{
  "$type": "site.standard.document",
  "description": "An anti-icing system (38) for a gas turbine system (10) includes multiple nozzles (40), wherein each nozzle (40) of the multiple nozzles (40) includes one or more outlets (102) that are configured to inject a heated fluid into an airflow (34) within an air intake conduit (13). The anti-icing system…",
  "path": "/patents/1388383",
  "publishedAt": "2026-01-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/04",
    "GENERAL ELECTRIC TECHNOLOGY GMBH [CH]"
  ],
  "textContent": "An anti-icing system (38) for a gas turbine system (10) includes multiple nozzles (40), wherein each nozzle (40) of the multiple nozzles (40) includes one or more outlets (102) that are configured to inject a heated fluid into an airflow (34) within an air intake conduit (13). The anti-icing system (38) also includes multiple plates (90) disposed upstream of the one or more outlets (102), wherein each plate (90) of the multiple plates (90) extends laterally across the air intake conduit (13) and is vertically spaced apart from one or more adjacent plates (90) to define one or more vertically-extending gaps (96). The multiple plates (90) are configured to direct the airflow (34) through the one or more vertically-extending gaps (96) to spread the airflow (34) upstream of the one or more outlets (102) to facilitate mixing of the heated fluid and the airflow (34).",
  "title": "ANTI-ICING SYSTEM WITH A FLOW-DEFLECTOR ASSEMBLY"
}