{
  "$type": "site.standard.document",
  "description": "An aircraft brake temperature control system (BTCS) for controlling a temperature of a brake of a landing gear of the aircraft . The BTCS includes a controller configured to cause at least one fluid moving device to drive a flow of fluid onto the brake , selectively in one of a plurality of modes…",
  "path": "/patents/1321449",
  "publishedAt": "2022-06-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F16D65/847",
    "Airbus Operations Limited"
  ],
  "textContent": "An aircraft brake temperature control system (BTCS) for controlling a temperature of a brake of a landing gear of the aircraft . The BTCS includes a controller configured to cause at least one fluid moving device to drive a flow of fluid onto the brake , selectively in one of a plurality of modes, to control the temperature of the brake . The BTCS may be incorporated into an aircraft system with at least one fluid moving device , wherein the aircraft system is on an aircraft",
  "title": "AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM"
}