{
  "$type": "site.standard.document",
  "description": "System (300) and method for cleaning deposits from a component (102) of an assembled, on-wing gas turbine engine (100) are provided. Accordingly, the method includes operably coupling a delivery assembly (306) to an annular inlet of the core gas turbine engine. A portion of cleaning fluid is…",
  "path": "/patents/1411513",
  "publishedAt": "2024-10-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B08B3/02",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "System (300) and method for cleaning deposits from a component (102) of an assembled, on-wing gas turbine engine (100) are provided. Accordingly, the method includes operably coupling a delivery assembly (306) to an annular inlet of the core gas turbine engine. A portion of cleaning fluid is atomized with the delivery assembly to develop a cleaning mist (312) having a plurality of atomized droplets. The atomized droplets are suspended within any path of the core gas turbine engine from the annular inlet to an axial position downstream of a compressor (124) of the core gas turbine engine. A portion of the cleaning mist is impacted or precipitated onto the component so as to wet the component, and a portion of the deposits on the component is dissolved by the cleaning mist.",
  "title": "SYSTEM AND METHOD FOR CLEANING DEPOSIT FROM A COMPONENT OF AN ASSEMBLED, ON-WING GAS TURBINE ENGINE"
}