es-ESen-US

PBR

Preimpregnated materials

PBR


VALUE PROPOSITION

  • To determine the impact damage characteristics of selected geometries of curved panels with frames and stringers. 
  • To understand the damage mechanisms in both blade fragment and fuselage panel, in various impact configurations 
  • To provide data that assists in the validation of ESAZ analysis methods used to assess damage levels on CFRP S19 fuselage skin panels and stringers. 
  • To give preliminary results of velocity in case of panel perforation 

ACHIEVEMENTS

  • Development of a new process for airbus spain 
  • No results are available yet. Structural tests are being carrying out. 


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