{
  "$type": "site.standard.document",
  "description": "A method of braking left and light landing gear wheels on respective left and right sides of an aircraft. A desired left braking parameter (L) is received for the left wheel and a desired right braking parameter (R) is received for the right wheel. The left wheel is braked with a reduced left…",
  "path": "/patents/946545",
  "publishedAt": "2016-01-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T8/00",
    "AIRBUS OPERATIONS LTD [GB]"
  ],
  "textContent": "A method of braking left and light landing gear wheels on respective left and right sides of an aircraft. A desired left braking parameter (L) is received for the left wheel and a desired right braking parameter (R) is received for the right wheel. The left wheel is braked with a reduced left braking parameter (L') which is less than the desired left braking parameter (L), and the right wheel is braked with a reduced light braking parameter (R') which is less than the desired right braking parameter (R). A difference between the braking parameters is maintained so that L'-R'=L-R.",
  "title": "DIFFERENTIAL BRAKING OF AIRCRAFT LANDING GEAR WHEELS"
}