{
  "$type": "site.standard.document",
  "description": "Systems and methods are disclosed herein for an aircraft seat with a dual-function linear actuator (110;410). The linear actuator (110;410) may activate a first adjustable feature by moving in a first direction, and the linear actuator (110;410) may activate a second adjustable feature by moving in…",
  "path": "/patents/938978",
  "publishedAt": "2016-08-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "A47C1/02",
    "AMI IND INC [US]"
  ],
  "textContent": "Systems and methods are disclosed herein for an aircraft seat with a dual-function linear actuator (110;410). The linear actuator (110;410) may activate a first adjustable feature by moving in a first direction, and the linear actuator (110;410) may activate a second adjustable feature by moving in a second direction. The linear actuator (110;410) may include a decoupling mechanism. The decoupling mechanism may decouple the first adjustable feature and the second adjustable feature from the linear actuator (110;410) in response to loss of power to the linear actuator (110;410).",
  "title": "DUAL-FUNCTION SEAT ACTUATOR"
}