Toggle navigation
Menu
home
Foundation
Origins of the foundation
General Objectives
Government Agency
Technical Orientation
Organization
Facilities
Workshop
Tape Lay up
ATL
AFP
Thermoplastics
Hot forming
Hot forming membrane
Hot forming press
Curing
Ovens
Autoclaves
Press
Hot plate press
Injection
Flat panel injection tool
Injection machines
NDT
Advanced manufacturing
ALM
Robots
Laboratory
Chemical Physical laboratory
Mechanical laboratory
Specimen preparation
Projects
Thermostable Prepreg
Dry fiber and resin transfer processing
Thermoplastic
Processes of manufacture of high cadence
Analysis and simulation of processes
Additive manufacturing
Training
Customers
News
Contact
Work with us
Projects
Project Detail
PBR
Preimpregnated materials
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.
123movies