{
  "$type": "site.standard.document",
  "description": "An upstream end (22) and a downstream end (24) of a channel (40) are connected to a port (44) and disposed within a low-pressure turbine nozzle (12), respectively. The channel forms a bypass fluid flow path (27) between the nozzle and an inter-turbine duct (20) comprising an annular structure…",
  "path": "/patents/1087639",
  "publishedAt": "2004-04-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/105",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "An upstream end (22) and a downstream end (24) of a channel (40) are connected to a port (44) and disposed within a low-pressure turbine nozzle (12), respectively. The channel forms a bypass fluid flow path (27) between the nozzle and an inter-turbine duct (20) comprising an annular structure. Independent claims are also included for the following: (1) gas turbine engine system; and (2) gas turbine engine performance optimization method.",
  "title": "Self-aspirating high-area-ratio interstage turbine duct assembly for use in a gas turbine engine"
}