{
  "$type": "site.standard.document",
  "description": "An assembly (72) is provided for an aircraft propulsion system (20). This aircraft propulsion system assembly (72) includes a thrust reverser system (38). The thrust reverser system (38) includes a cascade structure (68) and a scoop (94). The cascade structure (68) is configured with a plurality of…",
  "path": "/patents/1407981",
  "publishedAt": "2024-11-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/56",
    "ROHR INC [US]"
  ],
  "textContent": "An assembly (72) is provided for an aircraft propulsion system (20). This aircraft propulsion system assembly (72) includes a thrust reverser system (38). The thrust reverser system (38) includes a cascade structure (68) and a scoop (94). The cascade structure (68) is configured with a plurality of flow passages (92). Each of the flow passages (92) extends through the cascade structure (68). The flow passages (92) include a first flow passage (92A). The scoop (94) is configured to direct fluid into at least the first flow passage (92A). The scoop (94) includes a serrated leading edge (102).",
  "title": "FLUID SCOOP FOR A THRUST REVERSER SYSTEM"
}