摘要
针对复合材料构件在固化时易报废的情况,提出了在预吸胶后先检测再固化的方法,并将新方法与原工艺的试验结果进行了对比。
A new method is put forward,i.e.composite structure part is inspected after prebleeding and then cured because the part is easily rejected during cure.The new method is compared with the old one in the paper as well.
出处
《航空工艺技术》
1997年第5期33-33,40,共2页
Aeronautical Manufacturing Technology
关键词
树脂基
飞机
复合材料构件
无损检测
固化成型
Resin matrix composite
Aircraft composite structure part
Nondestructive testing
Cure
