
KR102351904B1 (en) glass cloth
Chen et al. Improvement of interfacial adhesion for plasma‐treated aramid fiber‐reinforced poly (phthalazinone ether sulfone ketone) composite and fiber surface aging effects
CN105332098A (en) Carbon fiber activation process
JP2018115395A (en) Method for producing carbonized fiber
Jin et al. Properties of carbon fibers modified by oxygen plasma
CN108149483A (en) Carbon fibre manufacturing method
Skundric et al. Wetting properties of hemp fibres modified by plasma treatment
TWI663124B (en) Carbon fiber manufacturing method
TWM538950U (en) Carbide fiber manufacturing equipment
JP3209600U (en) Carbonized fiber manufacturing equipment
JP3682849B2 (en) Method for producing metal carbon fiber composite
JP2017137603A (en) Carbon fiber, manufacturing method of carbon fiber with sizing agent adhered
US20090098307A1 (en) Manufacturing method for far-infrared irradiating substrate
Safitri et al. Wettability comparison of argon and oxygen plasma treatment for coconut fiber with 2 MHZ RF plasma system
KR930009307B1 (en) Forming method for metalic complex materials
CN105839389A (en) Processing method of carbon fiber weaving fabric

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20180426

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20190718

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602017020368

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: D01F0009220000

Ipc: D01D0010000000

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: D06M 101/40 20060101ALI20200213BHEP

Ipc: D01D 10/00 20060101AFI20200213BHEP

Ipc: D01F 9/20 20060101ALI20200213BHEP

Ipc: D01F 9/32 20060101ALI20200213BHEP

INTG Intention to grant announced

Effective date: 20200227

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1295898

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200815

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602017020368

Country of ref document: DE

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20200729

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1295898

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200729

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201029

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201030

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201130

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201029

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201129

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602017020368

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

26N No opposition filed

Effective date: 20210430

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602017020368

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20210112

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210112

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20210131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210131

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210803

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210112

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210112

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200729

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20170112