{
  "$type": "site.standard.document",
  "description": "A gas turbine engine with a lubrication system (104; 204) includes a ball bearing assembly (108, 110) and a rotor (106) circumscribing a rotational axis and journaled within the ball bearing assembly (108, 110). The gas turbine engine also includes a lubrication system (104;204) located radially…",
  "path": "/patents/1420110",
  "publishedAt": "2023-07-19T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B33Y10/00",
    "RAYTHEON TECH CORP [US]"
  ],
  "textContent": "A gas turbine engine with a lubrication system (104; 204) includes a ball bearing assembly (108, 110) and a rotor (106) circumscribing a rotational axis and journaled within the ball bearing assembly (108, 110). The gas turbine engine also includes a lubrication system (104;204) located radially outward from a rotational axis and radially outward and adjacent to the ball bearing assembly (108, 110), which includes a lubrication channel (124; 224) having an inlet (120) and an outlet (126; 226) and a dispersion cone (128; 228) adjacent to the outlet (126; 226) of the lubrication channel (124; 224).",
  "title": "GAS TURBINE ENGINE WITH A LUBRICATION SYSTEM AND METHOD OF MANUFACTURING IT"
}