{
  "$type": "site.standard.document",
  "description": "The invention relates to a propulsion assembly (151) for an aircraft comprising a T-shaped frame (156) with a horizontal structure (156a) and a vertical structure (156b), a gearbox (155) fixed to the front of the frame (156) and a propulsion system (150) comprising the following propulsion…",
  "path": "/patents/1391985",
  "publishedAt": "2025-06-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L50/70",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The invention relates to a propulsion assembly (151) for an aircraft comprising a T-shaped frame (156) with a horizontal structure (156a) and a vertical structure (156b), a gearbox (155) fixed to the front of the frame (156) and a propulsion system (150) comprising the following propulsion elements: an electric motor (154a) driving the components of the gearbox (155), a fuel cell (154b), a tank and a cooling system (154d), where the propulsion elements (154a-d) are fixed under the horizontal structure (156a) and against the vertical structure (156b) by fixing means. [0002] With such an arrangement, it is easy to access each propulsion element from the side of the chassis during maintenance operations.",
  "title": "PROPELLER PROPULSION ASSEMBLY FOR AIRCRAFT"
}