{
  "$type": "site.standard.document",
  "description": "A gas turbine engine wash process (40) that facilitates reducing a formation of particulate matter within a gas turbine engine (10) is described. The engine wash process includes injecting (60) a first liquid into the engine to remove particulate matter formed within the engine and adversely…",
  "path": "/patents/1102946",
  "publishedAt": "2002-07-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B08B3/02",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A gas turbine engine wash process (40) that facilitates reducing a formation of particulate matter within a gas turbine engine (10) is described. The engine wash process includes injecting (60) a first liquid into the engine to remove particulate matter formed within the engine and adversely affecting engine operation and performance. A second liquid is then injected (80) into the engine to facilitate reducing a rate of formation of particulate matter within the gas turbine engine as the engine is operated in the future. More specifically, the second liquid is an anti-static liquid that coats compressor blades within the gas turbine engine.",
  "title": "Methods for washing gas turbine engines"
}