{
  "$type": "site.standard.document",
  "description": "A seal 10 for placement in a slot 18 between two turbine components 20 of a gas turbine 110 to seal a gap 19 between the components may include a sealing element 14 sized so as to be capable of placement within the slot 18 and of substantially sealing the gap 19 during operation of the gas turbine…",
  "path": "/patents/974027",
  "publishedAt": "2014-06-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/00",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A seal 10 for placement in a slot 18 between two turbine components 20 of a gas turbine 110 to seal a gap 19 between the components may include a sealing element 14 sized so as to be capable of placement within the slot 18 and of substantially sealing the gap 19 during operation of the gas turbine 110. A sacrificial coating 16 may be located on the sealing element 14. The sacrificial coating 16 may be configured with a size substantially conforming to a size of the slot 18, the sacrificial coating 16 including a material that is removable from the sealing element 14 via heating to a temperature achieved during operation of the gas turbine 110. Related gas turbine assemblies and methods of assembly are also disclosed.",
  "title": "System and method for sealing a gas path in a turbine"
}