{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "Disclosed is an aircraft brake temperature control system (BTCS) 100 for controlling a temperature of a brake 220 of a landing gear 201 of the aircraft 200. The BTCS 100 comprises a controller 110 that is configured to cause at least one fluid moving device 230, 231, 232 to drive a flow of fluid…",
  "path": "/patents/1409526",
  "publishedAt": "2024-04-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T17/22",
    "AIRBUS OPERATIONS LTD [GB]"
  ],
  "textContent": "Disclosed is an aircraft brake temperature control system (BTCS) 100 for controlling a temperature of a brake 220 of a landing gear 201 of the aircraft 200. The BTCS 100 comprises a controller 110 that is configured to cause at least one fluid moving device 230, 231, 232 to drive a flow of fluid onto the brake 220, selectively in one of a plurality of modes, to control the temperature of the brake 220. Also disclosed is: an aircraft system 1000 comprising the BTCS 100 and the at least one fluid moving device 230, 231, 232; an aircraft 200 comprising the BTCS 100 or the aircraft system 1000; and a method 300 of controlling a temperature of a brake of a landing gear of an aircraft.",
  "title": "AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM"
}