{
  "$type": "site.standard.document",
  "description": "The invention provides an aircraft brake control system for controlling antiskid braking of an aircraft wheel, the system comprising a control assembly 300 having a mode controller 327 which sets the mode of operation of an antiskid brake calculator 325, configured to set a first mode, when an…",
  "path": "/patents/1406422",
  "publishedAt": "2023-12-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T13/662",
    "AIRBUS OPERATIONS LTD [GB]"
  ],
  "textContent": "The invention provides an aircraft brake control system for controlling antiskid braking of an aircraft wheel, the system comprising a control assembly 300 having a mode controller 327 which sets the mode of operation of an antiskid brake calculator 325, configured to set a first mode, when an input of the indication of a brake energy supply configuration 305 indicates a first brake energy supply being used, in which the antiskid brake calculator applies a first restriction level on a rise rate of the antiskid brake command 330, and a second mode, when the input 305 indicates a second brake energy supply being used, in which the antiskid brake calculator applies a second, lower, restriction level on a rise rate of the antiskid brake command. The invention also provides other aircraft brake control systems, aircraft landing gear, aircraft and methods of braking an aircraft.",
  "title": "AN AIRCRAFT BRAKE CONTROL SYSTEM"
}