{
  "$type": "site.standard.document",
  "description": "The gas turbine thrust reverser has a cowl (28) whose rear portion (30) is more displaced in the axial direction of an engine. An annular free space arises in a front portion (29) of the cowl. The turning elements and blockage elements are coupled to rear portion of the cowl. A drive element is…",
  "path": "/patents/987211",
  "publishedAt": "2013-08-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/64",
    "ROLLS ROYCE DEUTSCHLAND [DE]"
  ],
  "textContent": "The gas turbine thrust reverser has a cowl (28) whose rear portion (30) is more displaced in the axial direction of an engine. An annular free space arises in a front portion (29) of the cowl. The turning elements and blockage elements are coupled to rear portion of the cowl. A drive element is arranged between the front portion and the rear portion to cause axial displacement of the rear portion. A drive element is formed in two stages for partial and full axial displacements of rear portion of cowl.",
  "title": "Aviation gas turbine thrust reversing device"
}