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AFRL(美国空军实验室)和波音公司在“复合材料成本可承受的创新C-17”技术转移演示项目中,开发出一种长寿命的C-17主起落架(MLG)复合材料舱门,其具有穿刺编织预成型件和真空辅助树脂浸渍成型的工艺特点,并改进了整体设计外形。为降低C-17主起落架舱门开启失效率,提高飞机执行任
AFRL (United States Air Force Laboratory) and Boeing developed a long-life MLG composite hatchback at the “Composites Cost Affordable Innovation C-17” technology transfer demonstration project, It has the process characteristics of piercing braided preform and vacuum assisted resin impregnation molding, and improves the overall design profile. In order to reduce the failure rate of C-17 main landing gear door opening and improve the performance of aircraft