JPH0571683B2 - - Google Patents
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- Publication number
- JPH0571683B2 JPH0571683B2 JP15393784A JP15393784A JPH0571683B2 JP H0571683 B2 JPH0571683 B2 JP H0571683B2 JP 15393784 A JP15393784 A JP 15393784A JP 15393784 A JP15393784 A JP 15393784A JP H0571683 B2 JPH0571683 B2 JP H0571683B2
- Authority
- JP
- Japan
- Prior art keywords
- fiber
- strength
- temperature
- fibers
- nylon
- Prior art date
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- 239000000835 fiber Substances 0.000 claims description 63
- 238000010438 heat treatment Methods 0.000 claims description 32
- 229920002302 Nylon 6,6 Polymers 0.000 claims description 21
- 238000004519 manufacturing process Methods 0.000 claims description 16
- 238000001816 cooling Methods 0.000 claims description 13
- 238000009987 spinning Methods 0.000 claims description 12
- 238000012545 processing Methods 0.000 claims description 8
- 238000002844 melting Methods 0.000 claims description 7
- 230000008018 melting Effects 0.000 claims description 7
- 239000012298 atmosphere Substances 0.000 claims description 6
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 4
- 229920001778 nylon Polymers 0.000 claims description 4
- 239000001301 oxygen Substances 0.000 claims description 4
- 229910052760 oxygen Inorganic materials 0.000 claims description 4
- 239000004677 Nylon Substances 0.000 claims description 2
- 230000007423 decrease Effects 0.000 description 11
- 239000013078 crystal Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 6
- 230000000052 comparative effect Effects 0.000 description 4
- WSFSSNUMVMOOMR-UHFFFAOYSA-N Formaldehyde Chemical compound O=C WSFSSNUMVMOOMR-UHFFFAOYSA-N 0.000 description 3
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- WNLRTRBMVRJNCN-UHFFFAOYSA-N adipic acid Chemical compound OC(=O)CCCCC(O)=O WNLRTRBMVRJNCN-UHFFFAOYSA-N 0.000 description 2
- 229920001577 copolymer Polymers 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- NAQMVNRVTILPCV-UHFFFAOYSA-N hexane-1,6-diamine Chemical compound NCCCCCCN NAQMVNRVTILPCV-UHFFFAOYSA-N 0.000 description 2
- 239000004816 latex Substances 0.000 description 2
- 229920000126 latex Polymers 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000006864 oxidative decomposition reaction Methods 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 238000006116 polymerization reaction Methods 0.000 description 2
- GHMLBKRAJCXXBS-UHFFFAOYSA-N resorcinol Chemical compound OC1=CC=CC(O)=C1 GHMLBKRAJCXXBS-UHFFFAOYSA-N 0.000 description 2
- QAOWNCQODCNURD-UHFFFAOYSA-N sulfuric acid Substances OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 1
- 235000003403 Limnocharis flava Nutrition 0.000 description 1
- 244000278243 Limnocharis flava Species 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 239000001361 adipic acid Substances 0.000 description 1
- 235000011037 adipic acid Nutrition 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005537 brownian motion Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000010622 cold drawing Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000009661 fatigue test Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000012770 industrial material Substances 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 239000013081 microcrystal Substances 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000008707 rearrangement Effects 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 230000007847 structural defect Effects 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Spinning Methods And Devices For Manufacturing Artificial Fibers (AREA)
- Artificial Filaments (AREA)
Description
産業上の利用分野
本発明は、高強度高耐疲労性ナイロン66繊維の
製造法に関する。
従来の技術
ナイロン66繊維はその耐疲労性、強力、弾性、
回復力やゴム、樹脂やプラスチツクとの接着性が
他の繊維に比べて優れているので、タイヤコード
やカーペツトなどの産業資材分野に広く応用され
ている。しかるに、従来使用されてきたナイロン
66繊維は、強度の高いものは耐疲労性が劣り、耐
疲労性があるものは強度が劣るという欠点を有し
ていた。すなわち、従来公知の方法では、耐疲労
性および強度の両者共に優れているナイロン66繊
維を得ることはできなかつた。従来のナイロン66
繊維は、冷延伸もしくは融解温度以下での熱延伸
(例えば、ゾーン延伸ゾーン熱処理(T.Kunugiet
al;Polymer Preprints,Japan31(No.4),761
(1982))により強度、弾性率を向上させている。
しかし、この方法では結晶領域を連結するところ
のいわゆるタイ(tie)分子鎖の比率が高まり、
非晶領域の緊張度が増すため、耐疲労性が劣るこ
とが、ナイロン66繊維の微細構造と繊維の力学物
性との間の相関性を研究した結果、明らかとなつ
た。
発明が解決しようとする問題点
本発明者らはナイロン66繊維の微細構造と耐疲
労性、高強度、高弾性率との間の相関性を研究
し、Tnaxおよび(tan〓)naxと繊維の力学物性(強
度、弾性率、耐疲労性など)との間に密接な関係
があることを見い出し、高強力でかつ高耐疲労性
繊維の微細構造として伸び切り鎖の比率が高くか
つ非晶領域内部の分子鎖の緊張度が少ない構造が
必要であるとの知見を得、これに基づいて本発明
を完成するに至つた。
本発明の目的は、高強度でしかも耐疲労性に優
れたナイロン66繊維の製造法を提供するにある。
問題点を解決するための手段
本発明に係る高強度高耐疲労性ナイロン66繊維
の製造法は、紡速4000m/min以上で紡糸された
ナイロン66繊維を熱処理するに際し、
(1) 該繊維の繊維軸方向にかかる張力の大きさ
が、0.5(g/d)以上で且つ0.99T(g/d)
(但し、Tは該繊維の引張り破断時の強度であ
る)以下、
(2) 実質的に酸素が存在しない雰囲気中におい
て、
(3) 熱処理温度が240℃を超えて、Tm3+
5/9×102υ〔但し、Tm3は昇温速度10℃/min
で測定されるDSC融解曲線の基線にもどる温
度(図3を参照)、υは処理速度(mm/min)
である。〕未満で、
(4) 繊維軸方向の長さl(mm)が1≦l≦1+
4υ+5d/1.5θ(ここで、υは処理速度(mm/min)、
dは該繊維のデニール、θは熱処理温度(℃)
である)である熱処理ゾーンで熱処理し、次い
で
(5) 温度勾配の絶対値が|300|(℃/cm)以上
で、−60℃以下の冷却温度に冷却する、
ことを特徴とする。
なお、本発明において、「ナイロン66繊維」と
は、実質的にヘキサメチレンジアミンとアジピン
酸より重合されるポリヘキサメチレンアジパミド
で構成される繊維を意味し、ポリヘキサメチレン
アジパミドの特性が損なわれない限り、少量の他
の共重合成分を含むコポリアミドの繊維であつて
もよいし、他の高分子との混合物で構成される繊
維であつてもよい。ナイロン66繊維の重合度は高
ければ高いほど力学的破壊強度が増大するので望
ましく、特に粘度平均分子量M〓(95%濃硫酸中に
て測定、粘度式〔η〕=2.5+0.0209M0.832による)
が42000以上であるものが望ましい。
本発明による製造法で得られるナイロン繊維の
第1の特徴は、測定周波数110Hzにおける力学的
損失正接のピーク値〔(tan〓)nax〕に対する温度
(Tnax)が100℃未満で、かつピーク値〔(tan〓)na
x〕が0.06を超えて0.10未満である点にある。な
お、従来の衣料用繊維の(tan〓)naxは0.09〜0.13
に分布し、Tnaxは120℃以上である。また、冷延
伸あるいはゾーン延伸ゾーン熱処理法で得られる
繊維の(tan〓)naxは0.04以下で、Tnaxは110℃以上
である。
Tnaxが100℃未満であると、tie分子鎖の比率が
少なくかつ非晶領域内部の分子鎖の緊張度が低
い。この緊張度の低下に原因して、Tnax<100℃
の繊維は耐疲労性に優れた特性を有する繊維とな
る。Tnaxが100℃以上であると、tie分子鎖比率が
増すために、非晶領域内部の分子鎖の緊張度が増
し、おそらくこれが原因して耐疲労性は低下す
る。耐疲労性はTnaxが低ければ低いほど上昇す
るが、Tnaxが低くなるに従つて30℃における弾
性率が低下する傾向がある。したがつて紡糸、後
処理技術のうえでTnaxの下限値が決定される。
また、無定形領域内部の分子鎖の中で主鎖のミ
クロブラウン運動が可能な成分の量を反映する
(tan〓)naxの値については、0.060を超えて、0.10
未満の範囲である必要がある。(tan〓)naxの値が
この範囲に入つていると、耐疲労性が高くかつ30
℃における弾性率もすぐれ、強度も高い。(tan〓)
naxが0.060以下であると、耐疲労性が劣る。ま
た、(tan〓)naxが0.10以上であると強度の低下が著
しい。
本発明による製造法で得られるナイロン繊維の
第2の特徴は、該繊維の中心部分に於ける平均複
屈折率(Δn(0))の値が5.8×10-2以上である点に
ある。平均複屈折率は繊維の結晶部分および非晶
部分の分子鎖の配向に強く依存する。Δn(0)が5.8
×10-2以上であれば、伸び切り鎖比率が高く、分
子鎖の繊維軸方向への配向度も高い為に、繊維の
強度、弾性率、耐疲労性が高い。Δn(0)が5.8×
10-2未満であると、伸び切り鎖比率が減少し、強
度、弾性率の低下が著しい。
こうして本発明の製造法で得られた高強度でか
つ耐疲労性の優れたナイロン66繊維は従来公知の
繊維とは異なつた特異な微細構造を持つといえ
る。
本発明の製造法の第1の特徴は、紡速4000m/
min以上で紡糸された高速紡糸繊維を使用する点
にある。ここで「紡速」とは、第2図に示すよう
に常用される紡糸装置において、紡糸ヘツド2か
ら吐出され、管状加熱域3、流体吸収装置4、油
剤付与装置5および集束装置6を順次経由した糸
条1が引取りロール7にて引取られる速度を意味
する。本発明を貫ぬく基本的な原理は、繊維に含
まれる高融点の伸び切り分子鎖に着目し、それ以
外の低融点の結晶部分を高張力下で局所加熱して
融解させ分子鎖を引き延ばし、続く急冷処理で伸
び切り分子鎖を基に再結晶化させ、この時同時に
非晶領域分子鎖も固定化するものである。従つ
て、用いる繊維は伸び切り分子鎖をより多く含む
必要がある。紡速4000m/min未満の繊維では、
伸び切り分子鎖をほとんど含まないが、4000m/
min以上で紡糸された繊維は伸び切り分子鎖を多
く含む。紡糸速度が高いほど伸び切り分子鎖を多
く含む。本発明において、紡速4000m/minで紡
糸された繊維を使用するのはそのためである。な
お、紡速5500m/min以上で紡糸された高速紡糸
繊維であるとより好ましい。
本発明の製造法の第2の特徴は、熱処理時に糸
にかかる張力の大きさが0.5(g/d)以上で糸の
引張破断時に於ける強度Tに0.99をかけた値
0.99T(g/d)以下に保持する点にある。強度
が0.5g/d未満であると、局所加熱により融解
した領域内の分子鎖は十分に引き延ばされずに続
く急冷ゾーンで固定化されてしまうので強度、弾
性率の顕著な増大は起らない。また、0.99T
(g/d)を超えると局所加熱中に糸切れが発生
する頻度が高く、処理が不可能となる場合が多
く、また、もう不可能ではないとしても、巨視的
な欠陥部が発生しやすく、強度・弾性率が逆に低
下し耐疲労性も劣る。
本発明による製造法の第3の特徴は、実質的に
酸素が存在しない雰囲気中で処理を行なう点にあ
る。本発明による処理は、上述のようにかなり高
温で行なうために、雰囲気中に酸素が存在すると
繊維の酸化分解が起こり強度、弾性率の低下を招
く。従つて、熱処理は窒素ガスなどの不活性気体
雰囲気下で行なう。なお処理を真空中で行なうと
糸の酸化分解を防ぐと共に糸の重合度が増大し、
糸の力学的性質が向上するのでより望ましい。
本発明による製造法の第4の特徴は、240℃を
超えてTm3+5/9×102υ(但し、Tm3は、昇温速
度10℃/minで測定される第3図に示すような
DSC融解曲線の基線Gにもどる温度、υは処理
速度(mm/min)である。)未満の温度で、局所
加熱する点にある。ここで「局所加熱」とは、繊
維をできるだけ狭い領域で加熱し、伸び切り分子
鎖以外の結晶領域を融解させる操作である。糸を
なるべくむらなく加熱するためおよび応力を最も
効率的に加熱部に集中させるためには、糸を加熱
する加熱ゾーンの繊維軸方向の長さl(mm)は、
処理速度υ(mm/min)、処理温度θ(℃)、糸の繊
度d(デニール)からなる関係式:1≦l≦1+
4υ+5d/1.5θを満足することが必要である。糸が240
℃以下で局所加熱されると、実質的に折りたたみ
鎖結晶や他の微結晶などの低融解温度成分が融解
されず、従つて伸び切り分子鎖の比率は高まら
ず、非晶領域内の分子鎖の緊張、結晶間を結ぶ
tie分子鎖の緊張度の増大、巨視的な構造欠陥な
どを引き起こすので、糸の耐疲労性の低下、強度
の低下を引き起こす。熱処理温度が240℃を超え
て、Tm3+5/9×102υ未満であると、結晶成分の
組みかえ(水素結合方向の結晶の成長)が起こ
り、非晶領域を含めた、伸び切り鎖への再結晶化
が促進され、伸び切り鎖比率の増大が起こり、強
度、弾性率の増大が著しい。特に従来不可能とさ
れていたTm3以上でTm3+5/9×102υ未満の温
度での熱処理は第5の特徴で述べる|300|℃/
cm以上の急激な温度勾配による冷却で初めて実現
され、この温度での熱処理による伸び切り鎖比率
の増大は著しい。熱処理温度がTm3+5/9×102υ
以上であると糸の融け切れが多く、実質的に処理
が不可能となる。
本発明による製造法の第5の特徴は、局所加熱
の後、温度勾配の絶対値が|300|(℃/cm)以上
で、−60℃以下の冷却温度に冷却する点にある。
|300|(℃/cm)以上の温度勾配があると、局
所加熱で融解した分子鎖の繊維軸方向への配向が
即座に固定化される(Tm3+5/9×102υ未満の温
度で熱処理できるのはこの為と考えられる)の
で、配向度が著しく増大し、伸び切り鎖の比率が
高まるので、強度・弾性率の増大が起こる。また
−60℃以下への冷却によつて、非晶領域の分子鎖
はtie分子鎖の比率が低く、緊張度が小さいけれ
ども比較的繊維軸方向への配向度が高い状態で瞬
間的に固定化されるので、強度、弾性率とともに
耐疲労性が高い繊維となる。|300|(℃/cm)未
満の温度勾配であると、局所加熱で融解した分子
鎖への応力集中が小さく伸び切り鎖の比率は高ま
らない。また、−60℃より高い冷却温度では、瞬
間的な非晶領域内の分子鎖の固定化が不充分で、
得られる糸は強度、弾性率および耐疲労性の面で
劣る。
本発明に係る繊維を特徴づける構造および物性
値は次のように測定される。
〔力学的損失正接(tan〓)および動的弾性率
(E′)〕
力学的損失正接(tan〓)および動的弾性率
(E′)の測定には、東洋ポールドウイン社製レ
オ・バイブロン(Rheo−Vibron)DDV−c型
を用いる。測定周波数110Hz、昇温速度10℃/
min、乾燥空気中でtan〓−温度(T)特性、E′−
温度(T)特性を測定する。tan〓−T曲線から
tan〓ピーク高さ(tan〓)naxとtan〓ピーク温度
(Tnax)とを読みとる。なお、測定前には試料は
48時間以上相対湿度0%の雰囲気下で調整され
る。
〔平均複屈折率Δn(0)〕
Ernst Leitz Wetzlar製偏光顕微鏡SM−LUX
−POLを用いて、波長546nmの光で、Berek
Compensator法により繊維の中心部分の複屈折
率Δn(0)を測定した。
〔強伸度〕
東洋ボールドウイン社製、Tensilon−UM−
−20型引張試験機により、20℃60%R.H.(相対湿
度)の条件下で、初長10cm、引張速度10cm/min
で測定した。
〔耐疲労性試験〕
ナイロン66フイラメント(840d/260f)に48
回/10cmずつ上撚および下撚加工し、以下の組成
をもつレゾルシン−ホルムアルデヒド−ラテツク
ス系接着剤に浸せきし、次いで、230℃において
3分間熱処理した。
成 分 重量部
レゾルシン 11.0
水 238.4
ホルムアルデヒド 16.2
水酸化ナトリウム 0.3
スチレン−ブタジエン−ビニルピリジン共重合
体ラテツクス(固形分41重量%) 244.0
509.9
このようにして得た処理コードについて、グツ
ドイヤー式チユーブ疲労試験機を用いてJISL−
1017(チユーブ疲労強さA法)に従い、チユーブ
疲労試験を行なつた。
実施例
以下、実施例について本発明を具体的に説明す
る。
相対粘度(UR)82(25℃、濃硫酸)のナイロ
ン66を孔径0.23mm、孔数12の紡糸口金より295℃
で熔融紡糸し、冷却し、油剤付与によつて集束性
を与え、引取り速度5500m/minで引き取つた。
この試料を、窒素雰囲気下、張力の大きさ0.9T
(g/d)の状態下、熱処理温度260,265,270
(±1℃)で0.7sec局所加熱後、450℃/cm以上の
温度勾配で−196℃まで急速冷却し、実施例No.2,
No.3,No.4の本発明による製造法で得られた繊維
を得た。これらの試料について、(tan〓)nax,Tnax,
Δn(0),30℃および150℃における貯蔵弾性率E′30,
E′150(GPa)、耐疲労性、強度(g/d)、伸度
(%)、の各数値を測定した。結果は表1に示す通
りである。
なお、比較例として、未処理糸(No.1)、0.9T
(g/d)の張力で熱処理温度260℃、温度勾配
250℃/cmで冷却温度10℃に冷却して得た糸(No.
5)、熱処理温度230℃、温度勾配290℃/cmで、
冷却温度−60℃に冷却して得た糸(No.6)、市販
旭化成ナイロン66タイヤコード(1260d/210f)
(No.7)の構造・物性の各数値を実施例と比較し
て表1に示した。
INDUSTRIAL APPLICATION FIELD OF THE INVENTION The present invention relates to a method for producing high-strength, high-fatigue-resistant nylon 66 fibers. Conventional technology Nylon 66 fiber is characterized by its fatigue resistance, strength, elasticity,
Because it has superior resilience and adhesion to rubber, resin, and plastic compared to other fibers, it is widely applied in the field of industrial materials such as tire cords and carpets. However, the nylon that has traditionally been used
66 fibers had the disadvantage that those with high strength had poor fatigue resistance, and those with fatigue resistance had poor strength. That is, by conventionally known methods, it has not been possible to obtain nylon 66 fibers that are excellent in both fatigue resistance and strength. conventional nylon 66
The fibers can be cold-stretched or hot-stretched below their melting temperature (e.g., zone-stretch zone heat treatment (T. Kunugiet
al; Polymer Preprints, Japan31 (No. 4), 761
(1982)) to improve strength and elastic modulus.
However, this method increases the proportion of so-called tie molecular chains that connect crystal regions,
A study of the correlation between the microstructure of nylon 66 fibers and the mechanical properties of the fibers revealed that fatigue resistance is poor due to the increased tension in the amorphous region. Problems to be Solved by the Invention The present inventors studied the correlation between the microstructure of nylon 66 fibers, fatigue resistance, high strength, and high elastic modulus, and found that T nax and (tan〓) nax and fiber We found that there is a close relationship between the mechanical properties (strength, elastic modulus, fatigue resistance, etc.) of fibers, and found that the microstructure of highly strong and highly fatigue resistant fibers has a high ratio of extended chains and is amorphous. We found that a structure with low tension in the molecular chains inside the region is required, and based on this we completed the present invention. An object of the present invention is to provide a method for producing nylon 66 fibers that have high strength and excellent fatigue resistance. Means for Solving the Problems The method for producing high-strength, high-fatigue-resistant nylon 66 fibers according to the present invention includes: (1) when heat treating nylon 66 fibers spun at a spinning speed of 4000 m/min or more; The magnitude of the tension applied in the fiber axis direction is 0.5 (g/d) or more and 0.99T (g/d)
(However, T is the tensile strength of the fiber at break.) Below, (2) in an atmosphere substantially free of oxygen, (3) at a heat treatment temperature exceeding 240°C, Tm 3 +
5/9×10 2 υ [However, Tm 3 is the temperature at which the DSC melting curve returns to the baseline measured at a heating rate of 10°C/min (see Figure 3), υ is the processing speed (mm/min)
It is. ], (4) Length l (mm) in the fiber axis direction is 1≦l≦1+
4υ+5d/1.5θ (where, υ is the processing speed (mm/min), d is the denier of the fiber, and θ is the heat treatment temperature (℃)
), and then (5) cooling to a cooling temperature where the absolute value of the temperature gradient is |300|(°C/cm) or more and -60°C or less. In the present invention, "nylon 66 fiber" means a fiber substantially composed of polyhexamethylene adipamide polymerized from hexamethylene diamine and adipic acid, and the characteristics of polyhexamethylene adipamide It may be a copolyamide fiber containing a small amount of other copolymer components, or a fiber composed of a mixture with other polymers, as long as the properties are not impaired. The higher the polymerization degree of nylon 66 fibers, the higher the mechanical breaking strength, so it is desirable, especially the viscosity average molecular weight M〓 (measured in 95% concentrated sulfuric acid, according to the viscosity formula [η] = 2.5 + 0.0209M 0.832 )
It is desirable that the value is 42000 or more. The first characteristic of the nylon fiber obtained by the manufacturing method according to the present invention is that the temperature (T nax ) with respect to the peak value [(tan〓) nax ] of the mechanical loss tangent at a measurement frequency of 110 Hz is less than 100°C, and the peak value [(tan〓) na
x ] is greater than 0.06 and less than 0.10. In addition, the (tan〓) nax of conventional clothing fibers is 0.09 to 0.13.
distribution, and T nax is over 120℃. Furthermore, the (tan〓) nax of the fiber obtained by cold drawing or zone drawing zone heat treatment method is 0.04 or less, and T nax is 110° C. or more. When T nax is less than 100°C, the ratio of tie molecular chains is small and the tension of the molecular chains inside the amorphous region is low. Due to this decrease in tension, T nax <100℃
The fibers have excellent fatigue resistance. When T nax is 100°C or higher, the tie molecular chain ratio increases, which increases the tension of the molecular chains inside the amorphous region, and this is probably the reason why fatigue resistance decreases. The fatigue resistance increases as T nax decreases, but as T nax decreases, the elastic modulus at 30°C tends to decrease. Therefore, the lower limit of T nax is determined based on spinning and post-processing technology. In addition, the value of nax , which reflects the amount of components capable of micro-Brownian motion of the main chain in the molecular chain inside the amorphous region (tan〓), exceeds 0.060 and exceeds 0.10.
Must be within the range below. (tan〓) If the nax value is within this range, fatigue resistance is high and 30
It has excellent elastic modulus at °C and high strength. (tan〓)
When nax is 0.060 or less, fatigue resistance is poor. Moreover, when (tan〓) nax is 0.10 or more, the strength decreases significantly. A second feature of the nylon fiber obtained by the production method of the present invention is that the average birefringence (Δn (0) ) in the central portion of the fiber is 5.8×10 −2 or more. The average birefringence strongly depends on the orientation of molecular chains in the crystalline and amorphous portions of the fiber. Δn (0) is 5.8
If it is ×10 -2 or more, the ratio of elongated chains is high and the degree of orientation of the molecular chains in the fiber axis direction is also high, so the strength, elastic modulus, and fatigue resistance of the fiber are high. Δn (0) is 5.8×
When it is less than 10 -2 , the ratio of fully extended chains decreases, and the strength and elastic modulus decrease significantly. Thus, it can be said that the nylon 66 fibers with high strength and excellent fatigue resistance obtained by the production method of the present invention have a unique microstructure different from conventionally known fibers. The first feature of the production method of the present invention is a spinning speed of 4000 m/
The point is to use high-speed spun fibers spun at a speed of min or more. Here, "spinning speed" means that in a commonly used spinning device as shown in FIG. This refers to the speed at which the yarn 1 that has passed through is taken up by the take-up roll 7. The basic principle underlying the present invention is to focus on the high-melting-point extended molecular chains contained in the fiber, and to elongate the molecular chains by locally heating and melting the other low-melting-point crystal parts under high tension. In the subsequent rapid cooling treatment, the elongated molecular chains are recrystallized, and at the same time, the amorphous region molecular chains are also immobilized. Therefore, the fibers used need to contain more extended molecular chains. For fibers with a spinning speed of less than 4000m/min,
4000m/
Fibers spun at min or more contain many elongated molecular chains. The higher the spinning speed, the more elongated molecular chains are included. This is why fibers spun at a spinning speed of 4000 m/min are used in the present invention. In addition, it is more preferable to use high-speed spun fibers spun at a spinning speed of 5500 m/min or more. The second feature of the manufacturing method of the present invention is that when the tension applied to the yarn during heat treatment is 0.5 (g/d) or more, the strength T at the time of tensile breakage of the yarn is multiplied by 0.99.
The point is to keep it below 0.99T (g/d). If the strength is less than 0.5 g/d, the molecular chains in the region melted by local heating will not be sufficiently stretched and will be fixed in the subsequent quenching zone, so no significant increase in strength or elastic modulus will occur. . Also, 0.99T
(g/d), yarn breakage occurs frequently during local heating, making processing impossible in many cases, and even if it is not impossible, macroscopic defects are likely to occur. On the contrary, the strength and elastic modulus decrease, and the fatigue resistance is also inferior. A third feature of the manufacturing method according to the invention is that the treatment is carried out in an atmosphere substantially free of oxygen. Since the treatment according to the present invention is carried out at a considerably high temperature as described above, the presence of oxygen in the atmosphere causes oxidative decomposition of the fibers, resulting in a decrease in strength and elastic modulus. Therefore, the heat treatment is performed under an inert gas atmosphere such as nitrogen gas. Furthermore, if the treatment is carried out in a vacuum, it will prevent the oxidative decomposition of the thread and increase the degree of polymerization of the thread.
This is more desirable because it improves the mechanical properties of the yarn. The fourth feature of the manufacturing method according to the present invention is that Tm 3 +5/9×10 2 υ (where Tm 3 is measured at a heating rate of 10°C/min as shown in Figure 3) at temperatures exceeding 240°C. Na
The temperature at which the DSC melting curve returns to the baseline G, υ, is the processing speed (mm/min). ) at the point of local heating. Here, "local heating" is an operation in which the fiber is heated in as narrow a region as possible to melt crystal regions other than the extended molecular chains. In order to heat the yarn as evenly as possible and to concentrate stress in the heating zone most efficiently, the length l (mm) in the fiber axis direction of the heating zone that heats the yarn is:
Relational expression consisting of processing speed υ (mm/min), processing temperature θ (°C), and yarn fineness d (denier): 1≦l≦1+
It is necessary to satisfy 4υ+5d/1.5θ. When the yarn is locally heated below 240 °C, the low melting temperature components such as folded chain crystals and other microcrystals are not substantially melted, and therefore the proportion of extended molecular chains does not increase, and the Tension in molecular chains, connecting crystals
This causes an increase in the tension of the tie molecular chains and macroscopic structural defects, resulting in a decrease in the fatigue resistance and strength of the yarn. When the heat treatment temperature exceeds 240℃ and is lower than Tm 3 +5/9×10 2 υ, rearrangement of crystal components (growth of crystals in the direction of hydrogen bonds) occurs, resulting in the formation of extended chains, including amorphous regions. recrystallization is promoted, the ratio of extended chains increases, and the strength and elastic modulus increase significantly. In particular, heat treatment at temperatures above Tm 3 and below Tm 3 +5/9×10 2 υ, which was considered impossible in the past, is described in the fifth feature |300|℃/
This was achieved for the first time by cooling with a sharp temperature gradient of cm or more, and the increase in the proportion of fully extended chains by heat treatment at this temperature is remarkable. If the heat treatment temperature is Tm 3 +5/9×10 2 υ or more, the yarn will melt and break so much that the treatment becomes virtually impossible. The fifth feature of the production method according to the present invention is that after local heating, the temperature gradient is cooled to a cooling temperature of -60°C or less with an absolute value of |300|(°C/cm) or more. If there is a temperature gradient of |300| (°C/cm) or more, the orientation of the molecular chains melted by local heating in the fiber axis direction is immediately fixed (temperatures below Tm 3 + 5/9×10 2 υ). (This is thought to be the reason why heat treatment can be performed at 30° C.), the degree of orientation increases significantly and the ratio of fully extended chains increases, resulting in an increase in strength and modulus of elasticity. In addition, by cooling to -60℃ or below, the molecular chains in the amorphous region have a low ratio of tie molecular chains, and although the degree of tension is low, they are instantly fixed in a state with a relatively high degree of orientation in the fiber axis direction. As a result, the fiber has high strength, modulus of elasticity, and fatigue resistance. If the temperature gradient is less than |300|(°C/cm), the stress concentration on the molecular chains melted by local heating will be small and the ratio of fully extended chains will not increase. Furthermore, at cooling temperatures higher than -60°C, the immobilization of molecular chains within the instantaneous amorphous region is insufficient.
The resulting yarn has poor strength, modulus and fatigue resistance. The structure and physical property values characterizing the fiber according to the present invention are measured as follows. [Mechanical loss tangent (tan〓) and dynamic modulus of elasticity (E′)] To measure the mechanical loss tangent (tan〓) and dynamic modulus of elasticity (E′), a Leo Vibron manufactured by Toyo Poldwin Co., Ltd. was used. (Rheo-Vibron) DDV-c type is used. Measurement frequency 110Hz, heating rate 10℃/
min, tan〓−temperature (T) characteristic in dry air, E′−
Measure temperature (T) characteristics. From tan〓−T curve
Read tan = peak height (tan =) nax and tan = peak temperature (T nax ). Note that the sample must be
Conditioned in an atmosphere of 0% relative humidity for 48 hours or more. [Average birefringence Δn (0) ] Ernst Leitz Wetzlar polarizing microscope SM-LUX
- Berek using POL with light at a wavelength of 546 nm
The birefringence Δn (0) at the center of the fiber was measured using the Compensator method. [Strong elongation] Manufactured by Toyo Baldwin, Tensilon-UM-
-20 type tensile testing machine, initial length 10cm, tensile speed 10cm/min under conditions of 20℃ 60%RH (relative humidity)
It was measured with [Fatigue resistance test] 48 on nylon 66 filament (840d/260f)
The fabric was twisted and pre-twisted once per 10cm, immersed in a resorcinol-formaldehyde-latex adhesive having the following composition, and then heat-treated at 230°C for 3 minutes. Ingredients by weight Resorcinol 11.0 Water 238.4 Formaldehyde 16.2 Sodium hydroxide 0.3 Styrene-butadiene-vinylpyridine copolymer latex (solid content 41% by weight) 244.0 509.9 The treatment code thus obtained was tested using a Gutdeyer tube fatigue tester. Using JISL-
1017 (tube fatigue strength method A), a tube fatigue test was conducted. EXAMPLES The present invention will be specifically described below with reference to Examples. Nylon 66 with a relative viscosity (UR) of 82 (25°C, concentrated sulfuric acid) was spun at 295°C from a spinneret with a pore diameter of 0.23 mm and 12 holes.
The fibers were melt-spun, cooled, added with an oil agent to give them convergence, and taken off at a take-off speed of 5500 m/min.
This sample was tested under a nitrogen atmosphere with a tension of 0.9T.
(g/d), heat treatment temperature 260, 265, 270
After local heating at (±1℃) for 0.7 seconds, rapid cooling to -196℃ with a temperature gradient of 450℃/cm or more, Example No. 2,
Fibers No. 3 and No. 4 obtained by the manufacturing method according to the present invention were obtained. For these samples, (tan〓) nax, T nax,
Δn (0), storage modulus E′ 30 at 30℃ and 150℃,
E′ 150 (GPa), fatigue resistance, strength (g/d), and elongation (%) were measured. The results are shown in Table 1. In addition, as a comparative example, untreated yarn (No. 1), 0.9T
(g/d) tension, heat treatment temperature 260℃, temperature gradient
Yarn obtained by cooling at 250℃/cm to a cooling temperature of 10℃ (No.
5), heat treatment temperature 230℃, temperature gradient 290℃/cm,
Thread obtained by cooling to -60℃ (No. 6), commercially available Asahi Kasei nylon 66 tire cord (1260d/210f)
Table 1 shows the numerical values of the structure and physical properties of (No. 7) in comparison with those of Examples.
【表】
*は比較例
表1からわかるように、本発明による製造法で
得られた繊維に相当する実施例No.2,3,4は高
強力でかつ高耐疲労性ナイロン66繊維であること
がわかる。なお、本発明による製造法で得られた
繊維(No.4)と比較例品(No.5)及び(No.6)の
強伸度曲線を第1図に示す。[Table] * indicates comparative example. As can be seen from Table 1, Example Nos. 2, 3, and 4, which correspond to the fibers obtained by the manufacturing method of the present invention, are high strength and high fatigue resistant nylon 66 fibers. I understand that. In addition, the strength and elongation curves of the fiber (No. 4) obtained by the production method according to the present invention and comparative example products (No. 5) and (No. 6) are shown in FIG.
第1図は、本発明による製造法で得られた繊維
(実施例試料No.3)、比較例(試料No.5,No.6)の
強伸度曲線の比較を示した図である。第2図は、
本発明方法に用いるナイロン66高速紡糸繊維を紡
糸する装置の一例の概略図である。図において、
1は糸条、2は紡糸ヘツド、3は管状加熱域、4
は流体吸引装置、5は油剤付与装置、6は集束装
置、7は引取りローラーである。第3図はナイロ
ン66繊維の典型的なDSC融解曲線であり、Tm1,
Tm2,Tm3の説明図である。図において、Gは
基線である。
FIG. 1 is a diagram showing a comparison of strength and elongation curves of a fiber obtained by the production method according to the present invention (Example Sample No. 3) and a comparative example (Samples No. 5 and No. 6). Figure 2 shows
1 is a schematic diagram of an example of an apparatus for spinning nylon 66 high speed spun fibers used in the method of the present invention. In the figure,
1 is a yarn, 2 is a spinning head, 3 is a tubular heating area, 4
5 is a fluid suction device, 5 is an oil applying device, 6 is a focusing device, and 7 is a take-off roller. Figure 3 shows a typical DSC melting curve of nylon 66 fiber, with Tm 1 ,
It is an explanatory diagram of Tm 2 and Tm 3 . In the figure, G is the baseline.
Claims (1)
66繊維を熱処理するに際し、 (1) 該繊維の繊維軸方向にかかる張力の大きさ
が、0.5(g/d)以上で且つ0.99T(g/d)
(但し、Tは該繊維の引張り破断時の強度であ
る)以下、 (2) 実質的に酸素が存在しない雰囲気中におい
て、 (3) 熱処理温度が240℃を超えて、Tm3+
5/9×102υ〔但し、Tm3は昇温速度10℃/min で測定されるDSC融解曲線の基線にもどる温
度(図3を参照)、υは処理速度(mm/min)
である。〕未満で、 (4) 繊維軸方向の長さl(mm)が1≦l≦1+
4υ+5d/1.5θ(ここでυは処理速度(mm/min)、d は該繊維のデニール、θは熱処理温度(℃)で
ある)である熱処理ゾーンで熱処理し、次い
で、 (5) 温度勾配の絶対値が|300|(℃/cm)以上
で、−60℃以下の冷却温度に冷却する、 ことを特徴とする高強度高耐疲労性ナイロン66繊
維の製造法。[Claims] 1. Nylon spun at a spinning speed of 4000 m/min or more
66 When heat treating fibers, (1) the magnitude of the tension applied to the fiber axis in the fiber axis direction is 0.5 (g/d) or more and 0.99T (g/d)
(However, T is the tensile strength of the fiber at break.) Below, (2) in an atmosphere substantially free of oxygen, (3) at a heat treatment temperature exceeding 240°C, Tm 3 +
5/9×10 2 υ [However, Tm 3 is the temperature at which the DSC melting curve returns to the baseline measured at a heating rate of 10°C/min (see Figure 3), υ is the processing speed (mm/min)
It is. ], (4) Length l (mm) in the fiber axis direction is 1≦l≦1+
4υ + 5d/1.5θ (where υ is the processing speed (mm/min), d is the denier of the fiber, and θ is the heat treatment temperature (°C)), and then (5) the temperature gradient is A method for producing high-strength, high-fatigue-resistant nylon 66 fiber, characterized by having an absolute value of |300|(°C/cm) or more and cooling to a cooling temperature of -60°C or less.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15393784A JPS6134216A (en) | 1984-07-26 | 1984-07-26 | Nylon 66 fiber having high strength and high fatigue resistance, and its manufacture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15393784A JPS6134216A (en) | 1984-07-26 | 1984-07-26 | Nylon 66 fiber having high strength and high fatigue resistance, and its manufacture |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6134216A JPS6134216A (en) | 1986-02-18 |
| JPH0571683B2 true JPH0571683B2 (en) | 1993-10-07 |
Family
ID=15573339
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15393784A Granted JPS6134216A (en) | 1984-07-26 | 1984-07-26 | Nylon 66 fiber having high strength and high fatigue resistance, and its manufacture |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6134216A (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4054072B2 (en) * | 1994-12-09 | 2008-02-27 | 株式会社ブリヂストン | Pneumatic radial tire |
| JP3792764B2 (en) * | 1995-12-08 | 2006-07-05 | 株式会社ブリヂストン | Pneumatic radial tire |
| US8864057B2 (en) | 2011-11-04 | 2014-10-21 | Shaw Industries Group, Inc. | Processes for recycling carpet and products of such processes |
| KR102858092B1 (en) * | 2020-06-23 | 2025-09-10 | 코드사 테크닉 테크스틸 아노님 시르케티 | High-strength nylon 6.6 yarn |
-
1984
- 1984-07-26 JP JP15393784A patent/JPS6134216A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6134216A (en) | 1986-02-18 |
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