With the acquirement of excellent FST behaviors and convenient manufacture of composites in aircraft and mass-transit interior laminate and sandwich panels,
The forming process of composite vane of hollow pipe with large length to diameter ratio was investigated, the method of forming process including co-curing
The key technological parameters and problems during the two-step hot melt preprag production, includes the drying and coating temperature of resin, fiber s
By using thermocouple and fiber bragg grating sensor, the temperature and strain profile of the composite in autoclave process were in situ monitored, strai
In the processing of fiber placement, due to the coefficient of thermal expansion of the fiber and matrix is not matching and the action of thermos-mechanic