{
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  "description": "A lubrication system (60) for a gas turbine engine (20) includes a primary fluid tank (62) to receive a primary fluid, at least one secondary fluid tank (64) to receive at least one fluid additive, and a mixer (66). The mixer (66) has at least a first inlet (68) in fluid communication with the…",
  "path": "/patents/1419184",
  "publishedAt": "2024-04-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/20",
    "RTX CORP [US]"
  ],
  "textContent": "A lubrication system (60) for a gas turbine engine (20) includes a primary fluid tank (62) to receive a primary fluid, at least one secondary fluid tank (64) to receive at least one fluid additive, and a mixer (66). The mixer (66) has at least a first inlet (68) in fluid communication with the primary fluid tank (62) and a second inlet (70) in fluid communication with the at least one secondary fluid tank (64). The mixer (66) has at least one outlet (72) that delivers a mixture of the primary fluid and the at least one fluid additive to a gas turbine engine component (74).",
  "title": "FLUID ADDITIVE SYSTEM"
}