摘要
为了测量铺放过程中粘合点温度峰值和复合材料的温度场分布,构建了基于LabVIEW的温度场在线测量系统。实验中预浸带铺放5层,热风枪稳定温度为200℃。实验结果表明,随着铺放过程的进行,每一层预浸带的温度曲线都出现多个峰值,且峰值逐渐降低,其中第1个峰值即为粘合点温度,平均分别为80.1、91.4、101.3、113、108.3℃。由比较可知,各层预浸带粘合点温度逐渐升高。同时,建立了预浸带铺放温度场有限元模型,利用ANSYS中的生死单元以及循环加载技术,模拟了预浸带动态铺放过程。有限元模拟结果中的粘合点温度分别为71.8、96.2、104.3、107.9、105.3℃,与实验结果相比,误差可控制在10%以内,且粘合点温度越高,其准确性越好。
A temperature online measurement system based on LabVIEW was established, aiming at measuring the temperature peak at the nip-point and the temperature distribution in the prepreg placement process. In the experiment, 5 layers of prepreg were laid-up and the stable temperature of hot air was 200 ℃. The experimental results show that along with the placement process, the temperature curves of every layer have several peaks decreasing gradually and the first peak was the nip-point temperature. The nip- point temperatures of each layer increased gradually, they were 80.1 ℃, 91.4 ℃, 101.3 ℃, 113 ℃ and 108.3 ℃ respectively. In addition, a finite element model of temperature field was established and a dynamic finite element simulation for prepreg placement process was done by using the birth-death element strategy and the cyclic loading strategy in ANSYS. The nip-point temperatures in the finite element simulation results were 71.8 ℃, 96.2 ℃, 104.3 ℃, 107.9 ℃ and 105.3 ℃ respectively. The error of the nip- point temperature between finite element simulation results and experimental results can be controlled within 10%, and the higher the nip-point temperature get, the more accurate the result became.
出处
《固体火箭技术》
EI
CAS
CSCD
北大核心
2016年第1期116-119,145,共5页
Journal of Solid Rocket Technology
基金
国家自然科学基金(11372220)
天津市应用基础与前沿技术研究计划重点项目(11JCZDJC23000)
关键词
预浸带铺放
温度场分布
动态仿真
实验
prepreg placement
temperature distribution
dynamic finite element simulation
experiment