{
  "$type": "site.standard.document",
  "description": "The engine has a core thruster (10) surrounded by a by-pass channel (29). A radially expressed engine cowl (30) encloses the by-pass channel and is placed at a rear portion of a thrust-reverser (31). The thrust-reverser is moveable relative to the engine cowl. A periphery radiator part e.g. surface…",
  "path": "/patents/996056",
  "publishedAt": "2012-11-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D29/00",
    "ROLLS ROYCE DEUTSCHLAND [DE]"
  ],
  "textContent": "The engine has a core thruster (10) surrounded by a by-pass channel (29). A radially expressed engine cowl (30) encloses the by-pass channel and is placed at a rear portion of a thrust-reverser (31). The thrust-reverser is moveable relative to the engine cowl. A periphery radiator part e.g. surface cooler, matrix cooler and oil cooler, extends in an intermediate area (40) between the engine cowl and the thrust-reverser. The radiator element is arranged at a diverting region (33) of the engine cowl, where the radiator element includes a flow-guiding element (44).",
  "title": "Turbojet engine with oil cooler in the engine nacelle"
}