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THERMOFORMING HEADER OF SINGLE CURVATURE PARTS Sub<strong>header</strong> <strong>TenCate</strong> Reet ut venim Cetex ad magna feu facillu mmodit lam zzriuscil del ex et, conOrting eum non henisci lisisim vulputat consequisit delenim digna con hent augait, sisl diam, vel et amcommo adit, quismolenit, quisl iurer susci tin ea alit prat adip eugiat loborem num ip ercilla dolese tat, suscilis ent dolorperil illum in utpat. Ed dio odiam, vulla faciliquatue alit inis eu faciduis dolortio dolor incipis duipit accum aliquisi. Agnis nonsecte dolorpe rcinci tie feu facin dolessim veriuscidunt et ut laorem velesequat ad feugue facilla feuissequis alis alit alit diamcom moluptat. Ut ad tin vel ipsum amefaccum ent nos nonsequi blaor alit dionsequat lor inim incing num vulluptate vel euissim illa ad er si euisl e, con Rserddeet ut venim ad magna feu facillu mmodit et amcommo loborem Erciliq uating elesequate consenisit iriusci nos am, vel utem num ercilla oreriurem dolese, mmodit suscilis ent dolorperil dolore facin ullamcor secte tatum euguero deliqui er iuscinc illum dolor incipis duipit accum er aliquisi. tisit vel ulput vuautat nis nullam zzrit praesecte velisl delis nim nos am, vel utem dolore facin ullamcor secte tatum Agnis alit diamcom moluptat. Ut ad tin vel ipsum ametums euguero deliqui er iuscinc consequis niatio con ullum dio andipsum adit vent nulputpat lamet lum ad magna faccum consendipisi exer susci tisit vel ulput vuautat nis nullam zzrit veraestrud ent num vulluptate vel euissim illa ad er si euisl praesecte velisl delis nim autat, quisi eugait ® System3 can be easily thermoformed into single and fi xing them to the core material again utilising the thermoplastic curvature parts and subsequently assembled without damage to the adhesive as the fi xing agent. high quality surface fi nish of the facing skins. To form shapes, a one This process takes minutes, not hours and again like the panel sided or match tooling philosophy can be applied and in some cases manufacture the fi nal parts need little of no fi nishing. This process tooling cost can be minimised to using sheet metal forms or MDF allows many interior profi les to be manufactured easily like the A340 forms. The basis of the process is stress forming the surface skins lightweight overhead bin produced by AIM aviation. 6 AEROSPACE COMPOSITES Heat up Heat Heat Form Tool Tool
SEE THE BENEFITS IN THE FINISHING TIMELINE 1 HR 1 HR 1 HR 1 HR 1 HR 2 HRS Paint finish Primer Primer Sand and sweep Primer Primer Sand and sweep Moulding � Phenolic or Sytem 3 � 7 Hours max. 3 Hours max. Paint finish (opt.) Primer (opt.) Moulding Taking cost out System 3 1 HR 1 HR 15 mins - HR AEROSPACE COMPOSITES 7
Page 1 and 2: AEROSPACE COMPOSITES Product outlin
Page 3 and 4: A thermoplastic technology driven s
Page 5: TEST RESULTS Skins: GI 0303 002 170

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