{
  "$type": "site.standard.document",
  "description": "A head impact criteria (HIC) device (200) for a controlling a breakover rate of a seatback (110) of an aircraft seat (100), and a method of manufacturing (300) the same, are disclosed. A first energy absorbing member (210) is coupled to the seatback of the aircraft seat. A second energy absorbing…",
  "path": "/patents/1396685",
  "publishedAt": "2025-04-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60N2/42709",
    "BE AEROSPACE INC [US]"
  ],
  "textContent": "A head impact criteria (HIC) device (200) for a controlling a breakover rate of a seatback (110) of an aircraft seat (100), and a method of manufacturing (300) the same, are disclosed. A first energy absorbing member (210) is coupled to the seatback of the aircraft seat. A second energy absorbing member (220) is coupled to a frame (120) of the aircraft seat. A fuse link (230) is encapsulated by the first energy absorbing member and the second energy absorbing member. In response to the HIC device being subjected to a threshold load associated with a dynamic event, the fuse link breaks and the first energy absorbing member and the second energy absorbing member rotate around the axis (240).",
  "title": "HEAD IMPACT CRITERIA MITIGATING DEVICE INCLUDING FUSE LINK"
}