{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
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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 a thermal management system 2000 to regulate the temperature of the brake…",
  "path": "/patents/1409508",
  "publishedAt": "2024-06-26T00:00:00.000Z",
  "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 a thermal management system 2000 to regulate the temperature of the brake 220, on the basis of a selection of an objective for regulating the temperature of brake from a plurality of objectives 121, 122 for regulating the temperature of the brake. Also disclosed is: an aircraft 200 comprising the BTCS; and a method 300 of controlling a temperature of a brake of a landing gear of an aircraft.",
  "title": "AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM"
}