{
  "$type": "site.standard.document",
  "description": "The method involves discharging a part of a secondary air stream to reduce residual thrust of a turbofan (1). The air stream is discharged using a radial opening unit of an engine nacelle (9). The opening unit has an orifice (12) that is closed or opened by a door (13). The air stream passes in a…",
  "path": "/patents/1071418",
  "publishedAt": "2005-12-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C7/02",
    "SNECMA [FR]"
  ],
  "textContent": "The method involves discharging a part of a secondary air stream to reduce residual thrust of a turbofan (1). The air stream is discharged using a radial opening unit of an engine nacelle (9). The opening unit has an orifice (12) that is closed or opened by a door (13). The air stream passes in a secondary tube (10) defined between a case (8) of a turbofan core and an inner wall of the nacelle. An independent claim is also included for a turbofan.",
  "title": "Method for braking aircraft and turbo fan jet engine for implementing the method"
}