{
  "$type": "site.standard.document",
  "description": "The pipe has an internal skin (2) inside which circulates a primary air flow (FP) and which comprises chevrons (4), at an external end. An external skin (3) partially surrounds the internal skin and along which flows a secondary air flow (FS). The external skin is movable along the internal skin. A…",
  "path": "/patents/1073714",
  "publishedAt": "2005-09-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/48",
    "AIRBUS FRANCE [FR]"
  ],
  "textContent": "The pipe has an internal skin (2) inside which circulates a primary air flow (FP) and which comprises chevrons (4), at an external end. An external skin (3) partially surrounds the internal skin and along which flows a secondary air flow (FS). The external skin is movable along the internal skin. A sliding device (5) is placed between the internal skin and the external skin. An independent claim is also included for an aircraft with turbofan engine.",
  "title": "Primary nozzle with chevrons for bypass turboreactor engine of an aircraft and aircraft with such a nozzle"
}