ޘड़ᑕ̈́Ԯᖼຫ๋၆
Gr/PEEK ᎕ᆸڕคШᐖၗૻޘᄃি౻ုᇆᜩ̝ࡁտ
ܘϖ̌
઼ϲလཌྷ̂ጯϠۏ፟̍ጯր
ཧᅛߵ ӓރጳ
઼ϲර̂ጯજ˧፟ୠ̍ጯր
ၡ! ࢋ
дώࡁտ̚Ăֹϡ၁រ៍၅͞ё၆ሤّኑЪՄफ़(Gr/PEEK)צזޘٕ
Ԯᖼຫ๋ޢĂᐖၗٛҩૻޘᄃি౻ုٙצזᇆᜩซҖࡁտĄϤ၁រඕڍޝ
ۢĂޘड़ᑕ၆ٺᐖၗٛҩૻޘ֭՟ѣᇆᜩĂҭ၆ٺি౻ုݒѣٙຫ चĄ҃Ԯᖼຫ๋ົࢫҲٛҩૻޘᄃি౻ုĄТॡĂϤ၁រඕڍΞ൴னĂགྷ Ԯᖼຫ๋Гགྷޘᇆᜩٙౄј۞ຫ๋ົͧགྷޘᇆᜩޢГགྷԮᖼຫ๋ٙౄј
۞ຫ๋ᚑࢦĄΩ˘͞ࢬĂ၆̏צזຫ๋۞ྏͯд200oC ซҖሤᑅ࣒ྃĂ֭ͷࡁ տ࣒ྃޢ۞ྏͯᐖၗٛҩૻޘᄃি౻ုĄޝځព۞Ăሤᑅ࣒ྃޢ۞ྏͯ
௲ᆸࢬ᎕ົត͌ĄЯѩĂ၆ٺዎצԮᖼຫ๋ٕ۰གྷޘᇆᜩ۞ྏͯĂགྷ200oC ሤᑅ࣒ྃޢি౻ုົᆧΐĄ҃ޘᄃԮᖼ̝ม߉ΐдྏͯ˯۞ึԔĂ၆ٺ
࣒ྃޢ۞ྏͯдি౻ု˯۞ᇆᜩ̙̂Ą ᙯᔣෟĈᐖၗٛҩૻޘăি౻ုăሤᑅ࣒ྃĄ
STUDY ON TEMPERATURE AND TORSION-DAMAGED EFFECTS ON STATIC STRENGTH AND FATIGUE LIFE OF THE GRAPHITE/PEEK
COMPOSITE LAMINATES
Yung-Chuan Chiou
Department of Biomechatronic Engineering National Chiayi University Chiayi, Taiwan 600, R.O.C.
Ming-Chuen Yip Wei-Hsien Wu
Department of Power Mechanical Engineering National Tsing- Hua University
Hsinchu, Taiwan, 300, R.O.C.
Key Words: ultimate strength, fatigue life, thermoforming repair.
ABSTRACT
By experimental observation, the effects of temperature and torsion-
damage on ultimate strength and fatigue life were investigated, respectively,
for the Graphite/PEEK laminate in this study. It is evident from the
experimental results that there is no influence on residual strength after exposure to temperature changes. But temperature change effects are detrimental to the fatigue life. It can be found that the ultimate strength and fatigue are decreased life after torsion damage. Furthermore, by comparing the experimental results, it is found that the damage from temperature change effects after twisting is more serious than the damage from twisting after temperature changes. Meanwhile, the damaged specimens are repaired by thermoforming at a temperature of 200
oC. The corresponding static strength and fatigue life are also investigated in this study. Obviously, due to torsion-damage or temperature change effects, the area of delamination can be improved by thermoforming. Hence, the thermoforming method can increase the fatigue life of a specimen that has experienced temperature changes or twisting. It is noted that temperature and twist action has less influence on fatigue life for the repaired specimens.
˘ă݈ ֏
ܕѐֽ၆ٺ፟ୠ̮Іనࢍ˯۞ࢋՐߏૻޘ̈́ᅅณ
̼ĄЯѩѣּͧૻޘ̈́ݏޘඈᐹᕇ۞ញჯૻ̶̼
̄ኑЪՄफ़צזޘڦϫĄϫ݈дਝ͉ຽăՠ֘ຽ̈́ྻજ ጡՄඈ࠹ᙯ̍ຽĂኑЪՄफ़̏̂ณפܛᛳՄफ़҃జᇃھ
ֹϡĄّਕኑЪՄफ़ॲፂૄՄ(matrix)۞̙ТĂΞ̶ᙷј ሤّᄃሤّኑЪՄफ़̂ᙷĄ҃ሤّૄՄͧሤّ
ૄՄдᄦ˯ॡมൺͷᄦౄјώྵҲĂТॡѣྵ۞
ᗼิّăྵ̂۞ຫ๋टԡޘ̈́ྵҲ۞ޘӛќதඈᐹᕇĄ
҃ሤّኑЪՄफ़ΞͽࢦາΐሤႦᏉГ̼ĂЯѩΞٽٺ
࣒ྃĂ֭ࣘΞаќГӀϡ۞ᒖܲໄهĂֹሤّኑЪ Մफ़д̍ຽ˯ు႙צזࢦෛĄ
ϤኑЪՄफ़ٙј۞ၹІдວྻ̈́྅࿅̈́၁ᅫ
ٚצি౻ྶ̚ĂΞਕצזШԮ١۞үϡ҃ౄјຫ๋Ą Ϥ͛ᚥ[1-3]̚ΞۢĂኑЪՄफ़ዎצԮ١࿅̚Ă௲ᆸன෪ ҋྏͯ۞ᙝன֭ͷഈྏ̰ͯొјܜĂТॡĂᐌԮᖼ
Ѩ۞ᆧΐ௲ᆸޘົᚑࢦĄኑЪՄफ़Чᆸ̝มЯࠎ ፘ⟯ăញჯ̈́ញჯଵЕ͞Ш̙ТĂౄјᆸᄃᆸ̝มЯγࠧ
ޘ˯̿ॡĂ̙Т۞ሤᎶኮณ҃ጱሤᑕ˧யϠĂֹૄ
ՄயϠෘᓀԛјຫ๋Ą૱֍тਝ۩ጡдརࢳҖ̝
มĂٙ۞ᒖဩޘត̼ࠤ̂Ăԛј˘ሤೈᒖĂౄјૄՄ யϠෘᓀඈຫ๋ĄЯѩֹϡኑЪՄफ़ٙј۞ၹІĂื
҂ᇋזᒖဩޘ۞ត̼၆ၹІౄј۞ຫ๋̈́ု۞ᇆ ᜩĄ҃ᒖဩޘត̼၆ኑЪՄफ़۞ݏޘ̈́ি౻ု۞ᇆᜩ ᄃෘᓀ۞Ϡјඈ࠹ᙯ۞ࡁտт͛ᚥ[4-9]ٙ̚ϯĄ
Ϥͽ˯͛ᚥΞۢຫ๋ߏౄјኑЪՄफ़ݏޘ̈́ি౻ု
ഴ͌۞ЯĄ҃ኑЪՄफ़ၹІдֹϡ࿅̚ĂυؠົЯ γࠧྶăᒖဩֹ̈́ϡ̙༊ඈኜкЯ৵҃ౄјຫ๋Ą˘ό Մफ़ѣٙຫ๋ĂтڍਕдϏԆБᗼ݈ซҖዋ༊࣒ྃĂޭ
ೇՄफ़۞ྶٚצਕ˧ĂΞͽؼܜֹϡѐࢨĂࢫҲјώĄ
ૄٺ҂ᇋזၹІჯ࣒۞ܮӀّ̈́щБّĂሤّኑЪՄफ़
ٙѣ۞࣒ྃপّՀצזࢦෛĄҌٺሤّኑЪՄफ़࣒ྃ
ԫఙ͞ࢬĂགྷ૱జֹϡ۞࣒ྃ͞ڱࠎሤᑅ࣒ྃĄϤ͛ᚥ̚
[10-13] ពϯĂ̙Т۞ሤᑅ࣒ྃ୧ІົᇆᜩՄफ़࣒ྃޢ۞
ᐖၗૻޘᄃি౻ૻޘਕ˧Ą
ώ͛ϫ۞д៍၅ޘड़ᑕ(60ƨ72 ̈ॡ)̈́Ԯᖼຫ๋
(4°Ҍ 40°ć900 Ѩ)၆ញჯૻ̼ჸゝゝ⟮(Gr/PEEK)ሤ
ّኑЪՄफ़ૄᆸڕдᐖၗૻޘ̈́คШি౻ု۞ᇆᜩĂ֭
ኢགྷ࿅ޘड़ᑕ̈́Ԯᖼຫ๋АޢึԔ̙Тଐڶ˭Ăྏͯ
ᐖၗૻޘᄃি౻ု۞ត̼ĄТॡ၆̏צזຫ๋ྏͯซҖ ሤᑅ࣒ྃĂଣགྷሤᑅ࣒ྃޢᐖၗૻޘᄃি౻ု۞ត̼
࣒̈́ྃड़தĂԓ୕ᖣѩ၁រᇴፂޙ˘ྤफ़ऱĂүࠎ͟ޢ࣒
ྃ̍ү˯̝ણ҂Ą
˟ă၁រ̰ट
ώ ࡁ տ ၆ ሤ ّ ኑ Ъ Մ फ़ ů ჸ ゝ ゝ ⟮ ([0/45/90/-45]2s Gr/PEEK)᎕ᆸڕ۞ᐖၗໂࢨૻޘ(ultimate strength)̈́ি౻ૻޘ(fatigue strength)ซҖ၁រ̶ژĄ֭ͷ
̶ژѩ˘ኑЪՄफ़᎕ᆸڕдצזޘड़ᑕٕ۰Ԯᖼຫ๋
۞ଐڶ˭၆ᐖၗૻޘ̈́ি౻ု۞ᇆᜩĄТॡĂ៍၅
ᒖဩЯ৵߉ΐึԔ̙Тଐԛ˭ĂՄफ़۞ᐖၗണዶ
ૻޘ̈́ি౻ု۞ត̼Ąซ˘ՎଣĂሤᑅ࣒ྃ၆צז ᒖဩЯ৵ᇆᜩ˭Ă᎕ᆸڕՄफ़۞፟ୠّኳ˯ߏӎѣԼ චĄຫ๋ྏͯᄦౄᄃ࠹ᙯ۞၁រણᇴనؠͽ̈́၁រ߹
ᄃ̰टĂ̶т˭Ĉ 1. ྏͯᄦү
ֶፂ ASTMD3039-76 ۞ఢቑ᎕ᆸڕ̷౷ј࠹ᙯ۞
͎̇ĂޢГϡCN ቱӵڕ(end tab)ቱЪٺ᎕ᆸڕ˯Ă ͽԆј၁រྏͯĄٙԆј۞၁រྏͯγݭᄃྏ͎ͯ̇Ăт ဦ 1 ٙϯĄ၆ٙᄦј۞ྏͯĂд၁រ݈࠰ֹϡࢰگ C-Scan ซҖᑭീĂྏͯବೡඕڍтဦ 2 ٙϯĄࢰگବೡ Ξ࿅̙ТᗞҒӔன̙Т۞ྏͯࡍதĂТॡᑭീବೡ ඕڍΞۡତϤОܑ፟ᑕЕОֽĄЯѩĂΞۡତ៍၅ྏ
ͯ̚ౝ۞ٙд̈́ౝ۞̂̈Ąдѩࡁտ̚ĂЯֹϡ۞ྏ
ͯ࠰ࠎπڕېĂ߇ଳϡࢰگࡍ͞ё၆ྏͯซҖᑭീĂ
ܑ˘ ᐖၗٛҩૻޘ၁រඕڍ(Original ultimate strength;σo, residual strength;σ) Mean value σ/σo Mean value σ/σo
a 類試片 736.26 (MPa) e 類試片 703.90 (MPa) 95.60 (%) b 類試片 744.63 (MPa) 101.14 (%) f 類試片 700.27 (MPa) 95.11 (%) c 類試片 684.50 (MPa) 92.97 (%) g 類試片 666.23 (MPa) 90.49 (%) d 類試片 688.23 (MPa) 93.48 (%) h 類試片 660.73 (MPa) 89.74 (%)
127 (Gage length) 19.14
ဦ1 ྏ͎ͯ̇ဦ(unit: mm)
ဦ2 ࣧՄྏ̝ͯࢰگ C-Scan ဦ
ဦ3 གྷԮᖼ 900 Ѩޢ̝ࢰگ C-Scan ဦ
ဦ4 གྷ 60ƨ72 ̈ॡޘᇆᜩޢ̝ࢰگ C-Scan ဦ
ֹϡ۞ࢰگC-Scan ᑭീրࠎ AIT-5112 ݭĄϤᑭീඕ ڍΞ൴னώࡁտֹ̚ϡ۞ྏͯԆፋّ̂։рĄࠎܮӀ ᄲځͽ̈́ͧྵ࠹ᙯ۞၁រன෪Ăώ͛၆ٺ̏జᄦј᎕ᆸڕ
ྏͯჍࠎa ᙷྏͯĄ
(˘) Ԯᖼຫ๋ᄃޘड़ᑕనؠ
၆ٺԮᖼຫ๋నؠĂдώࡁտֹ̚ϡInstron-1322 ݭ ᗕคШি౻၁រ፟၆̏జᄦј᎕ᆸڕྏͯ߉ΐ900 Ѩ̝
ԮᖼྶĂ၆ྏͯ߉ΐ۞̂Ԯᖼ֎ࠎ 40°Ăͷ̂Ԯᖼ
֎ᄃ̈Ԯᖼ֎̝ͧଠטࠎ0.1Ăᐛதࠎ 0.5HzĄ၆ٺ̏జ ߉ΐѨԮᖼྶ۞ྏͯซҖࢰگC-Scan ᑭീĂΞ൴ன
ྏͯბ̈́ᙝቡனځព۞௲ᆸĂТॡྏͯ̚มϺѣ௲ᆸ
۞ϠјĄ߇дѩԮᖼણᇴనؠ˭Ăྏͯѣ௲ᆸ۞ᗼயϠĂ ᖣѩ˞ྋѩ˘Ԯᖼຫ๋၆Մफ़۞ᐖၗૻޘ̈́ি౻ု۞ᇆ ᜩĄѩ˘ѣԮᖼຫ๋۞ྏͯдώ͛̚జჍࠎ c ᙷྏ
ͯĄдώࡁտ̚၆ٺଣޘड़ᑕ၆ Gr/PEEK ኑЪՄफ़
᎕ᆸڕ۞ᇆᜩĂྏͯᄦౄ߹ߏa ᙷྏͯཉٺॸ˯ݭ
ޮޮᒅ၁រ፟̚Ăޘనؠд60ƨĂᒅޘࠎ༊ॡވ˭
۞ᒅޘĂཉٸॡมనࠎ72 ̈ॡĄ၆ٺ̏צזޘᇆᜩ˭۞
ྏͯซҖࢰگ C-Scan ᑭീĂϤဦ 3 Ξ࠻ྏ֭ͯ՟ѣ ຫ๋ĂЯѩ 60ƨ72 ̈ॡ۞ޘड़ᑕ̙֭ົ၆ྏͯயϠ௲ ᆸĄ၆ٺצזޘᇆᜩ˭۞ྏͯజჍࠎb ᙷྏͯĄώࡁտ
̚၆Ԯᖼຫ๋ޘड़ᑕᒖဩЯ৵ĂЯ߉ΐึԔ̙
Тଐԛ˭၆Մफ़۞ᇆᜩซҖ̶ژᄃ៍၅ĄЯѩ၆ٺАޘ ड़ᑕГགྷԮᖼຫ๋۞ྏͯჍࠎe ᙷྏͯĂАԮᖼຫ๋Гགྷ
ޘड़ᑕ۞ྏͯჍࠎg ᙷྏͯĄ (˟) ᑅ࣒ྃڱ
ሤᑅ࣒ྃ၆ٺ Gr/PEEK ኑЪՄफ़д࣒ྃ˯ѣᐹ ๕ĄЯࠎሤّૄՄдॡѣࢦّĂЯѩΞజࢦኑ
ֹϡĄҭሤᑅ࣒ྃ۞͞ёޘ̙Ξ͉Ăࡶޘ࿅ૄՄ
۞Ⴆᕇ(343ƨ)ĂऻѣౄјႦᏉېૄՄ߹εཱ̝ĂጱՄ फ़ّኳК̼ĄЯѩ࣒ྃޘ૱ᏴؠдૄՄ̝ࠟሬᖼೱޘ
Ⴆᕇ̝มĄώ͛ࠎ˞ྋሤᑅ࣒ྃ၆ٺצזԮᖼຫ๋ᄃ
ޘड़ᑕᇆᜩ˭۞࣒ྃड़ਕĂЯѩ၆c ᙷĂe ᙷᄃ g ᙷྏͯ
ཉٺሤᑅ፟̚ซҖ࣒ྃĄሤᑅ࣒ྃ୧Іߏֶፂ͛ᚥ[3]࣒
ྃޘؠࠎ 200ƨĂሤᑅᑅ˧ࠎ 6.89 MPa (1000 psi)Ăሤᑅ ॡมࠎ̶̣ᛗĂޢГٸˢ18ƨ̈́ 6.89 Mpa ۞ҽݒ፟̚
ާిҽݒ5 ̶ᛗĄ၆ٺ c ᙷĂe ᙷᄃ g ᙷˬᙷݭ۞ྏ
ͯдགྷ࣒ྃޢ̶ҾజჍࠎ d ᙷ f ᙷᄃ h ᙷݭྏͯĄ 2. ၁រણᇴనؠ
(˘) ᐖၗૻޘ၁រ
ώࡁտॲፂASTM D3039-76 ̝ᐖၗٛҩ၁រఢॾ၆ a ᙷĂb ᙷĂc ᙷĂd ᙷĂe ᙷĂf ᙷĂg ᙷᄃ h ᙷ۞ྏ̶ͯҾ ซҖᐖၗٛҩ၁រĄֹٙϡ۞၁រ፟ݭࠎ Instron-1322 ݭ ᗕคШি౻၁រ፟ĄଠטሀёࠎҖଠטĂӵᐝٛҩిத నؠࠎ0.01mm/sĂͽ႕֖၁រࠎᐖၗ۞నĄགྷѩ၁រ ΞפՄफ़۞ໂࢨૻޘ(σo)̈́ണዶૻޘ(σ )ĄՏᙷݭྏ
ͯണዶૻޘ۞πӮࣃ̂̈тܑ˘ٙϯĂͷπӮࣃ̂̈ઇ ࠎЧᙷݭྏͯซҖคШি౻၁រ̚ᑕ˧ॎ಼۞ણ҂Ą (˟) ি౻၁រ
ώࡁտ࠰ֹϡ Instron-1322 ݭᗕคШি౻၁រ፟၆ٙ
ѣᙷݭྏͯซҖคШি౻၁រĄଠטሀёࠎఈଠטĂᐛ தనؠࠎ3HzĂീྏگԛࠎϒؽگĄ၆ٺՏ˘ᙷݭ۞ྏͯ
࠰̶Ҿдαᑕ˧ॎ಼˭ซҖি౻၁រĂᐂি౻ု
(N )Ăͽޙϲᑕ˧ॎ಼ি౻ု̝ม۞ᙯాّĄ҃၁រf
̚۞ᑕ˧ॎ಼̂ࣃ࠰פҋٺໂࢨૻޘ(σo)ٕണዶૻޘ (σ)۞ 85%ă80%ă75%ă70%ă67%ĂТॡᑕ˧ͧ࠰ؠࠎ 0.1ĄՏ˘ᙷݭྏͯ۞ি౻၁រඕڍтܑ˟ٙЕĄ
ܑ˟ ٛҩি౻၁រඕڍ(ᑕ˧ͧࠎ 0.1)
a ᙷྏͯ b ᙷྏͯ c ᙷྏͯ d ᙷྏͯ
σa
(Mpa) Cycles
σa(Mpa) Cycles
σa(Mpa) Cycles
σa(Mpa) Cycles
281.62 1883 268.07 3469 246.42 4455 247.76 3324 281.62 243 268.07 956 246.42 2660 247.76 2099 281.62 2191 268.07 1003 246.42 1466 247.76 4615 265.05 5974 251.31 45724 231.02 22922 232.28 14260 265.05 12646 251.31 12726 231.02 2721 232.28 18412 265.05 3072 251.31 5776 231.02 25249 232.28 34107 248.49 24235 234.56 51392 215.62 65031 216.79 39182 248.49 19826 234.56 63564 215.62 61517 216.79 84581 248.49 31300 234.56 39139 215.62 40995 216.79 67507 231.92 106872 224.51 82669 206.38 125544 207.50 97332 231.92 154046 224.51 120200 206.38 66400 207.50 218000 221.98 300000 224.51 199730 206.38 253433 207.50 129606221.98 300000
e ᙷྏͯ f ᙷྏͯ g ᙷྏͯ h ᙷྏͯ
σa
(Mpa) Cycles
σa(Mpa) Cycles
σa(Mpa) Cycles
σa(Mpa) Cycles
253.40 4309 252.10 13718 239.84 1471 237.87 7889 253.40 2447 252.10 7068 239.84 1806 237.87 17529 253.40 1113 252.10 1248 239.84 1974 237.87 1990 237.57 15874 236.34 45065 224.85 10747 223.00 20647 237.57 11872 236.34 49278 224.85 6931 223.00 62513 237.57 4812 236.34 28153 224.85 30569 223.00 21237 221.73 48391 220.59 89622 209.86 119120 208.13 168083 221.73 161817 220.59 63073 209.86 43788 208.13 106886 221.73 53065 220.59 113251 209.86 81399 208.13 75631 212.23 77744 211.13 79080 200.87 101148 199.21 300000 212.23 218200 211.13 300000 200.87 223813 199.21 214600 212.23 224986 211.13 300000 200.87 76681 199.21 111409ˬăണዶૻޘ̶ژ
ॲፂASTM D3039-76 ̝ᐖၗٛҩ၁រఢቑĂ၆ώࡁ տٙᄦј۞ᇴᙷݭྏͯซҖᐖၗٛҩ၁រĂณീണዶ
ૻޘĂͽଣޘड़ᑕᄃԮᖼຫ๋үϡޢണዶૻޘ۞ត
̼ĄТॡͽࣧՄྏͯ۞πӮᐖၗٛҩૻޘࠎૄᖂ˭Ăώ
͛ٙనؠ۞ޘड़ᑕᄃԮᖼຫ๋̈́ሤᑅ࣒ྃ͞ڱ၆ണዶૻ
ޘᇆᜩĂ̶ҾซҖଣт˭Ĉ
1. Ԯᖼຫ๋ᄃགྷޘड़ᑕᇆᜩ˭ണዶૻޘ̶ژ ဦ5 ពன̏གྷԆјޘड़ᑕ၁រᄃԮᖼຫ๋̈́ሤᑅ
࣒ྃޢ۞̙ТᙷݭྏͯĂണዶૻޘπӮࣃ۞̂̈ត̼ᄃ ണዶૻޘπӮࣃ၆ࣧՄᐖၗٛҩૻޘπӮࣃ̝ม۞ͧࣃĄ
ֱ၁រᇴፂүࠎ̙ТᙷݭྏͯซҖٛҩ-ٛҩېၗ˭
ি౻၁រᑕ˧ॎ಼ֶ̝̂̈ፂĄϤဦ5 Ξ࠻གྷޘड़ᑕ ޢ̝ണዶૻޘ(case (b))ᄃࣧՄྏͯ۞ᐖၗٛҩૻޘ̝ม۞
ͧࣃ̂ٺ 1Ăពϯགྷޘड़ᑕޢ၆ྏͯᐖၗૻޘ̙ົౄј К̼үϡĄТॡϤဦ4 Ξ࠻གྷޘड़ᑕޢ۞ྏ֭ͯ՟ѣ
௲ᆸຫ๋ĂЯѩޘड़ᑕ̙ົ၆ྏͯౄјᐖၗૻޘ̝ഴ ҲĄϤԮᖼຫ๋ޢണዶૻޘ(case (c))ᄃࣧՄྏͯ۞ᐖၗٛ
ҩૻޘ̝ม۞ͧࣃĂΞ࠻གྷԮᖼຫ๋ޢົጱྏ
ͯૻޘ˭ࢫĄϤဦ3 ̚ពϯགྷԮᖼຫ๋ޢĂྏͯბ̈́ᙝ ቡځពѣ௲ᆸயϠĂͷдྏͯ̚ม˵ѣ௲ᆸ۞ϠјĂܑ
ϯྏͯдԮᖼޢົౄј˘ؠޘ۞ຫֹ๋ૻޘࢫҲĄ၆ ٺАགྷޘड़ᑕޢГགྷԮᖼຫ๋(case (e))ണዶૻޘᄃࣧ
Մྏͯ۞ᐖၗٛҩૻޘ̝ม۞ͧࣃࠎ 0.956Ăពனޘ ड़ᑕᄃԮᖼຫ๋ౄјྏͯѣ௲ᆸன෪۞னĂ҃ጱᐖၗ
ٛҩૻޘࢫҲĄٺАགྷԮᖼຫ๋ޢГགྷޘड़ᑕ(case (g))
۞ྏͯĂϤဦ 5 ̚Ξពனྏͯ۞ᐖၗٛҩૻޘࡗ˭ࢫ 10%νΠĄૻޘ˭ࢫ۞ЯߏֽҋٺԮᖼྶ၆ྏͯԛј
௲ᆸĂֹᐖၗૻޘࢫҲĄͧྵcase (b)ᙷݭྏͯᄃ case (e) ᙷݭྏͯ۞ᐖၗٛҩૻޘĂΞ࠻՟ѣயϠޘड़ᑕᄃԮ
500 550 600 650 700 750 800
Mean ultimatetension strength: σ0 = 736.26 (Mpa)
Mean residual s rength, σ, (Mpa)
Residual Strength σ/σ0
80 90 100 110 120
σ/σ0 (%)
Case (b) Case (c)Case (d) Case (e) Case (f) Case (g) Case (h)
ဦ5 ̙Тᒖဩຫ๋̈́ሤᑅ࣒ྃޢ̝πӮണዶૻޘ
̶Ҷͧྵ
102 103 104 105 106
210 220 230 240 250 260 270 280 290 300
Stress amplitude σa, (MPa)
: σa = 347.51-22.377log(Nf)
σmin / σmax = 0.1 Original
Cycles to failure (Nf)
ဦ6 ࣧՄᇾྏ̝ͯি౻ုѡቢ
ᖼྶΐј۞К̼ड़ڍĂ߇Ԯᖼٙౄј۞௲ᆸ၆ٛҩૻޘ ѣۡତᇆᜩĄϤͧྵcase (c)ᙷݭྏͯᄃ case (g)ᙷݭྏͯ
۞ᐖၗٛҩૻޘĂΞ൴ᛇޢ۰ૻޘ࠹၆ٺ݈۰ࠎ̈ĂЯѩ
ޘड़ᑕ၆ֽҋٺԮᖼٙౄј۞௲ᆸѣᆧ̂ᆧк۞ड़ ᑕĂТॡ၆case (e)ᙷݭྏͯᄃ case (g)ᙷݭྏͯ۞ᐖၗٛ
ҩૻޘซҖͧྵĂϺΞ࠻ԮᖼྶГགྷޘड़ᑕүϡ˭
யϠΐј۞К̼ड़ڍᚑࢦٺགྷޘड़ᑕޢГགྷԮᖼྶү ϡౄј۞К̼ड़ڍĄ
2. ሤᑅ࣒ྃ၆ᐖၗૻޘ̶࣒ྃژ
Ϥဦ5 ̚Ξͽ࠻ࣧՄؕྏͯགྷԮᖼྶٕԮᖼྶ
ລ੨ޘड़ᑕүϡ˭Ăྏͯѣ௲ᆸ۞யϠĂពனԮᖼ
ྶ၆ྏͯౄј˘ؠޘ۞ຫ๋Ą҃ሤᑅ࣒ྃ၆௲ᆸຫ๋
ѣ࣒ྃΑਕĂ၆Մफ़۞፟ୠّኳቁ၁ѣ೩̿۞ड़ڍĂЯѩ ώ͛၆Ԯᖼຫ๋ᄃགྷޘड़ᑕᇆᜩ˭۞ྏͯซҖ࣒ྃĂซ
҃ଣሤᑅ࣒ྃ၆ຫ๋ྏͯണዶૻޘ۞࣒ྃड़ᑕĄϤ၁រ
̚Ξ࠻ԮᖼྶޢГགྷ࣒ྃ۞ྏͯ(case (d))Ăᐖၗπ Ӯٛҩૻޘ֭՟ѣځព۞೩̿ĄЯࠎሤᑅ࣒ྃΪߏొЊ
௲ᆸ̈́ෘᓀᕆЪĂ௲ᆸ̈́ຫ๋֭ڱԆБொੵĂЯѩдૻ
ޘ˯ѣֱధ۞೩̿ҭૻޘڱԆБޭೇߏΞͽഇ۞Ą၆
(a)
(b) 3000
(c) 6000
(d) 9000
(e) 106872 (failure
ဦ7 ᑕ˧ॎ಼ࠎ 231.92Mpa үϡ˭ࣧՄྏͯд̙Т
Ѩ̝ࢰگC-scan ବೡဦ
ٺ࣒ྃགྷޘड़ᑕޢГགྷԮᖼྶ۞ྏͯ(case (f))Ă൴ன གྷሤᑅ࣒ྃޢ۞ૻޘ՟ѣ೩̿Ă҃ͅѣൾ˭ࢫ۞ᔌ๕Ă ТॡགྷԮᖼি ౻ޢГགྷޘ ड़ᑕ۞ྏͯд ࣒ྃޢ(case (g))Ăૻޘ˵ѣൾ˭ࢫ۞ᔌ๕ĄϤѩពனሤᑅ࣒ྃ၆
ޘड़ᑕᄃԮᖼྶౄј۞К̼ΐјड़ڍĂ၆ᐖၗૻޘ̙
ѣ࣒ྃΑਕĄ
αăি౻ု̶ژ
၁រඕڍពனĂࣧՄྏͯགྷ߉ΐԮᖼ֎ॎ಼ቑಛд4°
Ҍ40°Ăүϡ 900 ѨޢĂྏͯ̚யϠ௲ᆸຫ๋ĄЯѩ
ଣĂѩԮᖼ௲ᆸຫ๋၆ٛҩি౻ု۞ᇆᜩĂ֭၆60ƨ 72 ̈ॡ۞ޘड़ᑕтңᇆᜩি౻ုซҖ̶ژĄТॡଣ
ޘड़ᑕລ੨Ԯᖼຫ๋ٙౄј۞ΐјК̼үϡ၆Մफ़ٛҩ
ি౻ု۞ᇆᜩĂ֭ซ˘Վϡ 200ƨ၆̏צຫ๋ྏͯซҖ ሤᑅ࣒ྃĂͽ៍၅ሤᑅ࣒ྃޢ፟ୠّኳаೇّĄ၁រඕڍ ᄃ̶ژт˭Ĉ
1. ࣧՄٛҩি౻ု۞ଣ̶ژ
дѩࡁտ̚ĂВפ̣࣎ᑕ˧ॎ̶಼Ҿ၆ࣧՄྏͯซҖ
ি౻၁រĄᑕ˧ॎ಼ᄃি౻ု̝ม۞ᙯాّтဦ 6 ٙ ϯĄဦ̚ពϯՄफ़ٚצᑕ˧ॎ಼ĂՄफ़۞ি౻ုົ
ҲĄဦ7 ߏдᑕ˧ॎ಼ࠎ 231.92 Mpa үϡଐڶ˭ĂࣧՄ
ྏͯՏགྷ30000 ѨĂซҖࢰگ C-scan ବೡ۞ϯຍဦĂ ဦ̚ពϯ௲ᆸࢬ᎕ੵѨᇴᆧΐ҃ᕖ̂ͷ௲ᆸϤᙝࠧฟؕ
யϠ֭ͷШྏͯ̚มјܜĄГଂဦ7(d)ᄃဦ 7(e)۞ͧྵ̚Ă
300 290 280 270 260 250 240 230 220 210 200 190
102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
Original σa = 347.51-22.377log (Nf) Temperature σa = 3332.15-20.42log (Nf)
ဦ8 ࣧՄᄃགྷޘड़ᑕᇆᜩޢ۞ি౻ုѡቢ̝ͧྵ
300 290 280 270 260 250 240 230 220 210 200 190
102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
Original σa
= 347.51-22.377log (Nf) Torque σa
= 311.14-19.921log (Nf)
ဦ9 ࣧՄᄃ̏Ԯᖼຫ๋۞ি౻ုѡቢ̝ͧྵ
Ξͽ൴னдޢ۞ုѨ̚Ăྏͯ̚۞௲ᆸົԣి۞ؼ ҩ̈́ᆧΐĂጱޢౄјྏͯ۞ᗼĄ
2. Ԯᖼຫ๋ᄃགྷޘड़ᑕᇆᜩ˭̝ি౻ု̶ژ
གྷ 60ƨ72 ̈ॡޘड़ᑕޢ۞ྏͯĂ̶ҾซҖα࣎
ᑕ˧ඈ৺۞ٛҩি౻၁រĂٙזඕڍтဦ8 ٙϯĄϤဦ 8 ̚ពனĂצޘड़ᑕޢ۞ྏͯি౻ုځព˭ࢫĂ ͷΞ࠻צޘड़ᑕޢ۞ি౻ုѡቢͧࣧՄྏͯ۞ি౻
ုѡቢځពгШνઐொĄ҃ౄјি౻ု˭ࢫ۞ࣧЯĂ Ξਕֽҋٺޘड़ᑕ̶ֹ̄ૄՄயϠК̼҃ጱٺញ ჯᄃૄՄ۞ᕆّ˭ࢫĂֹෘᓀᄃ௲ᆸඈՄफ़ౝĂд
ি౻࿅̚јܜՀࠎԣిĂֹি౻ုᒺൺĄဦ9 ពϯ
ྏͯགྷԮᖼຫ๋ޢГซҖα࣎ᑕ˧ඈ৺۞ি౻၁រඕڍĄ дѩဦ̚ϤͧྵࣧՄྏͯ۞ုѡቢᄃԮᖼຫ๋ޢ۞ྏͯ
۞ုѡቢĂΞځព࠻ĂྏͯགྷԮᖼྶޢயϠ௲ᆸຫ
๋ౄјЧᑕ˧ඈ৺˭ি౻ု۞˭ࢫĂֹགྷԮᖼຫ๋ޢ
۞ি౻ုѡቢӔன˘Шνઐொ۞ᔌ๕ĄАགྷޘड़ᑕГ གྷԮᖼຫ๋ޢ۞ি౻ုѡቢᄃАԮᖼຫ๋ޢГགྷޘड़
280 270 260 250 240 230 220 210 200
190102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
Temperature + Torque σa
= 316.47-19.59log (Nf) Torque + Temperature σa
= 301.05-18.99log (Nf)
ဦ10 གྷޘᇆᜩޢГགྷԮᖼຫ๋ᄃАགྷԮᖼຫ๋Гགྷ
ޘᇆᜩ̝ি౻ုѡቢͧྵ
300 290 280 270 260 250 240 230 220 210 200 190
102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
σa = 332.42-20.42log (Nf) σa = 316.47-15.59log (Nf)
Temperature Temperature + Torque
ဦ11 གྷޘᇆᜩޢГགྷԮᖼຫ๋ᄃ่གྷޘᇆᜩ̝ি
౻ုѡቢͧྵ
ᑕ۞ি౻ုѡቢ̝ม۞ͧྵтဦ10 ٙϯĄϤဦ̚ពϯА
ٚצԮᖼຫ๋Гགྷޘड़ᑕޢٙౄјК̼ड़ڍົͧٚצ
ޘड़ᑕޢГԮᖼຫ๋யϠΐј۞К̼ड़ڍᚑࢦĄЯѩΞ
ۢĂᒖဩ୧ІЯ߉ΐ۞ึԔົ၆Մफ़۞ি౻ုౄј̙
˘۞ᇆᜩĄဦ 6 ពன۞ࣧՄྏͯ۞ုѡቢᄃဦ 10
ٙ̚ϯ̝ޘड़ᑕᄃԮᖼຫ๋ΐјүϡ˭۞ုѡቢซҖ
ͧྵĄΞ൴னזĂٚצޘड़ᑕ̈́Ԯᖼຫ๋ΐјүϡ˭۞
ি౻ုѡቢӮӔனШνઐொ۞ᔌ๕ĄϤѩΞۢĂдޘ ड़ᑕᄃԮᖼຫ๋ΐј۞үϡ˭၆ྏͯౄј௲ᆸຫ๋Ă
ֹྏͯ۞ি౻ٚྶ˧˭ࢫĄдဦ11 ̚၆གྷޘड़ᑕᇆᜩ۞
ি౻ုѡቢᄃАགྷޘड़ᑕᇆᜩޢГٚצԮᖼྶ۞ি
౻ုѡቢซҖͧྵĄϤဦ̚Ξ൴னĂΪಏ৷צޘड़ᑕ ᇆᜩ˭۞ি౻ٚྶ˧ͧٚצޘ̈́Ԯᖼຫ๋ᗕࢦड़ᑕүϡ
˭۞ি౻ٚྶ˧ૻĄ҃ဦ12 ࠎགྷޘड़ᑕᇆᜩ۞ি౻ု
ѡቢᄃԮᖼຫ๋ޢГགྷޘड़ᑕᇆᜩ۞ি౻ုѡቢ۞
ͧྵဦĄϤဦ11 ᄃဦ 12 ۞ͧྵΞ൴னԮᖼޢГ߉ΐޘ
300 290 280 270 260 250 240 230 220 210 200 190
102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
σa = 332.42-20.42log (Nf) σa = 301.05-18.99log (Nf)
Temperature Torque + Temperature
ဦ12 АགྷԮᖼຫ๋Гགྷޘᇆᜩᄃ่གྷޘᇆᜩ̝ি
౻ုѡቢͧྵ
300 290 280 270 260 250 240 230 220 210 200 190
102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
σa = 311.4-19.92log (Nf) σa = 316.47-19.59log (Nf)
Torque
Temperature + Torque
ဦ13 གྷޘᇆᜩޢГགྷԮᖼຫ๋ᄃ่གྷԮᖼຫ๋ᇆᜩ
̝ি౻ုѡቢͧྵ
ड़ᑕயϠ۞௲ᆸೋ̼ଐڶྵࠎᚑࢦĄ่གྷԮᖼຫ๋۞ি
౻ုѡቢᄃАٚצޘᇆᜩޢГགྷԮᖼຫ๋۞ি౻ု
ѡቢซҖͧྵĂ୧ি౻ုѡቢͧྵඕڍтဦ 13 ٙ ϯĄϤဦ̚Ξ࠻୧ি౻ုѡቢ࠹༊ତܕĄពϯ
АԮᖼຫ๋ޢГٚצޘड़ᑕயϠΐј۞К̼ड़ڍ̙ព
Ă၆ٺি౻ုᇆᜩѣࢨĄΩγĂͧྵΪٚצԮᖼຫ๋
АٚצགྷԮᖼຫ๋ޢГޘड़ᑕ୧ি౻ုѡቢĂ тဦ14 ٙϯĄ୧ি౻ုѡቢ˵࠹༊ତܕĂҭޘड़ ᑕޢГ߉ΐԮᖼྶٙౄј۞К̼үϡᔘߏྵࠎᚑࢦĄϤ ဦ13 ᄃဦ 14 ۞ͧྵĂΞ֍ޘड़ᑕ߉ΐ۞ึԔ၆ٺি౻
ု֭՟ѣព۞ᇆᜩĄ
3. ሤᑅ࣒ྃ၆ি౻ု̶࣒ྃژ
၆Ԯᖼຫ๋۞ྏͯซҖሤᑅ࣒ྃĂ֭ͷ࣒ྃޢ۞
ྏͯซҖคШٛҩি౻၁រĂඕڍтဦ 15 ٙϯĄдဦ 15 ̚ТॡពϯԮᖼຫ๋۞ྏͯдሤᑅ࣒݈ྃޢ۞ি౻
300 290 280 270 260 250 240 230 220 210 200 190
102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
σa = 311.4-19.92log (Nf) σa = 301.05-18.99log (Nf)
Torque
Torque + Temperature
ဦ14 АགྷԮᖼຫ๋Гགྷޘᇆᜩᄃ่གྷԮᖼຫ๋ᇆᜩ
̝ি౻ုѡቢͧྵ
300 290 280 270 260 250 240 230 220 210 200 190
102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
σa = 347.51-22.377log (Nf) σa = 311.14-19.92log (Nf) σa = 330.04-23.43log (Nf)
Original Torque Torque + Repair
ဦ15 Ԯᖼຫ๋дሤᑅ࣒݈ྃޢᄃࣧՄ̝ি౻ုѡ ቢͧྵ
ုѡቢ̈́ࣧՄি౻ုѡቢĄϤဦ̚ি౻ုѡቢ̝ม
۞ͧྵĂΞ൴னז࣒ྃޢি౻ုѡቢ࠹၆ٺ࣒݈ྃ
۞ি౻ုѡቢځពгШΠઐொĂពனԮᖼຫ๋۞
ྏͯགྷሤᑅ࣒ྃޢি౻ုྵሤᑅ࣒݈ྃѣځពԼචĄ ТॡΞ൴னሤᑅ࣒ྃੵ˞дҲᑕ˧ॎ಼үϡ˭ྵ՟ѣពன
࣒ྃड़ڍγĂдι۞ᑕ˧ॎ಼үϡ˭Ă൴னি౻ု࠰
ѣ˘ؠޘ۞೩̿ĄГ۰Ϥ࣒ྃޢ۞ি౻ုѡቢᄃࣧՄ
ྏͯ۞ি౻ုѡቢ̝ม۞ͧྵĂԧࣇΞͽځព࠻Ăྏ
࣒ͯྃड़ڍ֭ڱ྿זࣧՄېၗĂࣧЯࠎྏͯЯሤᑅ࣒
ྃ҃ࢦາᕆЪĂҭѣొЊ௲ᆸ̈́ෘᓀ֭ڱԆБொੵĄ҃
ֱ՟ѣజሤᑅ࣒ྃᕆЪ۞௲ᆸ̈́ෘᓀĂົдি౻࿅̚
јܜ̈́ቭЪĂֹ࣒ྃޢি౻ုٚྶ˧ڱ྿זࣧՄې
ၗĄЯѩĂሤᑅ࣒ྃΞྏͯѣ۞௲ᆸࢬ᎕ഴ͌ҭڱ ԆБΝੵĄ၆ٺАགྷޘड़ᑕޢГགྷԮᖼຫ๋ሤᑅ࣒݈ྃ
ޢ̝ি౻ုѡቢͧྵтဦ16 ٙϯĄϤဦ̚Ξ࠻࣒ྃޢ
۞ি౻ုѡቢ࠹၆ٺ࣒݈ྃি౻ုѡቢѣځពгШΠ
280 270 260 250 240 230 220 210 200 190
102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
σa = 316.47-219.59log (Nf) σa = 329.05-21.39log (Nf)
Temperature + Torque Temperature + Torque + Repair
ဦ16 གྷޘᇆᜩޢГགྷԮᖼຫ๋дሤᑅ࣒݈ྃޢ̝ি
౻ုѡቢͧྵ
280 270 260 250 240 230 220 210 200
190102 103 104 105 106
Cycles to failure (Nf) Stress amplitude, σa, (MPa)
σmin/σmax= 0.1
σa = 301.05-18.99log (Nf) σa = 317.50-21.58log (Nf)
Torque + Temperature Temperature + Torque + Repair
ဦ17 གྷԮᖼຫ๋ޢГགྷޘᇆᜩޢдሤᑅ࣒݈ྃޢ̝
ি౻ုѡቢͧྵ
ઐொېၗĄܑϯགྷሤᑅ࣒ྃޢĂྏͯ۞ি౻ုѣځព ԼචĄซ˘ՎϤ၁រᇴፂពனĂдᑕ˧ॎ಼үϡ˭Ă࣒
ྃޢি౻ုځព۞ӔࢺᇴᆧΐĄдҲᑕ˧ॎ಼үϡ˭Ă
࣒ྃޢি౻ု۞೩̿ᔵΪѣೀ˩࣎Ѻ̶ͧĂҭ၁ᅫ˯
ုณ۞೩̿ᄃϏ࣒݈ྃ࠹ͧĂᆧΐ۞ি౻ု࠹༊
кĄᔵдѩሤᑅ࣒ྃ۞୧І˭௲ᆸຫ๋ڱԆБజொ
ੵĂҭ௲ᆸຫ๋ࢬ᎕ѣځព۞ഴ͌ĄЯѩĂ၆ѩຫ๋ଐڶ
ٙซҖ۞ሤᑅ࣒ྃĂड़ڍߏ࠹༊̙۞Ąဦ17 ࠎАགྷԮ ᖼຫ๋ޢГགྷޘड़ᑕ۞ྏͯд࣒݈ྃޢি౻ုѡቢ۞
ͧྵĄϤဦ17 ̚Ξ៍၅Ă࣒ྃޢ۞ি౻ုѡቢ࠹၆ٺ
࣒݈ྃ۞ি౻ုѡቢځពгШΠઐொĂͷд̙Т۞ᑕ˧
ॎ಼үϡ˭ĂՄफ़۞ি౻ု࠰ѣ࠹༊ޘ۞೩̿Ăពϯ дѩຫ๋ଐڶ˭Ăሤᑅ࣒ྃ၆ি౻ုົѣځពԼචĄТ ॡĂΞ៍၅זሤᑅ࣒ྃ၆АགྷԮᖼຫ๋Гགྷޘड़ᑕᇆᜩ
۞ྏͯĂдЧ࣎ᑕ˧ॎ಼үϡ˭Ăি౻ု۞೩̿Ӯᐹ ٺАགྷޘड़ᑕޢГགྷԮᖼຫ๋۞ྏͯĄ
̣ăඕ ኢ
дώ͛̚ଣĂԮᖼྶ̈́ޘड़ᑕᒖဩྶ
၆ሤّኑЪՄफ़Gr/Peek дᐖၗૻޘͽ̈́คШি౻ု
۞ᇆᜩĄТॡдᒖဩྶޢ၆ྏͯซҖሤᑅ࣒ྃĂ֭ͷ̶
ژд࣒݈ྃޢᐖၗૻޘᄃি౻ု۞ត̼Ąགྷ၁រពϯ
۞ඕڍΞᕩৼт˭Ĉ
1. 60ƨ 72 ̈ॡޘड़ᑕົౄј̶̄ૄՄ۞К̼Ăጱ
ি౻ု۞ٚྶ˧ѣځព˭ࢫĂҭ၆ᐖၗૻޘ̙ົౄј К̼үϡĄ
2. ߉ΐԮ֎ቑಛд 4°Ҍ 40°̝มͷүϡѨᇴࠎ 900 ѨĂ Մफ़дണዶૻޘ˯யϠֱ۞К̼ͷি౻ုѣځព
۞˭ࢫĄҭགྷሤᑅ࣒ྃޢĂЯԮᖼྶ҃யϠ۞௲ᆸࢬ
᎕ѣځពត͌ĂֹԮᖼຫ๋Մफ़۞ি౻ုѣځព
۞೩̿Ą
3. གྷԮᖼྶГགྷޘड़ᑕᇆᜩޢ۞Մफ़Ăдᐖၗૻޘࡗ ѣ10 % ۞К̼үϡĂͷি౻ုѣځព۞˭ࢫĄѩᙷ ݭՄफ़གྷሤᑅ࣒ྃޢি౻ု˯ѣځព۞ԼචĄ 4. གྷޘड़ᑕᇆᜩГགྷԮᖼྶޢ۞Մफ़Ăдᐖၗૻޘ˯
֭ځព۞К̼Ăҭдি౻ု˯ѣځព۞˭ࢫĄѩ ᙷݭՄफ़ࣧѣ௲ᆸࢬ᎕གྷሤᑅ࣒ྃޢѣځពត͌Ăͷ
ি౻ုѣځព۞೩̿Ą
5. Ԯᖼ̈́ޘᒖဩྶົЯ߉ΐึԔ̙ТĂ၆Մफ़ дᐖၗૻޘ̈́ি౻ုౄјК̼ᇆᜩ˵ົ̙ТĄ
ણ҂͛ᚥ
1. Ferry, J., Perreux, D., Varchon, D., and Sicot, N., “Fatigue Behaviour of Composite Bars Subjected to Bending and Torsion,” Composite Science and Technology, Vol. 59, pp.
575-582 (1999).
2. Yip, M. C., and Chi, H. M., “Axial Fatigue Behaviour of the [0/+45/45/90]2s Carbon/Epoxy Composite under Pre-torsional Fatigue loading,” Proceeding of Internation Conference on Advanced Materials, Beijing, China, pp.
863-868 (1996).
3. Yip, M. C., and Lai, K. C., “Unaxial Low Cycle Fatigue Behaviour of the CFRP Composite Laminate Under Pre-torsional Fatigue loading and Thermal Effects,”
Proceeding of the 1st Asian-Australasian Conference on Composite Materials, Osaka, Japan, pp. 719~1-719~4 (1998).
4. Ferreeira, J. A. M., Costa, J. D. M., Reis, P. N. B., and Richardson, M. O. W., “Analysis of Fatigue and Damage in Glass-Fiber-Reinforced Polypropylene Composite Materials,” Composite Science and Technology, Vol. 59, pp. 1461-1467 (1999).
5. Lustiger, L., and Newaz, G. M., “Interlamellar Fracture
and Craze Growth in PEEK Composites Under Cycle Loading,” Journal of Composite Materials, Vol. 24, pp.
175-187 (1990).
6. Silverman, E. M., and Jones, R. J., “Property and Processing Performance of Graphite/PEEK Prepreg Tapes and Fabrics,” SAMPE Journal, pp. 33-40 (1988).
7. Jones, R., and Lukez, R., “Extended Thermal Cycle Testing of Graphite/Epoxy Composite Struts for Space Station Applications,” SAMPL Quarterly, pp. 34-38 (1989).
8. Herakovich, C. T., and Hyer, M. W., “Damage-Induced Property Change in Composites Subjected to Cyclic Thermal Loading,” Engineering Fracture Mechanics, Vol.
25, Nos. 5/6, pp. 779-791 (1986).
9. Satoshi, K., “Damage-Mechanics Analysis of Matrix Cracking in Cross-Ply CFRP Laminate Under Thermal Fatigue,” Composites Science and Technology, Vol. 61, pp. 1735-1742 (2001).
10. Cantwell, W. J., Davis, P., and Kausch, H. H., “Repair of
Impact-Damage Carbon PEEK Composite,” SAMPE Journal, Vol. 27, pp. 30-35 (1991).
11. Yao, W. X., and Himmel, N., “A New Cumulative Fatigue Damage Model for Fibre-Reinforced Plastics,”
Composites Science and Technology, Vol. 60, pp. 59-61 (2000).
12. Wilson, T. A., and Graves, M. J., “Repair of Graphite/
PEEK APC-2 Using Thermoforming,” SAMPE Journal, Vol. 23, pp. 51-56 (1991).
13. ཧᅛߵăోछĂĶሤᑅ࣒ྃ၆Gr/PEEK ኑЪՄफ़གྷค Шি౻̈́Ԯᖼি౻̝คШি౻ု̝ࡁտķĂ઼፟̚ୠ
̍ ጯ ົ ௐ ˩ ̱ ب Б ઼ ጯ ఙ ࡁ ົ ኢ ͛ ะ Ă ௐ H133-H140 ࢱ(1999).
2004 ѐ 08 ͡ 17 ͟! ќቇ 2004 ѐ 09 ͡ 01 ͟! ܐᆶ 2004 ѐ 09 ͡ 21 ͟! ኑᆶ 2004 ѐ 10 ͡ 04 ͟! ତצ