浙江理工大学学报
浙江理工大學學報
절강리공대학학보
JOURNAL OF ZHEJIANG SCI-TECH UNIVERSITY
2014年
2期
165-170
,共6页
聚合物基复合材料%片状填料%导热系数%有限元模拟%比等效热阻法
聚閤物基複閤材料%片狀填料%導熱繫數%有限元模擬%比等效熱阻法
취합물기복합재료%편상전료%도열계수%유한원모의%비등효열조법
polymer composite%flake filler%thermal conductivity%finite element simulation%equiva-lent thermal resistance
基于比等效热阻法建立了简化了的片状填料填充聚合物基复合材料的导热模型并推导出了相应的等效导热系数公式。以云母片填充聚乳酸为例,应用有限元软件ANSYS建立了云母体积分数在11%下的聚乳酸/云母复合材料的三维稳态热传导单元模型,并模拟了热流沿云母片厚度方向和径向传递的过程。结果表明,当热流沿云母片轴向方向上流动时,经ANSYS模拟求得的复合材料的等效导热系数和文中推导的公式的所给出的预测值更为接近;当热流沿云母片的径向流动时,随着云母体积分数的增加,复合材料的等效导热系数的预测值呈指数性增长,并且高于ANSYS的计算结果。有限元结果和本文的公式均表明,片状填料填充聚合物复合材料的等效导热系数可分解为是沿热流不同正方向上的贡献,更长的等效导热路径使片状颗粒在填充聚合物后能提供更为出色的导热性能。
基于比等效熱阻法建立瞭簡化瞭的片狀填料填充聚閤物基複閤材料的導熱模型併推導齣瞭相應的等效導熱繫數公式。以雲母片填充聚乳痠為例,應用有限元軟件ANSYS建立瞭雲母體積分數在11%下的聚乳痠/雲母複閤材料的三維穩態熱傳導單元模型,併模擬瞭熱流沿雲母片厚度方嚮和徑嚮傳遞的過程。結果錶明,噹熱流沿雲母片軸嚮方嚮上流動時,經ANSYS模擬求得的複閤材料的等效導熱繫數和文中推導的公式的所給齣的預測值更為接近;噹熱流沿雲母片的徑嚮流動時,隨著雲母體積分數的增加,複閤材料的等效導熱繫數的預測值呈指數性增長,併且高于ANSYS的計算結果。有限元結果和本文的公式均錶明,片狀填料填充聚閤物複閤材料的等效導熱繫數可分解為是沿熱流不同正方嚮上的貢獻,更長的等效導熱路徑使片狀顆粒在填充聚閤物後能提供更為齣色的導熱性能。
기우비등효열조법건립료간화료적편상전료전충취합물기복합재료적도열모형병추도출료상응적등효도열계수공식。이운모편전충취유산위례,응용유한원연건ANSYS건립료운모체적분수재11%하적취유산/운모복합재료적삼유은태열전도단원모형,병모의료열류연운모편후도방향화경향전체적과정。결과표명,당열류연운모편축향방향상류동시,경ANSYS모의구득적복합재료적등효도열계수화문중추도적공식적소급출적예측치경위접근;당열류연운모편적경향류동시,수착운모체적분수적증가,복합재료적등효도열계수적예측치정지수성증장,병차고우ANSYS적계산결과。유한원결과화본문적공식균표명,편상전료전충취합물복합재료적등효도열계수가분해위시연열류불동정방향상적공헌,경장적등효도열로경사편상과립재전충취합물후능제공경위출색적도열성능。
In this paper ,a simplified thermal equivalent model of the flake filler reinforced composite was established based on equivalent thermal resistance and corresponding equivalent thermal conductivity coefficient formula is derived .Take the mica plate used to fill polylactic acid for example .A three-dimen-sion steady-state thermal conduction unit model for polylactic acid/mica composite is made through ANSYS software with mica volume fraction of 11% .The process of thermal flux transferring to thickness direction and radial direction of the mica plate is simulated .The results show that when thermal flux flowed along the axial direction of the mica plate ,equivalent thermal conductivity coefficient of the composite gained through ANSYS simulation more approached the predicted value gained through the formula ;when ther-mal flux flowed along the radial direction of the mica plate ,as mica volume fraction rose ,the predicted val-ue of equivalent thermal conductivity coefficient of the composite presented exponential grow th and is high-er than the result of ANSYS .The finite element result and the formula in this paper showed equivalent thermal conductivity coefficient of flake filler polymer composite could be decomposed to contributions at different directions along the thermal flux ;longer equivalent thermal conductivity path made flake particles provide more outstanding thermal conduction property after filling the polymer .