{
  "$type": "site.standard.document",
  "description": "The present application and the resultant patent provide a gas turbine engine (100). The gas turbine engine (100) may include a compressor (110) for compressing a flow of air (120), a combustor (130) for combusting the flow of air (120) and a flow of fuel (140)to create a flow of combustion gases…",
  "path": "/patents/996066",
  "publishedAt": "2012-11-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D21/02",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "The present application and the resultant patent provide a gas turbine engine (100). The gas turbine engine (100) may include a compressor (110) for compressing a flow of air (120), a combustor (130) for combusting the flow of air (120) and a flow of fuel (140)to create a flow of combustion gases (150), a turbine (160) driven by the flow of combustion gases (150), a rotor (180) driven by the turbine and driving the compressor (110), a rotor speed sensor, (220) and a gas turbine shut down controller. The gas turbine shut down controller varies the flow of fuel (140) to the combustor (130) based upon a rotational speed of the rotor (180) as determined by a dynamic target trajectory schedule.",
  "title": "Systems and methods for optimized gas turbine shutdown"
}