{
  "$type": "site.standard.document",
  "description": "An exhaust nozzle (10) for an aircraft engine includes a mount (20) for attaching the nozzle (10) to a downstream end of the engine and first and second opposed upstream flaps (30) moveably connected to the mount (20) having inner surfaces (34) defining an upstream exhaust gas flow path. Each…",
  "path": "/patents/1105379",
  "publishedAt": "2002-04-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C15/02",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "An exhaust nozzle (10) for an aircraft engine includes a mount (20) for attaching the nozzle (10) to a downstream end of the engine and first and second opposed upstream flaps (30) moveably connected to the mount (20) having inner surfaces (34) defining an upstream exhaust gas flow path. Each upstream flap (30) extends between an upstream end and a downstream end and is moveable relative to the mount (20) between an open position in which the downstream ends of the upstream flaps (30) are spaced by a first distance, and a closed position in which the downstream ends touch to substantially block flow through the exhaust gas flow path. First and second opposed downstream flaps (50) are moveably connected to the first and second upstream flaps (30) having inner surfaces (52) defining a downstream exhaust gas flow path.",
  "title": "Flow blocking exhaust nozzle"
}