{
  "$type": "site.standard.document",
  "description": "A braking system (200) for an aircraft (100) is disclosed herein. The braking system (200) may comprise: a brake assembly (118; 218); a hydraulic braking subsystem (202) having a hydraulic brake actuator (217) configured to operate the brake assembly (118; 218); an electric braking subsystem (204)…",
  "path": "/patents/1397883",
  "publishedAt": "2025-07-09T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T13/662",
    "GOODRICH CORP [US]"
  ],
  "textContent": "A braking system (200) for an aircraft (100) is disclosed herein. The braking system (200) may comprise: a brake assembly (118; 218); a hydraulic braking subsystem (202) having a hydraulic brake actuator (217) configured to operate the brake assembly (118; 218); an electric braking subsystem (204) and a hydraulic braking subsystem (202). During a flight, one of the electric braking subsystem (204) and the hydraulic braking subsystem (202) may be selected as a primary braking system (200). The braking system (200) may be configured to command braking of a brake assembly (118; 218) by the hydraulic braking subsystem (202) and the electric braking subsystem (204) during an RTO phase of the flight. The braking system (200) may be configured to command braking of a brake assembly (118; 218) by a secondary braking system (200) in response to a failure of a primary braking system (200) during the RTO phase of the flight.",
  "title": "HYBRID BRAKE SYSTEMS AND METHODS"
}