{
  "$type": "site.standard.document",
  "description": "A gas turbine engine exhaust nozzle (38) includes a row of laterally sinuous chevrons (42) extending from an aft end of an exhaust duct (40). The chevrons (42) have radially outer and inner surfaces (44, 46) bound by a laterally sinuous trailing edge (48) extending between a base (50) of the…",
  "path": "/patents/1075179",
  "publishedAt": "2005-08-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D33/06",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A gas turbine engine exhaust nozzle (38) includes a row of laterally sinuous chevrons (42) extending from an aft end of an exhaust duct (40). The chevrons (42) have radially outer and inner surfaces (44, 46) bound by a laterally sinuous trailing edge (48) extending between a base (50) of the chevrons adjoining the duct and an axially opposite apex (52) of the chevrons. Each chevron (42) has a compound arcuate contour both axially and laterally, and the sinuous trailing edge (48) of the chevrons further compounds the arcuate configuration of each chevron.",
  "title": "Sinuous chevron exhaust nozzle"
}