{
  "$type": "site.standard.document",
  "description": "The aircraft (1) has a main combustion engine (6) e.g. oil engine, and an auxiliary electric machine (7) that are mechanically coupled to a power train (8). The power train drives a main rotor (3), in rotation, of a hybrid motorization assembly (5). The hybrid motorization assembly comprises a…",
  "path": "/patents/1006254",
  "publishedAt": "2012-01-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L3/0046",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The aircraft (1) has a main combustion engine (6) e.g. oil engine, and an auxiliary electric machine (7) that are mechanically coupled to a power train (8). The power train drives a main rotor (3), in rotation, of a hybrid motorization assembly (5). The hybrid motorization assembly comprises a hybridization system (37) with an auxiliary electrical wiring system (34). A main electric bus (35) and an auxiliary electric bus (36) are connected by a selective adaptation surface (38) such that an electrical wiring system (16) and the auxiliary electrical wiring system are electrically distinctible. An independent claim is also included for a method for operating an aircraft.",
  "title": "Electric architecture for a rotorcraft with hybrid motorisation and Method"
}