EP0024277A1 - Process for the manufacture of graphite fibres - Google Patents
Process for the manufacture of graphite fibres Download PDFInfo
- Publication number
- EP0024277A1 EP0024277A1 EP79301690A EP79301690A EP0024277A1 EP 0024277 A1 EP0024277 A1 EP 0024277A1 EP 79301690 A EP79301690 A EP 79301690A EP 79301690 A EP79301690 A EP 79301690A EP 0024277 A1 EP0024277 A1 EP 0024277A1
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- EP
- European Patent Office
- Prior art keywords
- fibre
- heating
- temperature
- process according
- furnace
- 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.)
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Classifications
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F9/00—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
- D01F9/08—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
- D01F9/12—Carbon filaments; Apparatus specially adapted for the manufacture thereof
- D01F9/14—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
- D01F9/32—Apparatus therefor
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F9/00—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
- D01F9/08—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
- D01F9/12—Carbon filaments; Apparatus specially adapted for the manufacture thereof
- D01F9/14—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
- D01F9/20—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products
- D01F9/21—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
- D01F9/22—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from polyacrylonitriles
Definitions
- Graphite fibres are generally different from carbon fibres in respect of carbon content (purity), structure and physical characteristics. Graphite fibres are preferable to carbon fibres for use in sports equipment such as fishing rods and golf club shafts which require high modulus, for use in electric components such as heaters which require high purity and low resistivity, and for use in the aerospace industry, where parts for aircraft, rockets etc., may have to have high oxidation resistivity and be made to high precision.
- graphite fibres cost much more than carbon fibres and this high cost is largely a result of difficulties in manufacturing processability and productivity. An inert atmosphere is required for production of graphite fibres, and a higher temperature is used than for carbon fibres.
- a process for the manufacture of graphite fibre by graphitizing precursor fibre characterised in that the precursor fibre or fibres pass successively through separately controllable first and second heating zones, both containing an inert atmosphere, the temperature at the hottest point in the said first heating zone being in the range of about 1500°C to about 2l00 o C, and the temperature at the hottest part in the said second heating zone being at least about 2100°C.
- graphite fibre as used herein is intended to mean a fibre which is obtained by heating a graphitizable precursor fibre in an inert atmosphere at a temperatue of about 2100°C, or more and which fibre contains about 95% or more by weight of carbon.
- graphitizable precursor fibre or “precursor fibre” is intended to mean a fibre which has sufficient structural integrity to maintain its fibrous character and which can be converted to a graphite fibre when heated in an inert atmosphere at a temperature of about 2100 o C or more.
- a typical example of a precursor fibre is an oxidized fibre obtained by heating an acrylic fibre, a cellulosic fibre (rayon), a polyvinylalcohol fibre or a pitch fibre in an oxidizing atmosphere at a temperature of about 200°C to 400°C.
- Another typical example is a carbon fibre obtained by heating the said oxidized fibre in an inert atmosphere at a temperature above about 400°C.
- a precursor fibre obtained from an acrylic fibre comprising about 95 mol % minimum of acrylonitrile (AN) and up to about 5 mol % of one or more ethylene-type vinyl compounds which are copolymerizable with acrylonitrile.
- the maximum temperature in the first heating zone is preferably in the range of 1700°Cto 1900°C.
- the second heating zone preferably has a maximum temperature in the range of 2100°C to 3500°C, more preferably in the range of 2300°C to 2700°C.
- the quality of the fibre produced is influenced by such things as the type of precursor fibre, whether it was pretreated or not, and the temperature profile of the heating zone; in some instances it is especially sensitive to the maximum temperature of the first heating zone and is reduced if this exceeds about 2100°C. In particular, the fibres tend to develop excessive surface fuzz and tend to break easily.
- the rate of heating of the precursor fibre as it passes through the heating zones is preferably within the range of 300°C/min to 2000°C/min in the first heating zone, more preferably within the range of 500°C/min to 1500°C/min, and preferably within the range of 2000°C/min to 10,000°C/min in the second heating zone.
- the treatment time of the precursor fibres in the first heating zone which is defined as the time during which the fibres are in the zone at a temperature above 1000°C. is preferably within the range of 10 seconds to 10 minutes, more preferably 30 seconds to 3 minutes.
- the separate first and second heating zones have respectively furnace tubes (2,3) to which heat is applied in a conventional way.
- the furnace tubes (2,3) are surrounded with insulation (4,5).
- An inert gas such as nitrogen is supplied to the furnaces (I,II) through pipes (6), and the gas is removed from the furnaces by pipes (7).
- furnace seals (8) supplied with inert gas through supply pipes (9).
- the precursor fibre (1) is first conducted through the seal (-8) into the furnace tube (2) of the furnace (1) which provides the first heating zone.
- the temperature profile inside this furnace tube (2) is controlled, to produce a profile as shown in Fig. 2. This is done by locally controlling the heat input at selected spots along the tube (2), in a conventional way.
- the precursor fibre is a carbon fibre, it is treated in this furnace until its weight is reduced to about 93% to 95% of its previous weight, and then it is conducted into the furnace tube (3) of the furnace (II) which provides the second heating zone. There the fibre is heated again, and is converted into a graphite fibre.
- Fig. 3 shows a typical temperature profile of the furnace tube (3) of the second heating zone, the maximum temperature of which is set at about 2500°C in this case.
- Carbon fibres were produced from acrylic fibres and carbonized in an inert atmosphere, the maximum temperature of which was 1100°C. They were taken from creels and heated to produce graphite fibres using separate furnaces as shown in Fig. 1. The conditions were varied, there being 3 conditions within the scope of the invention (Examples 1-3) and four conditions outside the scope of the invention (Comparative Examples 1-4). The conditions are shown in Table 1. The resulting data are shown in Table 2. Moreover, the usual temperatures, the periods of time between changes of furnace tubes and the number of days required to change them, with respect to both first and second furnaces, are shown in Table 3. Some of the properties of the fibres made in these examples are shown in Table 2.
- Table 3 gives an indication of the lifetime of the furnace tubes, at different operating temperatures, and the time taken to change them.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Textile Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Inorganic Fibers (AREA)
Abstract
Description
- Graphite fibres are generally different from carbon fibres in respect of carbon content (purity), structure and physical characteristics. Graphite fibres are preferable to carbon fibres for use in sports equipment such as fishing rods and golf club shafts which require high modulus, for use in electric components such as heaters which require high purity and low resistivity, and for use in the aerospace industry, where parts for aircraft, rockets etc., may have to have high oxidation resistivity and be made to high precision. However, graphite fibres cost much more than carbon fibres and this high cost is largely a result of difficulties in manufacturing processability and productivity. An inert atmosphere is required for production of graphite fibres, and a higher temperature is used than for carbon fibres.
- Efforts have been made to increase productivity in manufacturing graphite fibres. For example, it has been proposed to increase the temperature gradient and to shorten the time in graphitizing furnace. However, this produces increased amounts of fuzz on the surface of the graphite fibres and occasional breakage of the fibre strands.
- Also, these modifications tend to reduce the tensile strength of the fibres. Further, since the temperature of the inert atmosphere must be higher than that used for manufacturing carbon fibres the wear on the graphitizing furnace, particularly on its heating pipes, is considerably greater. As a result of such wear due to exceedingly high temperatures, deviations from the desired temperature profile tend to increase and the furnace tube must be changed frequently. This seriously interferes with production and processability, and also consumes large amounts of energy, labour and materials.
- According to the present invention there is provided a process for the manufacture of graphite fibre by graphitizing precursor fibre characterised in that the precursor fibre or fibres pass successively through separately controllable first and second heating zones, both containing an inert atmosphere, the temperature at the hottest point in the said first heating zone being in the range of about 1500°C to about 2l00oC, and the temperature at the hottest part in the said second heating zone being at least about 2100°C.
- By use of the present invention it is possible to obtain a stable method of manufacturing high grade and high quality graphite fibres, particularly graphite fibres which have a minimum of surface fuzz. The process may use a shorter heating zone than is usual in conventional processes. Additionally, it is possible to provide a manufacturing process in which the life of parts is lengthened, and their replacement is easier, thereby saving energy, materials and labour.
- The term "graphite fibre" as used herein is intended to mean a fibre which is obtained by heating a graphitizable precursor fibre in an inert atmosphere at a temperatue of about 2100°C, or more and which fibre contains about 95% or more by weight of carbon. The term "graphitizable precursor fibre" or "precursor fibre" is intended to mean a fibre which has sufficient structural integrity to maintain its fibrous character and which can be converted to a graphite fibre when heated in an inert atmosphere at a temperature of about 2100oC or more. A typical example of a precursor fibre is an oxidized fibre obtained by heating an acrylic fibre, a cellulosic fibre (rayon), a polyvinylalcohol fibre or a pitch fibre in an oxidizing atmosphere at a temperature of about 200°C to 400°C. Another typical example is a carbon fibre obtained by heating the said oxidized fibre in an inert atmosphere at a temperature above about 400°C. When using the process of the present invention it is preferable to use a precursor fibre obtained from an acrylic fibre comprising about 95 mol % minimum of acrylonitrile (AN) and up to about 5 mol % of one or more ethylene-type vinyl compounds which are copolymerizable with acrylonitrile.
- The maximum temperature in the first heating zone is preferably in the range of 1700°Cto 1900°C. The second heating zone preferably has a maximum temperature in the range of 2100°C to 3500°C, more preferably in the range of 2300°C to 2700°C.
- It has been discovered that if the front and rear heating zones are operated at heating temperatures outside the ranges from 1500°C to 2100°C and 2100°C to 3500°C, respectively, it is difficult to obtain high quality graphite fibre. The quality of the fibre produced is influenced by such things as the type of precursor fibre, whether it was pretreated or not, and the temperature profile of the heating zone; in some instances it is especially sensitive to the maximum temperature of the first heating zone and is reduced if this exceeds about 2100°C. In particular, the fibres tend to develop excessive surface fuzz and tend to break easily.
- The rate of heating of the precursor fibre as it passes through the heating zones is preferably within the range of 300°C/min to 2000°C/min in the first heating zone, more preferably within the range of 500°C/min to 1500°C/min, and preferably within the range of 2000°C/min to 10,000°C/min in the second heating zone.
- The treatment time of the precursor fibres in the first heating zone, which is defined as the time during which the fibres are in the zone at a temperature above 1000°C. is preferably within the range of 10 seconds to 10 minutes, more preferably 30 seconds to 3 minutes.
- An embodiment of the present invention will now be described by way of example with reference to the drawings, in which:
- Fig. 1 is a view in longitudinal section of graphitizing apparatus for carrying out the process of this invention;
- Figs. 2 and 3 respectively show typical examples of temperature profiles in the furnace tubes used in the respective heating zones.
- Referring to Fig. 1, the separate first and second heating zones (furnaces) have respectively furnace tubes (2,3) to which heat is applied in a conventional way. The furnace tubes (2,3) are surrounded with insulation (4,5). An inert gas such as nitrogen is supplied to the furnaces (I,II) through pipes (6), and the gas is removed from the furnaces by pipes (7). At each end of each furnace there are furnace seals (8), supplied with inert gas through supply pipes (9).
- As shown in Fig. 1, the precursor fibre (1) is first conducted through the seal (-8) into the furnace tube (2) of the furnace (1) which provides the first heating zone. The temperature profile inside this furnace tube (2) is controlled, to produce a profile as shown in Fig. 2. This is done by locally controlling the heat input at selected spots along the tube (2), in a conventional way. When the precursor fibre is a carbon fibre, it is treated in this furnace until its weight is reduced to about 93% to 95% of its previous weight, and then it is conducted into the furnace tube (3) of the furnace (II) which provides the second heating zone. There the fibre is heated again, and is converted into a graphite fibre. Fig. 3 shows a typical temperature profile of the furnace tube (3) of the second heating zone, the maximum temperature of which is set at about 2500°C in this case.
- By use of the present invention, a more efficient and therefore more profitable process for the manufacture of graphite fibres is possible. These advantages can be realised for the following reasons:
- (a) The heating zone is divided into two independently controlled zones, giving increased flexibility with the rate of heating the fibre. There is also better control of the temperature profile within the furnace;
- (b) The weight loss of the precursor fibre during initial heating up to 1500°C is usually large. It has been found that the use of a high rate of heating in the stage up to 1500°C tends to damage the precursor fibre. In the conventional, single heating zone system, the overall rate of heating must be so low that it restricts overall productivity. By use of the present, double heating zone system, it is possible to select optimum rates of heating for the first and second heating zones independently of each other. This allows manufacture of high quality graphite fibres with increased productivity;
- (c) With the process of the present invention, it is possible to reduce the overall length of the heating zone by dividing it, and the maintenance and custody of the furnace can thereby be made easier. The life of a furnace tube in the second furnace is much shorter than that of one in the first furnace, because of the higher temperature at which it operates. However, clearly the tube in the first furnace need not be replaced merely because the tube in the second furnace has to be, and also the tube in the second furnace, being relatively short compared with the tube in a single-heating zone furnace, is easier to handle. Thus, costs of time, labour, and materials can be reduced. Surprisingly the energy consumption can also be reduced. This is because it has been found possible to string up the fibres without lowering the temperatue of the furnace.
- Carbon fibres were produced from acrylic fibres and carbonized in an inert atmosphere, the maximum temperature of which was 1100°C. They were taken from creels and heated to produce graphite fibres using separate furnaces as shown in Fig. 1. The conditions were varied, there being 3 conditions within the scope of the invention (Examples 1-3) and four conditions outside the scope of the invention (Comparative Examples 1-4). The conditions are shown in Table 1.
The resulting data are shown in Table 2. Moreover, the usual temperatures, the periods of time between changes of furnace tubes and the number of days required to change them, with respect to both first and second furnaces, are shown in Table 3. Some of the properties of the fibres made in these examples are shown in Table 2. -
Claims (10)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE7979301690T DE2964615D1 (en) | 1979-08-17 | 1979-08-17 | Process for the manufacture of graphite fibres |
| EP19790301690 EP0024277B1 (en) | 1979-08-17 | 1979-08-17 | Process for the manufacture of graphite fibres |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP19790301690 EP0024277B1 (en) | 1979-08-17 | 1979-08-17 | Process for the manufacture of graphite fibres |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0024277A1 true EP0024277A1 (en) | 1981-03-04 |
| EP0024277B1 EP0024277B1 (en) | 1983-01-26 |
Family
ID=8186421
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19790301690 Expired EP0024277B1 (en) | 1979-08-17 | 1979-08-17 | Process for the manufacture of graphite fibres |
Country Status (2)
| Country | Link |
|---|---|
| EP (1) | EP0024277B1 (en) |
| DE (1) | DE2964615D1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USRE36014E (en) * | 1992-09-08 | 1998-12-29 | Fujitsu Limited | Voltage storage circuits |
| CN108560081A (en) * | 2018-05-30 | 2018-09-21 | 中国科学院宁波材料技术与工程研究所 | A kind of preparation system and method for high strength high modulus carbon fiber |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2006543A1 (en) * | 1968-04-19 | 1969-12-26 | Rolls Royce |
-
1979
- 1979-08-17 DE DE7979301690T patent/DE2964615D1/en not_active Expired
- 1979-08-17 EP EP19790301690 patent/EP0024277B1/en not_active Expired
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2006543A1 (en) * | 1968-04-19 | 1969-12-26 | Rolls Royce |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USRE36014E (en) * | 1992-09-08 | 1998-12-29 | Fujitsu Limited | Voltage storage circuits |
| CN108560081A (en) * | 2018-05-30 | 2018-09-21 | 中国科学院宁波材料技术与工程研究所 | A kind of preparation system and method for high strength high modulus carbon fiber |
| CN108560081B (en) * | 2018-05-30 | 2023-07-18 | 中国科学院宁波材料技术与工程研究所 | A system and method for preparing high-strength and high-modulus carbon fibers |
Also Published As
| Publication number | Publication date |
|---|---|
| DE2964615D1 (en) | 1983-03-03 |
| EP0024277B1 (en) | 1983-01-26 |
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