• Part: PHG600-68-50
  • Description: Fiber reinforced thermosetting preimpregnated materials
  • Manufacturer: Gurit
  • Size: 92.63 KB
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PHG600-68-50 Datasheet Text

.DataSheet.co.kr PHG600-68-50 Fiber reinforced thermosetting preimpregnated materials for aircraft interior parts. Woven fabric of E-glass filament yarn Style 7781, 296 g/m2, 8H satin, preimpregnated with 53% phenolic resin PH600. Self-adhesive resin system for sandwich panel application Non-halogenated resin formulation Excellent FST behaviour Outstanding adhesion to core materials Adjustable tackiness and retarded flow during curing Long shelf and shop life PDS PHG600-68-50-1-0907 Datasheet pdf - http://..net/ 1 .DataSheet.co.kr Description PHG600-68-50 consists of a E-glass fabric Style 7781, impregnated with the phenolic resin PH600. This resin is a halogen-free and self-adhesive phenolic system designed for wide variety of manufacturing processes, retarded flow during curing, excellent heat-release and smoke-density properties and outstanding adhesion to cores and metallic substrates. This prepreg meets the following AIRBUS material performance specification: ABS5047-08 AIMS 05-10-002 (certification) Cured laminates fulfil the flame-retardant specifications: FAR 25.853 (self-extinguishing) The prepreg is very suitable for the manufacturing of lightweight posite sandwich structures for aircraft interior with high interlaminar shear strength and oustanding adhesion to honeyb cores. Its tackiness is adjustable between dry and tacky to meet the fabrication requirements for press cured flat parts as well as vacuum or autoclave cured plex parts. Both monolithic and sandwich structures can be easily manufactured with this prepreg. The curing can be performed by press, vacuum and autoclave moulding with a pressure of at least 0.07 MPa. ABD 0031 The prepreg material is suitable for: Aviation and aerospace industries Marine and...