JPH03816A - High-performance pitch-based carbon fiber and production thereof - Google Patents
High-performance pitch-based carbon fiber and production thereofInfo
- Publication number
- JPH03816A JPH03816A JP13298689A JP13298689A JPH03816A JP H03816 A JPH03816 A JP H03816A JP 13298689 A JP13298689 A JP 13298689A JP 13298689 A JP13298689 A JP 13298689A JP H03816 A JPH03816 A JP H03816A
- Authority
- JP
- Japan
- Prior art keywords
- fiber
- carbon fiber
- pitch
- based carbon
- compressive strength
- 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.)
- Pending
Links
- 229920000049 Carbon (fiber) Polymers 0.000 title claims abstract description 60
- 239000004917 carbon fiber Substances 0.000 title claims abstract description 60
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title claims abstract description 37
- 238000004519 manufacturing process Methods 0.000 title claims description 6
- 239000000835 fiber Substances 0.000 claims abstract description 53
- 230000005684 electric field Effects 0.000 claims abstract description 6
- 239000007787 solid Substances 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 claims description 17
- 238000005468 ion implantation Methods 0.000 claims description 8
- 239000000463 material Substances 0.000 abstract description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 abstract description 8
- 229910052796 boron Inorganic materials 0.000 abstract description 8
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 abstract description 4
- 229910052757 nitrogen Inorganic materials 0.000 abstract description 4
- 230000006835 compression Effects 0.000 abstract 3
- 238000007906 compression Methods 0.000 abstract 3
- 239000007789 gas Substances 0.000 abstract 1
- 229920006253 high performance fiber Polymers 0.000 abstract 1
- 238000005470 impregnation Methods 0.000 abstract 1
- 239000011295 pitch Substances 0.000 description 21
- 150000002500 ions Chemical class 0.000 description 15
- 238000002513 implantation Methods 0.000 description 10
- 125000004429 atom Chemical group 0.000 description 8
- 238000002347 injection Methods 0.000 description 7
- 239000007924 injection Substances 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 239000002131 composite material Substances 0.000 description 6
- -1 boron fluoride Chemical class 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 239000007943 implant Substances 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 239000002994 raw material Substances 0.000 description 4
- 239000002344 surface layer Substances 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 230000001133 acceleration Effects 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- 239000011302 mesophase pitch Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 229910015900 BF3 Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- WTEOIRVLGSZEPR-UHFFFAOYSA-N boron trifluoride Chemical compound FB(F)F WTEOIRVLGSZEPR-UHFFFAOYSA-N 0.000 description 2
- 125000004432 carbon atom Chemical group C* 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 239000011888 foil Substances 0.000 description 2
- 238000005087 graphitization Methods 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- YXALYBMHAYZKAP-UHFFFAOYSA-N 7-oxabicyclo[4.1.0]heptan-4-ylmethyl 7-oxabicyclo[4.1.0]heptane-4-carboxylate Chemical compound C1CC2OC2CC1C(=O)OCC1CC2OC2CC1 YXALYBMHAYZKAP-UHFFFAOYSA-N 0.000 description 1
- 229920001342 Bakelite® Polymers 0.000 description 1
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 1
- PXGOKWXKJXAPGV-UHFFFAOYSA-N Fluorine Chemical compound FF PXGOKWXKJXAPGV-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 239000004637 bakelite Substances 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 238000003763 carbonization Methods 0.000 description 1
- 150000001793 charged compounds Chemical class 0.000 description 1
- 239000000460 chlorine Substances 0.000 description 1
- 229910052801 chlorine Inorganic materials 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000011300 coal pitch Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- JDVIRCVIXCMTPU-UHFFFAOYSA-N ethanamine;trifluoroborane Chemical compound CCN.FB(F)F JDVIRCVIXCMTPU-UHFFFAOYSA-N 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000011737 fluorine Substances 0.000 description 1
- 229910052731 fluorine Inorganic materials 0.000 description 1
- 238000005194 fractionation Methods 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 235000011187 glycerol Nutrition 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 238000005984 hydrogenation reaction Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910052743 krypton Inorganic materials 0.000 description 1
- DNNSSWSSYDEUBZ-UHFFFAOYSA-N krypton atom Chemical compound [Kr] DNNSSWSSYDEUBZ-UHFFFAOYSA-N 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 238000002074 melt spinning Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052754 neon Inorganic materials 0.000 description 1
- GKAOGPIIYCISHV-UHFFFAOYSA-N neon atom Chemical compound [Ne] GKAOGPIIYCISHV-UHFFFAOYSA-N 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000011208 reinforced composite material Substances 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 229910052714 tellurium Inorganic materials 0.000 description 1
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 239000011135 tin Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Landscapes
- Chemical Or Physical Treatment Of Fibers (AREA)
- Inorganic Fibers (AREA)
- Chemical Treatment Of Fibers During Manufacturing Processes (AREA)
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野コ
本発明は高性能なピッチ系炭素繊維、特に圧縮強度に優
れたピッチ系炭素繊維およびその製造方法に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to high-performance pitch-based carbon fibers, particularly pitch-based carbon fibers with excellent compressive strength, and a method for producing the same.
[従来の技術]
近年炭素繊維は、その優れた機械的物性から各種の複合
材に活用され、急速に需要が伸びつつある。これに伴い
、炭素繊維に対する要求性能がよすます高くなっている
。従来は引張特性に対する改良要求が中心であり、その
要求に応えて炭素繊維の引張強度は大幅に向上した。し
かし、圧縮強度は殆ど改良していないため、曲げ強度な
どの実用特性が圧縮強度に支配されて頭打ちになるとい
った問題が顕在化してきた。[Prior Art] In recent years, carbon fibers have been used in various composite materials due to their excellent mechanical properties, and demand is rapidly increasing. Along with this, the performance requirements for carbon fibers are becoming higher and higher. Conventionally, the focus has been on improving the tensile properties, and in response to these demands, the tensile strength of carbon fibers has been significantly improved. However, since there has been little improvement in compressive strength, the problem has emerged that practical properties such as bending strength are dominated by compressive strength and reach a plateau.
炭素繊維の剛性を有効に活用し、複合材料の一層の軽量
化効果を実現するためにはより薄肉の構造材とすること
が重要であり、そのために弾性率の高い炭素繊維が要求
されることから黒鉛結晶性の高いピッチ系炭素繊維が有
望視されているが、ピッチ系炭素繊維は易黒鉛化原料を
用いていることから剪断座屈が生じ易く、同一弾性率の
場合、ポリアクリロニトリル(PAN)系炭素繊維より
も圧縮強度が約1/2と低い問題がある。In order to make effective use of the stiffness of carbon fiber and further reduce the weight of composite materials, it is important to create a thinner structural material, which requires carbon fiber with a high modulus of elasticity. Pitch-based carbon fibers with high graphite crystallinity are seen as promising, but since pitch-based carbon fibers use easily graphitized raw materials, shear buckling is likely to occur. ) type carbon fiber has a problem that its compressive strength is about 1/2 lower than that of carbon fiber.
従来、引張特性の向上技術については数多くの提案がな
されているが、圧縮強度の向上技術については殆ど提案
されていないのが現状である。わずかに、PAN系炭素
繊維において製糸および焼成条件を特定化することによ
って圧縮強度の高い弾性率35し712以上の黒鉛化繊
維が提案されているだけであり(特開昭63−2113
26号公報)、ピッチ系炭素繊維については提案されて
いない。In the past, many proposals have been made regarding techniques for improving tensile properties, but at present there have been almost no proposals regarding techniques for improving compressive strength. Only a few graphitized fibers with high compressive strength and an elastic modulus of 35 to 712 or more have been proposed by specifying spinning and firing conditions for PAN-based carbon fibers (Japanese Patent Laid-Open No. 63-2113).
No. 26), pitch-based carbon fibers are not proposed.
そこで本発明者らは、ピッチ系炭素繊維において、圧縮
強度を向上させる技術を鋭意検討した結果、炭素繊維強
化複合材料の圧縮強度支配因子である炭素繊維の単繊維
圧縮強度を向上させることが重要であり、そのためには
繊維表層部の結晶性を低下させる、すなわち表N部をよ
り等方質に近い構造にすることにより、単繊維圧縮強度
が大幅に向上できることを見い出し、本発明に至ったも
のである。Therefore, the present inventors have intensively investigated techniques for improving the compressive strength of pitch-based carbon fibers, and found that it is important to improve the single fiber compressive strength of carbon fibers, which is the dominant factor in the compressive strength of carbon fiber reinforced composite materials. To this end, we have discovered that the single fiber compressive strength can be significantly improved by reducing the crystallinity of the surface layer of the fiber, that is, by making the N-surface part more nearly isotropic in structure, which led to the present invention. It is something.
なお、材料の表面からイオン化した原子あるいは分子を
加速して注入する。いわゆるイオン注入法は、半導体用
途を中心に各種材料の表層を改質する技術として検討さ
れている(特開昭58−87818号公報、特開昭58
−87894号公報)が、この種の技術をピッチ系炭素
繊維について適用された例は知られていない。Note that ionized atoms or molecules are accelerated and implanted from the surface of the material. The so-called ion implantation method is being studied as a technique for modifying the surface layer of various materials mainly for semiconductor applications (Japanese Patent Application Laid-Open No. 58-87818, Japanese Patent Application Laid-Open No. 58-87,
No. 87894) is not known to have applied this type of technology to pitch-based carbon fibers.
[発明が解決しようとする課題]
本発明の課題は、上記従来技術では達成し得なかった圧
縮強度の高い高性能なピッチ系炭素繊維を提供すること
にある。[Problems to be Solved by the Invention] An object of the present invention is to provide a high-performance pitch-based carbon fiber with high compressive strength that could not be achieved with the above-mentioned conventional techniques.
[課題を解決するための手段]
本発明の上記課題は、
(1)引張弾性率が35 j/mm2以上で、単繊維圧
縮強度が300 kg/mm2以上であることを特徴と
する高性能ピッチ系炭素繊維。[Means for Solving the Problems] The above-mentioned problems of the present invention are as follows: (1) A high-performance pitch characterized by having a tensile modulus of elasticity of 35 J/mm2 or more and a single fiber compressive strength of 300 kg/mm2 or more. carbon fiber.
(2)ピッチ系炭素繊維束を、イオン注入方向に対する
束厚みが単繊維径の5倍以下となるように開繊し、10
−3Torr以下の真空下で、常温で固体あるいは気体
である原子あるいは分子をイオン化し、を場によって加
速して炭素繊維束表面の少なくとも2方向から注入する
ことを特徴とする高性能ピッチ系炭素繊維の製造方法。(2) Spread the pitch-based carbon fiber bundle so that the bundle thickness in the ion implantation direction is 5 times or less the single fiber diameter, and
- High-performance pitch-based carbon fiber characterized by ionizing atoms or molecules that are solid or gaseous at room temperature under a vacuum of 3 Torr or less, accelerating them in a field, and injecting them from at least two directions on the surface of the carbon fiber bundle. manufacturing method.
によって解決することができる。It can be solved by
以下、まず本発明繊維について説明する。First, the fiber of the present invention will be explained below.
本発明のピッチ系炭素繊維は、引張弾性率が35 t/
mm2以上であることが必須である。これは、既述した
ように構造材を薄肉化するためには高弾性率、特に35
t/mm2以上の引張弾性率が必要とされるからであ
る。引張弾性率は高い程構造材を4肉化することができ
るが、引張弾性率が高くなるにつれて圧縮強度が低下す
る傾向があるので、好ましくは35〜60t、/mm2
.さらに好ましくは35〜55 t/mm2程度がバラ
ンス上良いといえる。The pitch-based carbon fiber of the present invention has a tensile modulus of 35 t/
It is essential that it is at least mm2. As mentioned above, in order to make the structural material thinner, a high elastic modulus, especially 35
This is because a tensile modulus of elasticity of t/mm2 or more is required. The higher the tensile modulus, the more the structural material can be made into four-walled material, but as the tensile modulus increases, the compressive strength tends to decrease, so it is preferably 35 to 60 t/mm2.
.. More preferably, it can be said that about 35 to 55 t/mm2 is good in terms of balance.
複合材料の圧縮強度の重要な因子である単繊維圧縮強度
σ。fは300 kg/mm2以上、好ましくは350
kg/mm2以上、さらに好ましくは400 kg/
mu2以上がよい。すなわち、単繊維圧縮強度と複合材
料の圧縮強度とは良い相関を示しており、本発明のピッ
チ系炭素繊維によって、単繊維圧縮強度σcTが300
kg/mn+2以上であるPAN系炭素繊維と同等の
複合材料圧縮強度を得ることができるのである。それに
よって従来圧縮強度律速のためにPAN系炭素繊維のみ
しか用いることのできなかった用途までピッチ系炭素繊
維を用いることが可能となった。Single fiber compressive strength σ is an important factor for the compressive strength of composite materials. f is 300 kg/mm2 or more, preferably 350
kg/mm2 or more, more preferably 400 kg/mm2 or more
Mu2 or higher is better. That is, there is a good correlation between the single fiber compressive strength and the compressive strength of the composite material, and the pitch-based carbon fiber of the present invention has a single fiber compressive strength σcT of 300.
It is possible to obtain a composite material compressive strength equivalent to that of PAN-based carbon fiber, which is at least kg/mn+2. This has made it possible to use pitch-based carbon fibers in applications where conventionally only PAN-based carbon fibers could be used because of compressive strength rate limiting.
ここで、本発明における引張弾性率、単繊維圧縮強度(
σ。「)は、それぞれ以下の方法により求めた値である
。Here, the tensile modulus and single fiber compressive strength (
σ. ``) are values obtained using the following methods.
■張彊作率
炭素繊維束に ″ベークライト”ERL−4221/三
フツ化ホウ素モノエチルアミン(BF3・MEA)/ア
セトン=100/3/4部を含浸し、得られた樹脂含浸
ストランドを130°Cで30分間加熱して硬化させ、
J l5−R−7601に規定する樹脂含浸ストランド
試験法に従って測定し、引張弾性率を求めた。■Zhang Jiao Production Carbon fiber bundle is impregnated with "Bakelite" ERL-4221/Boron Trifluoride Monoethylamine (BF3/MEA)/Acetone = 100/3/4 parts, and the resulting resin-impregnated strand is heated to 130°C. Heat for 30 minutes to harden,
The tensile modulus was determined by measuring according to the resin-impregnated strand test method specified in J I5-R-7601.
t σr
約10cmの単繊維をスライドグラス上に置き、中央部
にグリセリンを1〜2滴たらして単繊維をひねりながら
ループを作り、その上にプレパラートを置く。これを顕
微鏡下に置いて顕微鏡に接続したビデオカメラでモニタ
(CRT)上に映し、これを観察しながら常にループを
視野に捉えるようにする。そしてループの両端を指で押
さえながら、一定速度で引張り、歪をかける。破新する
までの挙動をビデオに録画し、再生画面を停止させなが
らループの短径(D)と長径(φ)をCRT上で測定す
る。単繊維径(d)とDから次式により図1のA点にお
ける歪(ε)を計算し、εを横軸、長径と短径との比(
φ/D)を縦軸にしてグラフにプロットする(図2)。t σr Place a single fiber of about 10 cm on a slide glass, add 1 to 2 drops of glycerin to the center, twist the single fiber to make a loop, and place the preparation on top of it. This is placed under a microscope and projected onto a monitor (CRT) using a video camera connected to the microscope, so that the loop is always visible while observing this. Then, while holding both ends of the loop with your fingers, pull it at a constant speed to apply strain. The behavior up to the point of failure is recorded on video, and the short axis (D) and long axis (φ) of the loop are measured on a CRT while the playback screen is stopped. The strain (ε) at point A in Figure 1 is calculated from the single fiber diameter (d) and D using the following formula, where ε is the horizontal axis and the ratio of the major axis to the minor axis (
φ/D) is plotted on a graph with the vertical axis (FIG. 2).
s=1.07Xd/D
φ/Dは、圧縮座屈しない領域では一定値(約1.34
)を示すが、圧縮座屈すると急に大きくなるので、φ/
Dが急に増大し始める歪を圧縮降伏歪(i cf)とし
て求める。これを約10本の単繊維につき測定し、その
平均値を求めた。得られた平均値に引張弾性率を掛けた
値を単繊維圧縮強度とした。s=1.07Xd/D φ/D is a constant value (approximately 1.34
), but it suddenly increases when compressive buckling occurs, so φ/
The strain at which D suddenly begins to increase is determined as the compressive yield strain (i cf). This was measured for about 10 single fibers, and the average value was determined. The value obtained by multiplying the obtained average value by the tensile modulus was defined as the single fiber compressive strength.
次に、本発明繊維の製造例について説明する。Next, an example of manufacturing the fiber of the present invention will be explained.
すなわち、本発明繊維の原料繊維であるピッチ系炭素繊
維としては、易黒鉛化性で黒鉛化処理により容易に高弾
性率が得られるメソフェーズピッチ系炭素繊維が好まし
い。メソフェーズピッチの原料は石炭系2石油系どちら
でも良く、従来公知の溶媒分別、水素添加、熱処理等を
行ない溶融紡糸してピッチ繊維とした後、酸化性雰囲気
中で不融化し、不活性雰囲気中、緊張下での炭化あるい
はさらに黒鉛化を行うことにより得られる。圧縮強度の
高いピッチ系炭素wA維を得るためには、ボイドなどの
欠陥の少ない炭素繊維が好ましく、たとえば引張強度レ
ベルで言えば、好ましくは300kg/mu2以上、よ
り好ましくは400 kg/mcn2以上である。また
、原料炭素繊維の引張弾性率レベルは好ましくは35t
/Ill!112以上である。That is, as the pitch-based carbon fiber that is the raw material fiber for the fiber of the present invention, mesophase pitch-based carbon fiber is preferable because it is easily graphitized and can easily obtain a high modulus of elasticity through graphitization treatment. The raw material for mesophase pitch can be either coal-based or petroleum-based, and after performing conventionally known solvent fractionation, hydrogenation, heat treatment, etc., and melt-spinning to make pitch fibers, it is made infusible in an oxidizing atmosphere, and then in an inert atmosphere. , by carbonization under tension or further graphitization. In order to obtain pitch-based carbon wA fibers with high compressive strength, carbon fibers with few defects such as voids are preferable.For example, in terms of tensile strength level, preferably 300 kg/mu2 or more, more preferably 400 kg/mcn2 or more. be. Further, the tensile modulus level of the raw carbon fiber is preferably 35t.
/Ill! It is 112 or more.
この様なピッチ系炭素繊維を用いて、常温で固体あるい
は気体である原子あるいは分子を真空下でイオン化し、
電場によって加速して炭素繊維表面に注入させる。Using such pitch-based carbon fibers, atoms or molecules that are solid or gaseous at room temperature are ionized under vacuum.
It is accelerated by an electric field and injected into the carbon fiber surface.
高速の原子あるいは分子をつくり、炭素w&雑の表面か
ら注入する最も好ましい方法は、真空下で原子2分子を
イオン化し、これを電場によって加速する。いわゆるイ
オン注入法と呼ばれているものである。すなわち、この
方法では電場を大きくすることにより電場に比例したエ
ネルギーをもつ原子9分子を得ることができるため、目
的とする深さまで原子9分子を注入することができる。The most preferred method for creating high-speed atoms or molecules and injecting them from the surface of carbon and other materials is to ionize two molecules of atoms under vacuum and accelerate them using an electric field. This is a so-called ion implantation method. That is, in this method, by increasing the electric field, it is possible to obtain nine molecules of atoms having energy proportional to the electric field, so that nine molecules of atoms can be implanted to a desired depth.
高速の原子あるいは分子は、炭素繊維を形成する炭素原
子と衝突し、その運動エネルギーを炭素原子に与えるこ
とによって炭素繊維中に照射損傷をつくる。このような
照射損傷がM損する結果、炭素繊維表層部に結晶性の低
い層、すなわちより等言質に近い層が形成され、繊維の
圧縮強度が向上するのである。The high-velocity atoms or molecules collide with the carbon atoms forming the carbon fibers and impart their kinetic energy to the carbon atoms, thereby creating radiation damage in the carbon fibers. As a result of such irradiation damage resulting in M loss, a layer with low crystallinity, that is, a layer that is more isomorphous, is formed on the surface layer of the carbon fiber, and the compressive strength of the fiber is improved.
注入するイオン種としては、例えばベリリウム。An example of the ion species to be implanted is beryllium.
ホウ素、炭素、ケイ素、リン、チタニウム、クロミウム
、鉄、ニッケル、コバルト、銅、亜鉛、ゲルマニウム、
銀、スズ、モリブデン、テルル、タンタル、タングステ
ン、金、白金などの常温で固体状の元素および水素、窒
素、ネオン、アルゴン。Boron, carbon, silicon, phosphorus, titanium, chromium, iron, nickel, cobalt, copper, zinc, germanium,
Elements that are solid at room temperature such as silver, tin, molybdenum, tellurium, tantalum, tungsten, gold, and platinum, as well as hydrogen, nitrogen, neon, and argon.
クリプトン、フッ素、塩素、などの常温で気体状の元素
あるいはそれらが複合したフッ化ボロンなどの分子イオ
ンを適用できるが、経済性および注入による圧縮特性向
上効果から窒素、ホウ素、アルゴン、炭素、ケイ素、チ
タニウム、クロミウム。Elements that are gaseous at room temperature, such as krypton, fluorine, and chlorine, or molecular ions, such as boron fluoride, which are composites of these elements, can be applied, but nitrogen, boron, argon, carbon, and silicon can be used due to economic efficiency and the effect of improving compressive properties by injection. , titanium, chromium.
ニッケル、銅が好ましく、さらに好ましくは窒素。Nickel and copper are preferred, and nitrogen is more preferred.
ホウ素、炭素、チタニウム、クロミウムがよい。Boron, carbon, titanium, and chromium are good.
また、二種類以上のイオン種を同時に、あるいは連続的
に注入することも処理効果向上のために有効である。Furthermore, it is also effective to implant two or more types of ion species simultaneously or successively to improve the processing effect.
注入条件は圧縮特性向上効果が大きい構造を得るのに最
も適したイオン種、加速電圧、注入量という観点から、
注入されるターゲットである炭素繊維との関係によって
選ばれるべきである。The implantation conditions are determined from the viewpoint of the most suitable ion species, accelerating voltage, and implantation amount to obtain a structure with a large effect of improving compressive properties.
It should be selected depending on the relationship with the carbon fiber that is the target to be injected.
注入時の真空度は、10−3Torr以下、好ましくは
10−’Torr以下、より好ましくは10−5Tor
r以下であることがイオン注入を効果的に行なうために
有効である。The degree of vacuum during injection is 10-3 Torr or less, preferably 10-'Torr or less, more preferably 10-5 Torr.
It is effective for the ion implantation to be less than or equal to r.
イオンの加速電圧は好ましくは50kV以上、より好ま
しくは100kV以上、さらに好ましくは150kV以
上がよい。イオン種および加速電圧の組み合わせにより
注入深さが決まるので、圧縮特性の向上の効果が大きい
所望の注入深さを得るために、その組み合わせを最適化
することが好ましい。The ion accelerating voltage is preferably 50 kV or higher, more preferably 100 kV or higher, even more preferably 150 kV or higher. Since the implantation depth is determined by the combination of ion species and accelerating voltage, it is preferable to optimize the combination in order to obtain a desired implantation depth that is highly effective in improving compressive properties.
注入量としては好ましくは10 ” (ions)/
c m2以上、より好ましくは10”/cm2以上、さ
らに好ましくは1017/cm2以上がよく、イオン種
および加速電圧との組み合わせにより注入量を最適化す
るのがよい。The injection amount is preferably 10” (ions)/
cm2 or more, more preferably 10"/cm2 or more, even more preferably 1017/cm2 or more, and the implantation amount is preferably optimized by combining the ion species and acceleration voltage.
注入時間は注入量と注入装置のビーム強度によって決ま
るが、例えば10”/cm2以上の注入量を生産性よく
注入するためにはO,lμA/cm2以上、好ましくは
1μA/crn2以上、さらに好ましくは5μA/cm
2以上のビーム強度がよい。1μA/crn2以上のビ
ーム強度により10分以下、好ましくは1分以下の処理
時間で注入することが可能である。The implantation time is determined by the implantation amount and the beam intensity of the implantation device, but for example, in order to implant an implantation amount of 10"/cm2 or more with good productivity, the injection time is O,lμA/cm2 or more, preferably 1μA/crn2 or more, more preferably 1μA/crn2 or more. 5μA/cm
A beam intensity of 2 or more is good. With a beam intensity of 1 μA/crn2 or more, it is possible to perform the implantation in a processing time of 10 minutes or less, preferably 1 minute or less.
この様に、開繊した繊維束にイオン注入することが重要
であるが、裏側への注入は難しいため、表と裏といった
少なくとも2方向から注入することが重要である。2方
向から注入する方法としては、同時に2方向から注入し
てもよいし、1方向から注入した後、他の方向から再度
注入してもよい。その際にイオン種を変えることも可能
である。As described above, it is important to implant ions into the spread fiber bundle, but since it is difficult to implant ions into the back side, it is important to implant ions from at least two directions, the front and back sides. As for the method of injecting from two directions, it is possible to inject from two directions at the same time, or to inject from one direction and then inject again from the other direction. At this time, it is also possible to change the ion species.
注入する際の炭素繊維束の供給方法としては、イオン注
入方向に対する束厚みが単繊維径の5倍以下、好ましく
は3倍以下、さらに好ましくは2倍以下となるように単
繊維が分散した状態に開繊することが重要である。すな
わち、真空中を直進するイオンはピッチ系炭素繊維の表
層から0.1〜2μm程度までしか注入できず、重なっ
た影の部分には注入されないため、繊維全体にイオンが
均一に注入できるようにするためには、上記開繊が必要
になる。この開繊が不十分であるとイオンが注入された
部分と注入されない部分が生じ、先に述べた単繊維圧縮
強度が充分に向上しないために好ましくない。The method for supplying carbon fiber bundles during injection is such that the single fibers are dispersed so that the bundle thickness in the ion implantation direction is 5 times or less, preferably 3 times or less, and more preferably 2 times or less the single fiber diameter. It is important to spread the fibers. In other words, ions traveling in a straight line in a vacuum can only be injected to a depth of about 0.1 to 2 μm from the surface layer of pitch-based carbon fibers, and are not injected into the overlapping shadow areas, so that ions can be injected uniformly throughout the fiber. In order to do so, the above-mentioned opening is necessary. If this fiber opening is insufficient, some parts are implanted with ions and some parts are not implanted, which is not preferable because the compressive strength of the single fiber mentioned above cannot be sufficiently improved.
開繊方法としては、単繊維を切り取り、金属枠などに固
定してもよいが、好ましくは炭素繊維束を低周波あるい
は超周波振動などの機械的振動を加えた拡幅ガイドによ
り開繊するのがよい。この際、平型および凸型ガイドを
組み合わせて用いることが好ましい。この方法により、
連続的に炭素繊維を供給することが可能となり、生産性
が向上するので好ましい方法である。As for the opening method, single fibers may be cut out and fixed to a metal frame, etc., but it is preferable to open the carbon fiber bundle using a widening guide that applies mechanical vibration such as low frequency or ultra-frequency vibration. good. At this time, it is preferable to use a combination of flat and convex guides. With this method,
This is a preferred method because it enables continuous supply of carbon fibers and improves productivity.
口実施例コ 以下、実施例により本発明をさらに具体的に説明する。oral example Hereinafter, the present invention will be explained in more detail with reference to Examples.
実施例1
石炭系ピッチを原料とした弾性率38 t/mm2のメ
ソフェーズピッチ系炭素繊維束から、単繊維約100本
を分別して、IQcm四方のアルミ枠に単繊維が並行に
並ぶように引き揃えて固定し、真空度3 X 10 =
Torr、加速電圧150kVでホウ素イオンをlX1
016/ 0m2注入した。この処理を表と裏の両面か
ら行なった。ビーム強度は0゜2μA/cm2であり、
処理時間は片面につき約20分であった。Example 1 Approximately 100 single fibers were separated from a mesophase pitch-based carbon fiber bundle with an elastic modulus of 38 t/mm2 made from coal-based pitch as a raw material, and arranged so that the single fibers were lined up in parallel on an IQcm square aluminum frame. and fix it, vacuum degree 3 x 10 =
Torr, boron ions at an acceleration voltage of 150 kV
016/0m2 injected. This treatment was performed from both the front and back sides. The beam intensity is 0°2μA/cm2,
Processing time was approximately 20 minutes per side.
イオン注入前後の炭素繊維につき単繊維圧縮強度を評価
した結果、単4a維圧縮強度σ。rは350kg/mu
”と、未注入糸(σc+ :170 kg/mm2)よ
りも大幅に向上していた。さらに単繊維引張特性は強度
380kg/m[lI22弾性率38 シ/mm2と、
未注入糸(強度340 kg#nm2.弾性率38 j
/mm2)に比べて弾性率を維持して、引張強度も向上
する効果が認められた。As a result of evaluating the single fiber compressive strength of carbon fibers before and after ion implantation, the single fiber compressive strength σ was found. r is 350kg/mu
”, which was significantly improved compared to the non-injected yarn (σc+: 170 kg/mm2).Furthermore, the single fiber tensile properties were 380 kg/m in strength [lI22 modulus of 38 sh/mm2,
Uninjected yarn (strength 340 kg#nm2. elastic modulus 38 j
/mm2), the effect of maintaining the elastic modulus and improving the tensile strength was observed.
実施例2
実施例1で用いたイオン注入前の炭素繊維束を、低周波
振動による凸型および平型加振ガイドを用いて、厚みが
単繊維径の3倍以下になるように開繊し、アルミホイル
をリードペーパーとしてボビンに巻き取った。得られた
巻き取りボビンを真空系内にセットし、リードペーパー
とともに炭素繊維束を引き出し、速度1cm/分で他の
ボビンに巻き取った。この走行炭素繊維束に、走行方向
に対して直角方向からホウ素イオンを連続的に注入した
。Example 2 The carbon fiber bundle used in Example 1 before ion implantation was opened using convex and flat excitation guides with low frequency vibration so that the thickness was three times or less the single fiber diameter. , aluminum foil was wound onto a bobbin as lead paper. The obtained winding bobbin was set in a vacuum system, and the carbon fiber bundle was pulled out together with the lead paper and wound onto another bobbin at a speed of 1 cm/min. Boron ions were continuously injected into this running carbon fiber bundle from a direction perpendicular to the running direction.
真空度はI X I 0−6Torr、加速電圧は15
0kV。Vacuum degree is IXI 0-6 Torr, acceleration voltage is 15
0kV.
注入量はlX1016/cm2であった。−度巻き取っ
た炭素繊維束を反対方向から解舒してもう一度処理する
ことにより、裏と表の両面から注入した。The injection volume was 1×1016/cm2. The carbon fiber bundle that had been wound up twice was unwound from the opposite direction and treated once again to inject it from both the back and front sides.
得られた炭素繊維につき単繊維圧縮強度を評価した結果
、340kg/mm2となり、未注入糸よりも大幅に向
上していた。さらに、単繊維引張特性は強度370 k
g/mm2.弾性率38t/mm2と、注入前に比べて
引張弾性率を維持して引張強度が向上する傾向が認めら
れた。As a result of evaluating the single fiber compressive strength of the obtained carbon fiber, it was found to be 340 kg/mm2, which was significantly improved compared to the non-injected yarn. In addition, the single fiber tensile properties have a strength of 370 k
g/mm2. The elastic modulus was 38 t/mm2, which showed a tendency to maintain the tensile elastic modulus and improve the tensile strength compared to before injection.
比較例1
実施例2において、ピッチ系炭素繊維束を低周波振動に
より、繊維束の厚みが単繊維径の10倍になるように開
繊し、アルミホイルをリードペーパーとしてボビンに巻
き取った。得られた巻き取りボビンは真空系内にセット
し、同様な条件下でホウ素イオンを裏と表の両面から炭
素繊維に連続的に注入した。Comparative Example 1 In Example 2, a pitch-based carbon fiber bundle was opened by low-frequency vibration so that the thickness of the fiber bundle was 10 times the single fiber diameter, and then wound around a bobbin using aluminum foil as a lead paper. The obtained winding bobbin was set in a vacuum system, and boron ions were continuously injected into the carbon fiber from both the back and front sides under the same conditions.
得られた炭素繊維の単繊維圧縮強度を評価した結果、2
10kF、/lllll12となり、未注入糸と比べほ
とんど向上していなかった。As a result of evaluating the single fiber compressive strength of the obtained carbon fiber, 2
The result was 10 kF/lllll12, which was almost no improvement compared to the non-injected thread.
比較例2
実施例1において、単繊維を10cm四方のアルミ枠に
平行に並ぶように引き揃えて固定した後、同様な条件で
片面のみホウ素イオンを注入した。Comparative Example 2 In Example 1, after the single fibers were aligned and fixed in parallel to a 10 cm square aluminum frame, boron ions were implanted only on one side under the same conditions.
得られた炭素繊維の圧縮特性を評価した結果、単繊維圧
縮強度σ。「は225 kg/mm2と、未注入糸と比
べてほとんど差はなく、1方向のみからイオンを注入し
た場合は圧縮特性の向上効果はほとんど得られなかった
。As a result of evaluating the compressive properties of the obtained carbon fibers, the single fiber compressive strength σ was determined. was 225 kg/mm2, which was almost no difference compared to the non-implanted yarn, and when ions were implanted from only one direction, almost no improvement in compressive properties was obtained.
[発明の効果コ
以上述べたように、本発明の引張弾性率が35t/mm
2以上、単繊維圧縮強度が300kg/mm2以上とい
うピッチ系炭素繊維により、特に航空機の一次構造材料
などの曲げ強度が要求される用途への展開を拡大するこ
とができる。[Effects of the Invention] As stated above, the tensile modulus of the present invention is 35t/mm.
Pitch-based carbon fibers with a single fiber compressive strength of 2 or more and 300 kg/mm2 or more can be used in applications that require high bending strength, particularly as primary structural materials for aircraft.
図1および2は、ループ法による単繊維圧縮強度の測定
法の概略図である(図工:ルーズの短径(D)と長径(
φ)の測定法。図2:歪εを横軸。
長径と短径との比(φ/D)を縦軸にしてグラフにプロ
ットしたもの。)。Figures 1 and 2 are schematic diagrams of a method for measuring single fiber compressive strength using the loop method (illustration: loose short axis (D) and long axis (
φ) measurement method. Figure 2: Strain ε on the horizontal axis. A graph plotted with the ratio of the major axis to the minor axis (φ/D) on the vertical axis. ).
Claims (2)
縮強度が300kg/mm^2以上であることを特徴と
する高性能ピッチ系炭素繊維。(1) A high-performance pitch-based carbon fiber characterized by having a tensile modulus of 35 t/mm^2 or more and a single fiber compressive strength of 300 kg/mm^2 or more.
束厚みが単繊維径の5倍以下となるように開繊し、10
^−^3Torr以下の真空下で、常温で固体あるいは
気体である原子あるいは分子をイオン化し、電場によつ
て加速して炭素繊維束表面の少なくとも2方向から注入
することを特徴とする高性能ピッチ系炭素繊維の製造方
法。(2) Spread the pitch-based carbon fiber bundle so that the bundle thickness in the ion implantation direction is 5 times or less the single fiber diameter, and
^-^ A high-performance pitch characterized by ionizing atoms or molecules that are solid or gaseous at room temperature under a vacuum of 3 Torr or less, accelerating them with an electric field, and injecting them from at least two directions on the surface of the carbon fiber bundle. A method for manufacturing carbon fiber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13298689A JPH03816A (en) | 1989-05-26 | 1989-05-26 | High-performance pitch-based carbon fiber and production thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13298689A JPH03816A (en) | 1989-05-26 | 1989-05-26 | High-performance pitch-based carbon fiber and production thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03816A true JPH03816A (en) | 1991-01-07 |
Family
ID=15094111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13298689A Pending JPH03816A (en) | 1989-05-26 | 1989-05-26 | High-performance pitch-based carbon fiber and production thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03816A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5968435A (en) * | 1997-04-24 | 1999-10-19 | Nippon Steel Corporation | Process for manufacturing pitch-type carbon fiber |
| WO2007018136A1 (en) | 2005-08-09 | 2007-02-15 | Toray Industries, Inc. | Flame-resistant fiber, carbon fiber, and processes for the production of both |
-
1989
- 1989-05-26 JP JP13298689A patent/JPH03816A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5968435A (en) * | 1997-04-24 | 1999-10-19 | Nippon Steel Corporation | Process for manufacturing pitch-type carbon fiber |
| WO2007018136A1 (en) | 2005-08-09 | 2007-02-15 | Toray Industries, Inc. | Flame-resistant fiber, carbon fiber, and processes for the production of both |
| US7976945B2 (en) | 2005-08-09 | 2011-07-12 | Toray Industires, Inc. | Flame resistant fiber, carbon fiber and production method thereof |
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