{
  "$type": "site.standard.document",
  "description": "A vane assembly (200) for a gas turbine engine (10). The vane assembly is a single unitary component that includes an aerofoil (202). The vane assembly further includes a leading edge passageway (230) disposed proximal to a leading edge (210) of the aerofoil and configured to receive a flow of a…",
  "path": "/patents/1399132",
  "publishedAt": "2025-12-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/02",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "A vane assembly (200) for a gas turbine engine (10). The vane assembly is a single unitary component that includes an aerofoil (202). The vane assembly further includes a leading edge passageway (230) disposed proximal to a leading edge (210) of the aerofoil and configured to receive a flow of a fluid (220) therein. The vane assembly further includes a connecting passageway (250) fluidly communicating the leading edge passageway with a trailing edge distribution passageway (240) that is spaced apart from the leading edge, the leading edge passageway (230) and a trailing edge (208) of the aerofoil. The vane assembly further includes a plurality of trailing edge passageways (260) disposed proximal to a pressure surface (212) of the aerofoil and extending from the trailing edge distribution passageway towards the trailing edge along a chordwise direction (C). Each of the plurality trailing edge passageways is configured to discharge the fluid through a corresponding passageway outlet (270) disposed on the pressure surface and in fluid communication with a corresponding trailing edge passageway.",
  "title": "VANE ASSEMBLY FOR A GAS TURBINE ENGINE"
}