{
  "$type": "site.standard.document",
  "description": "The method involves controlling an electromechanical actuator (EMA) that is not connected to a battery assembly to exert a force equal to a unitary maintenance force that is determined independently of a braking request of a pilot. The unitary maintenance force is a predetermined force and is…",
  "path": "/patents/1077155",
  "publishedAt": "2005-06-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T8/00",
    "MESSIER BUGATTI [FR]"
  ],
  "textContent": "The method involves controlling an electromechanical actuator (EMA) that is not connected to a battery assembly to exert a force equal to a unitary maintenance force that is determined independently of a braking request of a pilot. The unitary maintenance force is a predetermined force and is calculated based on thrust of aircraft engines. An independent claim is also included for braking system architecture to implement a method of controlling the architecture.",
  "title": "Braking system architecture managing method for an aircraft with electro-mechanical brakes as well as braking system architecture"
}