{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (10) configured to combust gaseous hydrogen fuel comprises a combustor (20) comprising an annular combustion chamber outer casing (36) surrounding an inner combustor case (34) and a fuel manifold (42) configured to provide gaseous fuel to a plurality of fuel injectors (18). The…",
  "path": "/patents/1388134",
  "publishedAt": "2025-03-26T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/222",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "A gas turbine engine (10) configured to combust gaseous hydrogen fuel comprises a combustor (20) comprising an annular combustion chamber outer casing (36) surrounding an inner combustor case (34) and a fuel manifold (42) configured to provide gaseous fuel to a plurality of fuel injectors (18). The fuel manifold (42) is formed integrally with the combustion chamber outer casing (36).",
  "title": "GAS TURBINE ENGINE"
}