{
  "$type": "site.standard.document",
  "description": "The invention relates to a propulsion assembly for an aircraft comprising a chassis (180) in the form of a cage with bars (181), a turbine, a dihydrogen supply pipe (170) winding inside a nacelle (149) to the rear of the turbine, with a radial step (204) towards the outside of the nacelle (149), a…",
  "path": "/patents/1390604",
  "publishedAt": "2025-11-26T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/12",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The invention relates to a propulsion assembly for an aircraft comprising a chassis (180) in the form of a cage with bars (181), a turbine, a dihydrogen supply pipe (170) winding inside a nacelle (149) to the rear of the turbine, with a radial step (204) towards the outside of the nacelle (149), a ramp with a radial step towards the outside of the nacelle (149), a bypass pipe (182) connected between the two radial steps (202) and to the outside of the nacelle (149), and protection means (300) comprising a protection plate (302), fastening means (306) of the protection plate (302) to the bars (181), and an absorption means (304) between the protection plate (302) and the associated bar (181). With such an arrangement, a blade of the turbine which becomes detached would be stopped in its motion by the protection and absorption means.",
  "title": "PROPULSION ASSEMBLY FOR AIRCRAFT",
  "updatedAt": "2026-06-18T17:31:19.457Z"
}