{
  "$type": "site.standard.document",
  "description": "The method involves injecting compressed air in a fuel supply circuit of a fuel injector (7), when a turbine engine (1) is stopped and fuel supply to fuel injection heads of the injector is stopped. The compressed air is injected directly and uniquely in each non-supplied fuel injection head in the…",
  "path": "/patents/1071789",
  "publishedAt": "2005-12-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/232",
    "SNECMA [FR]"
  ],
  "textContent": "The method involves injecting compressed air in a fuel supply circuit of a fuel injector (7), when a turbine engine (1) is stopped and fuel supply to fuel injection heads of the injector is stopped. The compressed air is injected directly and uniquely in each non-supplied fuel injection head in the downstream of check valves of the injection heads and disposed on inner fuel pipes of the injector. An independent claim is also included for a turbine engine comprising a system for protecting a fuel injector.",
  "title": "Method and system for the protection of fuel nozzles in a gas turbine engine"
}