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用于复合材料制造的自热模具

Self-Heating Mould for Composite Manufacturing.

作者信息

Kondratiev Andrii, Píštěk Václav, Purhina Svitlana, Shevtsova Maryna, Fomina Anna, Kučera Pavel

机构信息

Department of Building Technology and Construction Materials, O.M. Beketov National University of Urban Economy in Kharkiv, Marshal Bazhanov Str. 17, 61002 Kharkiv, Ukraine.

Institute of Automotive Engineering, Brno University of Technology, Technická 2896/2, 616 69 Brno, Czech Republic.

出版信息

Polymers (Basel). 2021 Sep 12;13(18):3074. doi: 10.3390/polym13183074.

DOI:10.3390/polym13183074
PMID:34577975
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC8467842/
Abstract

The shipbuilding industry, engine manufacturing, aviation, rocket and space technology are promising fields of application for polymeric composite materials. Shape-generating moulding tools with internal heating are used for the creation of a more economically viable method of moulding of internally heated composite structures. The use of a fine-fibered resistive structure in the heated tools allows implementation of effective heating of the composite and elimination of the need for expensive and energy-intensive heating equipment. The aim of this paper was the reduction of energy consumption for internally heated moulding tools by choosing the optimal parameters for their resistive layer. A method for determination of the parameters of the moulding tool resistive layer was developed. This method allows calculation of the heating layer parameters and implementation of the specified time-temperature regime for moulding of the composite structure. It was shown that energy saving for the heated fiberglass shape-generating moulding tools was from 40 to 60%. It was found that the increase in the thickness of the moulded package of the polymeric composite material resulted not only in a higher supplied power for the heating system, but also in a complication of the method for system control, because of the growing exothermic effect of the binder curing reaction. For composite products based on Hysol EA 9396 binder, thicknesses more than 4 mm are critical, because it is not possible to cope with the self-heating effect only by cooling with ambient air already utilized at the twentieth minute of the moulding process. The influence of the physical and mechanical characteristics of the moulding tool material and stiffening ribs was analysed in terms of energy consumption and controllability of the heating system. Fiberglass shows the lowest energy consumption. Heating of the aluminium and steel moulding tools for the same purpose will require 20% and 45% more power, respectively. An increase in the number of stiffening ribs has a strong effect on the heat removal of the heating system. With a small number of aluminium ribs it is not possible to maintain the specified temperature-time regime for a fiberglass moulded package of 5 mm thick with the use of the equipment. However, when the number of stiffeners is increased to 10, the exothermic effect of the reaction becomes smoother and then the heating equipment can cope with the task. An experimental prototype of heating equipment of moulding tools for the manufacturing of structures of polymeric composite materials, as well as a flexible thermal blanket for repair of non-separable structures, were developed. The results can be the basis for a new method of optimal design of parameters of moulding tool structure at minimal heat removal to the environment.

摘要

造船业、发动机制造、航空、火箭和太空技术是聚合物复合材料很有前景的应用领域。带有内部加热装置的成型模具被用于创造一种更经济可行的内部加热复合结构成型方法。在加热工具中使用细纤维电阻结构能够有效加热复合材料,并消除对昂贵且耗能的加热设备的需求。本文的目的是通过为其电阻层选择最佳参数来降低内部加热成型工具的能耗。开发了一种确定成型工具电阻层参数的方法。该方法能够计算加热层参数,并实现用于复合结构成型的特定时间 - 温度制度。结果表明,加热的玻璃纤维成型模具节能40%至60%。发现聚合物复合材料模压包厚度的增加不仅导致加热系统的供电功率更高,还由于粘合剂固化反应放热效应的增加而使系统控制方法变得复杂。对于基于Hysol EA 9396粘合剂的复合产品,厚度超过4毫米是关键的,因为在成型过程的第二十分钟已经利用环境空气冷却的情况下,仅靠环境空气冷却已无法应对自热效应。从加热系统的能耗和可控性方面分析了成型工具材料和加强肋的物理和机械特性的影响。玻璃纤维显示出最低的能耗。出于相同目的加热铝制和钢制成型工具分别需要多20%和45%的功率。加强肋数量的增加对加热系统的散热有很大影响。使用该设备时,对于5毫米厚的玻璃纤维模压包,若铝制肋条数量较少,则无法维持规定的温度 - 时间制度。然而,当肋条数量增加到10时,反应的放热效应变得更平稳,然后加热设备就能完成任务。开发了用于制造聚合物复合材料结构的成型工具加热设备的实验原型以及用于修复不可分离结构的柔性热毯。这些结果可为在向环境散热最小的情况下对成型工具结构参数进行优化设计的新方法奠定基础。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/bfc373f8f85e/polymers-13-03074-g014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/8258485b255f/polymers-13-03074-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/2f1ad3266b4f/polymers-13-03074-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/073ddf916bb8/polymers-13-03074-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/666d53b183c1/polymers-13-03074-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/6d0ec3cb41d6/polymers-13-03074-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/1d6df12928b8/polymers-13-03074-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/c40119e21839/polymers-13-03074-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/5794084c1502/polymers-13-03074-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/6b597f049630/polymers-13-03074-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/50f13eab159c/polymers-13-03074-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/863247cf0b66/polymers-13-03074-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/56657515c10d/polymers-13-03074-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/f53f3216fca5/polymers-13-03074-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/bfc373f8f85e/polymers-13-03074-g014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/8258485b255f/polymers-13-03074-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/2f1ad3266b4f/polymers-13-03074-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/073ddf916bb8/polymers-13-03074-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/666d53b183c1/polymers-13-03074-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/6d0ec3cb41d6/polymers-13-03074-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/1d6df12928b8/polymers-13-03074-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/c40119e21839/polymers-13-03074-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/5794084c1502/polymers-13-03074-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/6b597f049630/polymers-13-03074-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/50f13eab159c/polymers-13-03074-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/863247cf0b66/polymers-13-03074-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/56657515c10d/polymers-13-03074-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/f53f3216fca5/polymers-13-03074-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/327c/8467842/bfc373f8f85e/polymers-13-03074-g014.jpg

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本文引用的文献

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A Review on the Mechanical Modeling of Composite Manufacturing Processes.复合材料制造工艺的力学建模综述
Arch Comput Methods Eng. 2017;24(2):365-395. doi: 10.1007/s11831-016-9167-2. Epub 2016 Jan 20.
Polymers (Basel). 2022 Mar 5;14(5):1041. doi: 10.3390/polym14051041.
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Effects of the Temperature-Time Regime of Curing of Composite Patch on Repair Process Efficiency.复合材料补片固化温度-时间制度对修复过程效率的影响。
Polymers (Basel). 2021 Dec 11;13(24):4342. doi: 10.3390/polym13244342.
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Stress-Strain Behaviour of Reparable Composite Panel with Step-Variable Thickness.具有阶梯变厚度的可修复复合板的应力-应变行为
Polymers (Basel). 2021 Nov 5;13(21):3830. doi: 10.3390/polym13213830.