{
  "$type": "site.standard.document",
  "description": "The present embodiments relate to an electrical system 150, and, more particularly, to an electrical system 150 for an aircraft 100 comprising one or more energy sinks 240 and a hybrid energy storage system 200. The hybrid energy storage system 200 may comprise one or more primary energy sources…",
  "path": "/patents/1421902",
  "publishedAt": "2025-06-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L1/003",
    "AIRBUS HELICOPTERS DEUTSCHLAND GMBH [DE]"
  ],
  "textContent": "The present embodiments relate to an electrical system 150, and, more particularly, to an electrical system 150 for an aircraft 100 comprising one or more energy sinks 240 and a hybrid energy storage system 200. The hybrid energy storage system 200 may comprise one or more primary energy sources 210, a secondary energy source 220, and a secondary energy source control unit 230. The one or more primary energy sources 210 may be coupled to and supply power to the one or more energy sinks 440. The secondary energy source 220 may be coupled to the one or more primary energy sources 210 and adapted to supply power at a variable output voltage 324 to the one or more primary energy sources 210a to 210n.",
  "title": "A HYBRID ENERGY STORAGE SYSTEM"
}