{
  "$type": "site.standard.document",
  "description": "A base assembly (210) for an aircraft seat (200) is disclosed. The base assembly may include one or more leg sub-assemblies (216). Each leg sub-assembly may include a front leg (218), a rear leg (220), and a link beam (226) configured to couple the front leg to a portion of the rear leg. At least…",
  "path": "/patents/1399313",
  "publishedAt": "2024-09-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60N2/015",
    "BE AEROSPACE INC [US]"
  ],
  "textContent": "A base assembly (210) for an aircraft seat (200) is disclosed. The base assembly may include one or more leg sub-assemblies (216). Each leg sub-assembly may include a front leg (218), a rear leg (220), and a link beam (226) configured to couple the front leg to a portion of the rear leg. At least one of the front leg or the rear leg being at least partially formed of a hybrid composite structure. The link beam being at least partially formed of the hybrid composite structure. The hybrid composite structure formed of at least a first material and a second material, where the first material is different from the second material, the first material including a thermoplastic material configured to provide ductility for the base assembly, the second material being a composite material configured to provide strength for the base assembly.",
  "title": "AIRCRAFT SEAT BASE ASSEMBLY"
}