{
  "$type": "site.standard.document",
  "description": "A fuel supply system supplies fuel to a plurality of combustion sectors (70,74) of a combustion section of a gas turbine. Each of the combustion sectors includes at least two combustors. The fuel supply system generally includes a fuel distribution manifold (60) that is in fluid communication with…",
  "path": "/patents/974624",
  "publishedAt": "2014-05-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/222",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A fuel supply system supplies fuel to a plurality of combustion sectors (70,74) of a combustion section of a gas turbine. Each of the combustion sectors includes at least two combustors. The fuel supply system generally includes a fuel distribution manifold (60) that is in fluid communication with a fuel supply. A first flow path (68) is defined between the fuel distribution manifold (60) and a first combustion sector (60). A second flow path (72) is defined between the fuel distribution manifold (60) and a second combustion sector (74).",
  "title": "A Fuel Supply System for Supplying Fuel to a Combustion Section of a Gas Turbine"
}