{
  "$type": "site.standard.document",
  "description": "A method applies a heat-rejection coating directly on a substrate of a ceramic component. The steps include supplying a ceramic component (40), such as of a gas turbine engine, before applying a reflective-coating mixture onto the component (54), wherein the reflective-coating mixture comprises a…",
  "path": "/patents/1077170",
  "publishedAt": "2005-06-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "C23C24/04",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method applies a heat-rejection coating directly on a substrate of a ceramic component. The steps include supplying a ceramic component (40), such as of a gas turbine engine, before applying a reflective-coating mixture onto the component (54), wherein the reflective-coating mixture comprises a metallic pigment and a reflective-coating-mixture carrier, and wherein the step of applying is accomplished by a method selected from the group consisting of air-assisted spraying, airless spraying, brushing, and decal transfer. The component having the reflective-coating mixture thereon is fired (56) to form a reflective coating on the component.",
  "title": "Sprayable noble metal coating for high temperature use on ceramic and smoothcoat coated aircraft engine parts"
}