{
  "$type": "site.standard.document",
  "description": "An electricity generation and propulsion system of an aircraft is provided. The electricity generation and propulsion system includes a fuselage (120), a hybrid-electric power generation system (130) operably disposed in the fuselage and a ram air turbine (RAT) device (140). The RAT device is…",
  "path": "/patents/1395824",
  "publishedAt": "2025-08-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/10",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "An electricity generation and propulsion system of an aircraft is provided. The electricity generation and propulsion system includes a fuselage (120), a hybrid-electric power generation system (130) operably disposed in the fuselage and a ram air turbine (RAT) device (140). The RAT device is coupled with the hybrid-electric power generation system and is stowable in the fuselage and deployable to an exterior of the fuselage. The RAT device is operable as a RAT when deployed into an airstream that drives rotations of the RAT from which the hybrid-electric power generation system generates electricity, and the RAT device is operable as a propulsor when deployed and driven by the hybrid-electric power generation system.",
  "title": "STOWABLE ELECTRIC-HYBRID PROPFAN"
}