{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (10) includes a bleed structure (62A) which includes a forward wall (66) and a rear structural wall (64) to define a deposit space downstream of the bleed structure (62A) for a hail event of a predetermined duration.",
  "path": "/patents/1004108",
  "publishedAt": "2012-03-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/105",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A gas turbine engine (10) includes a bleed structure (62A) which includes a forward wall (66) and a rear structural wall (64) to define a deposit space downstream of the bleed structure (62A) for a hail event of a predetermined duration.",
  "title": "Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events"
}