Ostoskori (0)
Standardi

SAE AMS3970/6

Voimassa
Esikatsele

Lisää mahdolliset korjaukset ja lisäykset ostoskoriin alta.

Kieli
Toimitustavat

Soveltamisala

This Material Specification defines the requirements of carbon fiber reinforced epoxy prepreg for repair, 120 °C (250 °F) Vacuum curing, Plain Weave Fabric, 193 g/m 2x and a companion non-structural glass fiber fabric reinforced epoxy prepreg, 105 g/m 2x, qualified according to AMS3970/1 and AMS3970/2 for aerospace application. The prepreg system may include an epoxy film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests. If included, the requirements to be met by the adhesive are also defined in this document.

Julkaisun tiedot

  • Standardi julkaisijalta SAE International
  • Julkaistu:
  • Julkaisutyyppi: IS
  • Pages
  • Publisher SAE International
  • Distributor SAE International

Sidokset

  • Enums.Sd.Shared.Models.ProductRelationType.REFERRED_BY: SAE AMS3970/1A
  • Enums.Sd.Shared.Models.ProductRelationType.REFERRED_BY: SAE AMS3970/2A
  • Enums.Sd.Shared.Models.ProductRelationType.REFERRED_BY: SAE AMS3970A
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AMS3970/5
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AMS3970
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AMS3970/1
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AMS3970/2
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AMS3970/3
  • Enums.Sd.Shared.Models.ProductRelationType.REFERS: SAE AMS3970/4