{
  "$type": "site.standard.document",
  "description": "A method is provided during which a composite preform is provided that includes an electric heater (44), fiber-reinforcement and thermoset material. The composite preform is consolidated to provide a composite aircraft component (22). The consolidating includes heating the thermoset material using…",
  "path": "/patents/1395151",
  "publishedAt": "2026-04-22T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B29C35/0266",
    "ROHR INC [US]"
  ],
  "textContent": "A method is provided during which a composite preform is provided that includes an electric heater (44), fiber-reinforcement and thermoset material. The composite preform is consolidated to provide a composite aircraft component (22). The consolidating includes heating the thermoset material using the electric heater (44) to cure the thermoset material. The electric heater (44) and the fiber-reinforcement are embedded within the cured thermoset material. The electric heater (44) is configured as a part of a thermal anti-icing system (24) for melting and/or preventing ice accumulation on an exterior surface (28) of the composite aircraft component (22).",
  "title": "CURING THERMOSET MATERIAL USING ELECTRIC HEATER(S) FOR THERMAL ANTI-ICING SYSTEM"
}