{
  "$type": "site.standard.document",
  "description": "A lubrication system (70) for a gas turbine engine (20) may include a pump (86) for moving a lubricant through a conduit from a lubricant tank (82) to an engine component (80). Further, a scheduling valve (94) positioned in the conduit (90) between the lubricant tank (82) and the engine component…",
  "path": "/patents/1419824",
  "publishedAt": "2023-07-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/20",
    "RAYTHEON TECH CORP [US]"
  ],
  "textContent": "A lubrication system (70) for a gas turbine engine (20) may include a pump (86) for moving a lubricant through a conduit from a lubricant tank (82) to an engine component (80). Further, a scheduling valve (94) positioned in the conduit (90) between the lubricant tank (82) and the engine component (80) may vary a flow of the lubricant (74) to the engine component (78) based on a condition.",
  "title": "LUBRICATION SYSTEM FOR GAS TURBINE ENGINES"
}