{
  "$type": "site.standard.document",
  "description": "A propulsion system for an aircraft includes a propulsor, an engine, and an electrical distribution system. The engine includes a first rotor and a first shaft. The first shaft is connected to the first rotor. The electrical distribution system includes a low-voltage bus, a high-voltage bus, a…",
  "path": "/patents/1371341",
  "publishedAt": "2024-11-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D31/00",
    "Pratt & Whitney Canada Corp."
  ],
  "textContent": "A propulsion system for an aircraft includes a propulsor, an engine, and an electrical distribution system. The engine includes a first rotor and a first shaft. The first shaft is connected to the first rotor. The electrical distribution system includes a low-voltage bus, a high-voltage bus, a low-voltage generator, a DC:DC converter, and an electric motor. The low-voltage generator is coupled to the first shaft and electrically connected to the low-voltage bus. The low-voltage generator is configured to generate low-voltage electrical power and supply the low-voltage electrical power to the low-voltage bus. The DC:DC converter is electrically connected to the low-voltage bus and the high-voltage bus. The DC:DC converter is configured to convert the low-voltage electrical power to high-voltage electrical power and supply the high-voltage electrical power to the high-voltage bus. The electric motor is electrically connected to the high-voltage bus. The electric motor is configured to drive rotation of the propulsor.",
  "title": "SYSTEMS AND METHODS FOR CONTROLLING AN ELECTRICAL DISTRIBUTION SYSTEM FOR A HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEM"
}