{
  "$type": "site.standard.document",
  "description": "The present application thus provides a combustor (100) for use with a gas turbine engine. The combustor may include a turbine nozzle (110) and a liner cooling system (160) integral with the turbine nozzle. The liner cooling system (160) may include a liner (170) with one or more cooling features…",
  "path": "/patents/981015",
  "publishedAt": "2013-12-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "The present application thus provides a combustor (100) for use with a gas turbine engine. The combustor may include a turbine nozzle (110) and a liner cooling system (160) integral with the turbine nozzle. The liner cooling system (160) may include a liner (170) with one or more cooling features thereon and an impingement sleeve (180).",
  "title": "Impingment cooled combustor"
}