首页> 外国专利> Method for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores

Method for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores

机译:利用低密度,稳定的倾斜蜂窝状芯材对具有倾斜表面的轻质蜂窝状芯复合材料制品进行高压共固化成型的方法

摘要

A method for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low total density, stabilized ramped honeycomb cores. The low total density, stabilized ramped honeycomb core is formed by net shaping stabilized honeycomb core material into a ramped honeycomb core, which is prepped for lay-up and co-cure by applying a layer of low areal weight film adhesive to the upper, lower and ramped surfaces thereof. The honeycomb core material is stabilized for the net shaping operation by a layer of the low areal weight film adhesive applied to the upper and lower surfaces of the material in a predetermined picture frame format. Composite prepregs and the ramped honeycomb core are layed-up in a semi- rigid molding assembly including a rigid base member and a complementary semi-rigid mold member having at least one internal rigid reinforcement insert, which is vacuum bagged and disposed in an autoclave. The vacuum bag is evacuated, and the layed-up molding assembly is subjected to a two stage pressure, temperature cycle for high pressure co-cure. The autoclave is pressurized to a dwell pressure, and the temperature is then raised from ambient to a dwell temperature whereupon the autoclave is stabilized for a dwell period. Next, the autoclave pressure is increased to a high pressure, and the temperature is raised to a co-cure temperature whereupon the autoclave is stabilized for a co-cure period to effect curing of the lay-up. After curing is complete, the autoclave is cooled, and then depressurized for removal of the composite molding apparatus.
机译:一种利用具有低总密度的稳定的倾斜蜂窝状芯对具有倾斜表面的轻质蜂窝状芯复合制品进行高压共固化成型的方法。通过将稳定的蜂窝状芯材净成形为倾斜的蜂窝状芯材,形成低总密度,稳定的倾斜蜂窝状芯材,该蜂窝状芯材可通过在上,下层涂一层低面积重量的薄膜胶粘剂进行铺层和共固化及其倾斜的表面。蜂窝状芯材通过一层低面积重量的薄膜胶粘剂进行稳定的净成形操作,该胶粘剂层以预定的相框格式涂在材料的上,下表面。将复合材料预浸料和倾斜的蜂窝状芯层叠在半刚性模制组件中,该组件包括刚性基座构件和互补的半刚性模具构件,该互补的半刚性模具构件具有至少一个内部刚性增强插入件,该内部刚性增强插入件被真空包装并置于高压釜中。抽空真空袋,并使叠层的成型组件经受两阶段的压力,温度循环,以进行高压共固化。将高压釜加压至保压压力,然后将温度从环境温度升高至保压温度,随后使高压釜稳定一段保压时间。接下来,将高压釜压力升高至高压,并且将温度升高至共固化温度,随后将高压釜稳定共固化时间以实现叠层的固化。固化完成后,将高压釜冷却,然后减压以取出复合成型设备。

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