航空材料学报
航空材料學報
항공재료학보
JOURNAL OF AERONAUTICAL MATERIALS
2015年
3期
69-76
,共8页
肖飞%姜茂川%刘强%陈志平%张博明
肖飛%薑茂川%劉彊%陳誌平%張博明
초비%강무천%류강%진지평%장박명
VARI%副翼结构件%渗透率%注模模拟
VARI%副翼結構件%滲透率%註模模擬
VARI%부익결구건%삼투솔%주모모의
VARI%flap%permeability%infusion simulation
在复合材料液体成型工艺过程中,通过计算机软件的模拟研究,可以预先判断树脂在增强体中的流动形式和获得树脂的注模时间以及注模压力,进而为实际成型工艺提供参考设计。本文利用 PAM-RTM 模拟软件对复合材料副翼典型结构件的树脂流动过程进行了模拟计算。根据达西定律推导出树脂在增强纤维中一维流动渗透率计算公式,分别对增强纤维、缝线纤维进行了渗透率测试,在此基础上对渗透率数值进行了修正。利用渗透率修正值采用不同的流道设计方案对树脂注模过程进行了模拟研究,根据模拟结果最终选择合理的注射方式和流道布局。对所选方案进行了工艺试验验证,并对结构件进行了超声无损检测。结果显示:理论充模时间和试验充模时间基本一致,结构件没有内部缺陷,树脂填充完全,模拟工艺计算有效。
在複閤材料液體成型工藝過程中,通過計算機軟件的模擬研究,可以預先判斷樹脂在增彊體中的流動形式和穫得樹脂的註模時間以及註模壓力,進而為實際成型工藝提供參攷設計。本文利用 PAM-RTM 模擬軟件對複閤材料副翼典型結構件的樹脂流動過程進行瞭模擬計算。根據達西定律推導齣樹脂在增彊纖維中一維流動滲透率計算公式,分彆對增彊纖維、縫線纖維進行瞭滲透率測試,在此基礎上對滲透率數值進行瞭脩正。利用滲透率脩正值採用不同的流道設計方案對樹脂註模過程進行瞭模擬研究,根據模擬結果最終選擇閤理的註射方式和流道佈跼。對所選方案進行瞭工藝試驗驗證,併對結構件進行瞭超聲無損檢測。結果顯示:理論充模時間和試驗充模時間基本一緻,結構件沒有內部缺陷,樹脂填充完全,模擬工藝計算有效。
재복합재료액체성형공예과정중,통과계산궤연건적모의연구,가이예선판단수지재증강체중적류동형식화획득수지적주모시간이급주모압력,진이위실제성형공예제공삼고설계。본문이용 PAM-RTM 모의연건대복합재료부익전형결구건적수지류동과정진행료모의계산。근거체서정률추도출수지재증강섬유중일유류동삼투솔계산공식,분별대증강섬유、봉선섬유진행료삼투솔측시,재차기출상대삼투솔수치진행료수정。이용삼투솔수정치채용불동적류도설계방안대수지주모과정진행료모의연구,근거모의결과최종선택합리적주사방식화류도포국。대소선방안진행료공예시험험증,병대결구건진행료초성무손검측。결과현시:이론충모시간화시험충모시간기본일치,결구건몰유내부결함,수지전충완전,모의공예계산유효。
In the process of composites fluid molding,the filling time and pressure of resin can be forecasted with using computer-aided simulation software,which can provide reference design for the real molding process of resin flow.The simulation of the resin flow had been carried out for flap structural composite by using PAM-RTM software.According to the Darcy’s law,the formula of permeability was deduced when the resin flow along reinforce fiber.The permeability of carbon fiber and suture fiber was tested and revised respec-tively.The simulation of the resin flow was carried out by using several runner means.The final reasonable injection port and runner were chosen according to simulation results.The chosen means were verified by the process experims,also the structural component was tested by using ultrasonic nondestructive testing.The results show that the theoretical filling time is almost consistent with the fill-ing time measured by the experiments.It is not found that the internal defect is existed in structural components.The resin filling is e-nough,to prove that the simulation is valid.