{
  "$type": "site.standard.document",
  "description": "A liner assembly for use in a combustor (56) of a gas turbine engine (20) is disclosed. In various embodiments, the liner assembly includes a panel (200; 300) defining a left side and a right side and a hot side (202) and a cold side, the panel having a dilution hole (206; 306) and a plurality of…",
  "path": "/patents/1420688",
  "publishedAt": "2023-12-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/18",
    "RTX CORP [US]"
  ],
  "textContent": "A liner assembly for use in a combustor (56) of a gas turbine engine (20) is disclosed. In various embodiments, the liner assembly includes a panel (200; 300) defining a left side and a right side and a hot side (202) and a cold side, the panel having a dilution hole (206; 306) and a plurality of effusion holes (204; 304) extending between the hot side (202) and the cold side. In various embodiments, the plurality of effusion holes (204; 304) includes a first subgrouping (320) of effusion holes (204; 304) disposed downstream of the dilution hole (206; 306) and aligned in a generally left to right orientation toward a dividing line (318) extending downstream of the dilution hole (206; 306) and a second subgrouping (322) of effusion holes (204; 304) disposed downstream of the dilution hole (206; 306) and aligned in a generally right to left orientation toward the dividing line (318) extending downstream of the dilution hole (206; 306).",
  "title": "COMBUSTOR PANEL AND METHOD FOR COOLING THE SAME"
}