• Resin transfer molding(RTM) is one of the important processes for fabrication of fiber-reinforced polymer-matrix composites.

    树脂传递模塑工艺(RTM)是纤维增强聚合物基复合材料的重要制备工艺之一。

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  • The numerical simulation of curing processes in resin transfer molding is helpful to control the chemical reaction, material structures and properties.

    树脂传递模塑工艺的固化过程数值模拟有助于化学反应、材料结构与性能的控制,具有重要的科学意义和工程价值。

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  • This paper introduces the processes and characterizations of the resin transfer molding briefly.

    介绍了树脂传递模塑工艺过程及特点。

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  • Resin transfer molding is considered a promising manufacturing process for high performance composite materials.

    树脂传递模塑被认为是一种有前途的大量生产高性能复合材料的工艺。

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  • The invention relates to a device and a method which prepare composite materials by a resin transfer molding process.

    本发明涉及一种树脂传递模塑工艺制备复合材料的设备和方法。

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  • Resin transfer molding (RTM) is considered a promising manufacturing process for high performance composite materials.

    树脂传递模塑被认为是一种有前途的大量生产高性能复合材料的工艺。

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  • A three-dimensional mathematical model of the resin transfer molding(RTM) filling process for the automobile bumper was presented.

    首先建立了汽车保险杠树脂传递模塑充模过程的三维数学模型;

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  • The method of the invention is that the resin in a resin storage pot is executed with ultrasonic-processing continuously in the technical process of resin transfer molding.

    本发明的方法是在树脂传递模塑工艺过程中持续对储胶罐中的树脂进行超声处理。

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  • Transfer molding techniques provide for excellent consistency, density, and low permeability.

    转移成型工艺提供了良好的一致性,密度和低渗透。

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  • This paper addresses the resin Transfer Molding (RTM) process. The governing equations of resin flow are presented.

    介绍了RTM工艺过程及特点,给出了树脂渗流控制方程。

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  • The composite skirts for solid rocket motor shells fabricated by VARTM (VacuumAssisted Resin Transfer Molding) had poor mechanical properties because the fiber volume fraction was very small.

    VARTM工艺成型的固体火箭发动机壳体复合材料连接裙段构件纤维体积含量较低,复合材料力学性能不佳。

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  • The composite skirts for solid rocket motor shells fabricated by VARTM (VacuumAssisted Resin Transfer Molding) had poor mechanical properties because the fiber volume fraction was very small.

    VARTM工艺成型的固体火箭发动机壳体复合材料连接裙段构件纤维体积含量较低,复合材料力学性能不佳。

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