{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (100; 200; 300) includes a hydrogen fuel delivery assembly (202) configured to deliver a hydrogen fuel flow, a compressor section (110, 112) configured to compress air flowing therethrough to provide a compressed air flow, and a combustor (150; 401; 403; 405; 407; 409)…",
  "path": "/patents/1399477",
  "publishedAt": "2025-08-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/10",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A gas turbine engine (100; 200; 300) includes a hydrogen fuel delivery assembly (202) configured to deliver a hydrogen fuel flow, a compressor section (110, 112) configured to compress air flowing therethrough to provide a compressed air flow, and a combustor (150; 401; 403; 405; 407; 409) including a combustion chamber (430) having a burner length and a burner dome height. The combustion chamber (430) is configured to combust a mixture of the hydrogen fuel flow and the compressed air flow. The combustion chamber (430) is characterized by a combustor size rating between one inch and seven inches.",
  "title": "COMBUSTOR SIZE RATING FOR A GAS TURBINE ENGINE USING HYDROGEN FUEL"
}