{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
    "ref": {
      "$link": "bafkreibqbbu6paq5zpdwwsdponlnr75cmirm66xwgrbjomogggvuuf674m"
    },
    "mimeType": "image/png",
    "size": 101139
  },
  "description": "The activator has a support (116) mounted on a base (110) and rotated around an axis (120) by a direct current torque motor (124). The support holds a spinner (134) rotated around an axis (132) that is perpendicular to the axis (120), by a torque motor (144). The spinner has two flanges (136)…",
  "path": "/patents/1081878",
  "publishedAt": "2004-12-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64G1/244",
    "EADS ASTRIUM SAS [FR]"
  ],
  "textContent": "The activator has a support (116) mounted on a base (110) and rotated around an axis (120) by a direct current torque motor (124). The support holds a spinner (134) rotated around an axis (132) that is perpendicular to the axis (120), by a torque motor (144). The spinner has two flanges (136) connected by a shaft (142) that has a diameter less than that of the flanges. The support has a tube (122) on which the shaft turns.",
  "title": "Gyroscopic actuator specially for the attitude control of a satellite"
}