{
  "$type": "site.standard.document",
  "description": "Aircraft (1) fitted with a turbine engine (10) comprising a gas generator (15), the gas generator (15) comprising a compression assembly (20) supplying air to a combustion chamber (24) as well as a turbine assembly (25) supplied with gas by the combustion chamber (24), the aircraft (1) having a…",
  "path": "/patents/1386298",
  "publishedAt": "2026-02-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D33/02",
    "AIRBUS HELICOPTERS [FR]"
  ],
  "textContent": "Aircraft (1) fitted with a turbine engine (10) comprising a gas generator (15), the gas generator (15) comprising a compression assembly (20) supplying air to a combustion chamber (24) as well as a turbine assembly (25) supplied with gas by the combustion chamber (24), the aircraft (1) having a plenum (40) supplying air to the compression assembly (20). The aircraft (1) comprises a heating system (50), the heating system (50) comprising a heat exchanger (60) disposed in the plenum (40), the heating system (50) comprising a supply fluid link (70) and a discharge fluid link (80) connected to the heat exchanger (60), the supply fluid link (70) conveying hot air coming from the turbine engine (10) into the heat exchanger (60).",
  "title": "AIRCRAFT PROVIDED WITH A HEATING SYSTEM FOR A TURBINE ENGINE PLENUM",
  "updatedAt": "2026-06-11T15:50:40.426Z"
}