{
  "$type": "site.standard.document",
  "description": "A thrust reverser for a turbofan engine having an air duct defined radially inwardly by a cowl (10) around a gas turbine and radially outwardly in part by a fan case (12) of the engine includes a bulkhead (22) that is adapted to be mounted on the fan case (12). A translating sleeve (18) is…",
  "path": "/patents/1102650",
  "publishedAt": "2002-08-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/566",
    "ROHR INC [US]"
  ],
  "textContent": "A thrust reverser for a turbofan engine having an air duct defined radially inwardly by a cowl (10) around a gas turbine and radially outwardly in part by a fan case (12) of the engine includes a bulkhead (22) that is adapted to be mounted on the fan case (12). A translating sleeve (18) is supported for movement axially between a closed position adjacent the bulkhead (22) and an open position spaced apart axially to the rear of the bulkhead (22) so as to form a outlet opening for discharge of air from the air duct. A cascade array (40) fixed in the outlet opening has a substantially conical portion, the forward end of which is of a diameter substantially smaller than the diameter of the rearward end.",
  "title": "Cascade-type thrust reverser"
}