{
  "$type": "site.standard.document",
  "description": "The intake (18) has an annular internal shell (30) including fluid passage orifices, and an annular lip (24) connected to external and internal downstream edges (28, 32) of external shroud (26) and the shell, so as to form a leading edge of the intake. The shell has a portion (43) devoid of fluid…",
  "path": "/patents/1001362",
  "publishedAt": "2012-06-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D33/02",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The intake (18) has an annular internal shell (30) including fluid passage orifices, and an annular lip (24) connected to external and internal downstream edges (28, 32) of external shroud (26) and the shell, so as to form a leading edge of the intake. The shell has a portion (43) devoid of fluid passage orifices extending axially from an upstream edge (44) of the shell at a distance (L) ranging between 20 percent and 90 percent or axial average area of the shell and comprising a circumferential area ranging between 60 and 150 degrees around a longitudinal axis (46) of the intake. An independent claim is also included for a method for repairing an air intake of nacelle of propulsive system of aircraft.",
  "title": "Air intake for propulsion system of an aircraft with a structure withstanding overpressure and method for repairing an air intake of an aircraft propulsion system"
}