{
  "$type": "site.standard.document",
  "description": "The invention provides a bladed rotor wheel of an aero turbine stage comprising a portion of a rotor blade with a shank portion and a bottom surface; a portion of a forged rotor disk with a rim portion and an outer surface; and a joining structure provided by an additive manufacturing process…",
  "path": "/patents/1414690",
  "publishedAt": "2023-06-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B23P15/006",
    "ITP ENGINES UK LTD [GB]"
  ],
  "textContent": "The invention provides a bladed rotor wheel of an aero turbine stage comprising a portion of a rotor blade with a shank portion and a bottom surface; a portion of a forged rotor disk with a rim portion and an outer surface; and a joining structure provided by an additive manufacturing process configured for integrally merging the portion of a rotor blade with the portion of a forged rotor disk. The invention also provides an aero turbine comprising such bladed rotor wheel and an aircraft comprising such aero turbine.",
  "title": "BLADED ROTOR WHEEL"
}