{
  "$type": "site.standard.document",
  "description": "A gas turbine engine assembly is connected to a pylon (14) for mounting the gas turbine engine (10) to an aircraft. The assembly has a frame (26) supporting at least one accessory (35, 50) independently of the gas turbine engine (10). The frame (26) is attached to the pylon (14) at forward and…",
  "path": "/patents/965569",
  "publishedAt": "2014-12-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/402",
    "ROLLS ROYCE DEUTSCHLAND [DE]"
  ],
  "textContent": "A gas turbine engine assembly is connected to a pylon (14) for mounting the gas turbine engine (10) to an aircraft. The assembly has a frame (26) supporting at least one accessory (35, 50) independently of the gas turbine engine (10). The frame (26) is attached to the pylon (14) at forward and rearward engine mounting locations (16, 18). The frame (26) comprises at least one hollow tube (30, 32, 38) and at least one duct (70) is arranged to supply coolant (58) into the at least one hollow tube (30, 32, 38) and the at least one hollow tube (30, 32, 38) is arranged to supply coolant (58) to the at least one accessory (35, 50).",
  "title": "Gas turbine engine accessory mounting with cooling duct"
}