{
  "$type": "site.standard.document",
  "description": "A power management system for an aircraft with a hybrid power source comprises a rechargeable electricity source and an electricity generating source, a detector determining status data of the elements of the aircraft power consumption electrical circuit, and power data relating to the…",
  "path": "/patents/1367740",
  "publishedAt": "2024-08-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D31/18",
    "ASCENDANCE FLIGHT TECHNOLOGIES"
  ],
  "textContent": "A power management system for an aircraft with a hybrid power source comprises a rechargeable electricity source and an electricity generating source, a detector determining status data of the elements of the aircraft power consumption electrical circuit, and power data relating to the instantaneous electrical power demanded by the aircraft and/or the charging status of the rechargeable electricity sources, an automaton receiving the power data from the detector and determining a control status for the power sources, an adapter determining a backup electrical configuration when the status data indicate a failure, a controller determining an electrical control for the rechargeable electrical source and the electrical generating source based on the instantaneous electrical power demanded, and a switch emitting commands to the switches of the aircraft power consumption electrical circuit to implement a nominal electrical configuration, or, a backup electrical configuration for the adapter in case of receipt thereof.",
  "title": "SYSTEM FOR MANAGING ENERGY FOR AN AIRCRAFT WITH A HYBRID POWER SOURCE COMPRISING AT LEAST ONE RECHARGEABLE ELECTRICITY SOURCE AND ONE ELECTRICITY GENERATING SOURCE"
}