| 摘要 |
PROBLEM TO BE SOLVED: To solve structural problems with composite materials comprising a fillet having a radius filler for use as a component in an aircraft or architecture field.SOLUTION: In one embodiment, a method of forming a composite part comprises: joining a first structural element 310A and a second element 310B to form a fillet 330A at an intersection of the first structural element 310A and the second element 310B; positioning an inflatable radius filler in the fillet 330A; positioning the composite part in a vacuum chamber; venting the inflatable radius filler to an environment external to the vacuum chamber; creating a vacuum in the vacuum chamber; and curing the composite part. |
