{
  "$type": "site.standard.document",
  "description": "The wall has a set of heat exchangers, and a separator nose (10) for separating a primary flow and a secondary flow. An intermediate casing supports a rotor (2), and a wall portion is placed between a leading edge of the nose and the intermediate casing. A surface air-oil heat exchanger forms an…",
  "path": "/patents/1011425",
  "publishedAt": "2011-06-29T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/14",
    "TECHSPACE AERO SA [BE]"
  ],
  "textContent": "The wall has a set of heat exchangers, and a separator nose (10) for separating a primary flow and a secondary flow. An intermediate casing supports a rotor (2), and a wall portion is placed between a leading edge of the nose and the intermediate casing. A surface air-oil heat exchanger forms an annular segment of the wall portion, and a support arm (8) is fixed on the intermediate casing. The support arm extends from the intermediate casing towards the leading edge. Independent claims are also included for the following: (1) a turbojet engine comprising a nacelle (2) a method for cooling oil of a lubrication and cooling circuit of a bypass axial turbo machine.",
  "title": "Inner side of the annular bypass duct of a turbojet engine and method for assembling such an annular duct"
}