{
  "$type": "site.standard.document",
  "description": "A method and system for providing fuel to primary, 30, and secondary, 32, fuel nozzles in a gas turbine engine fuel system, 12, comprises generating a fuel flow and routing primary fuel from the fuel flow to a primary fuel nozzle, 30. Backpressure on the fuel flow is maintained using a valve. The…",
  "path": "/patents/983902",
  "publishedAt": "2013-10-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/232",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "A method and system for providing fuel to primary, 30, and secondary, 32, fuel nozzles in a gas turbine engine fuel system, 12, comprises generating a fuel flow and routing primary fuel from the fuel flow to a primary fuel nozzle, 30. Backpressure on the fuel flow is maintained using a valve. The valve is opened at increased fuel flow to route secondary fuel from the fuel flow to a secondary fuel nozzle, 32. The valve is progressively opened under increasing fuel flows to reduce a pressure drop across the valve produced by the secondary fuel.",
  "title": "Passive equalization flow divider valve"
}