{
  "$type": "site.standard.document",
  "description": "The seat has beam guides (5) located in a rear portion of the seat and oriented along a direction (Z1) perpendicular to a floor (100) of an aircraft cabin. The beam guides are fixed at a bucket seat (1) interdependent of a structure of connection of the beam guides with the floor. The bucket seat…",
  "path": "/patents/980925",
  "publishedAt": "2013-12-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60N2/20",
    "EADS SOGERMA [FR]"
  ],
  "textContent": "The seat has beam guides (5) located in a rear portion of the seat and oriented along a direction (Z1) perpendicular to a floor (100) of an aircraft cabin. The beam guides are fixed at a bucket seat (1) interdependent of a structure of connection of the beam guides with the floor. The bucket seat is secured at a back side (3) of the seat, where the connection structure comprises four attachment points (110a, 110b) that are arranged on two lines on the floor. The lines are parallel to a longitudinal direction (X) and arranged at a distance from a vertical symmetry plane of the seat.",
  "title": "Aircraft seat with single-beam structure and aircraft comprising such a seat"
}