{
  "$type": "site.standard.document",
  "description": "Various methods and systems are provided for adjusting a turbine boost control actuator based on a single common reference value. In one example, a method for an engine (104) includes adjusting a turbine boost control actuator to control an intake manifold pressure to a limit, the limit based at…",
  "path": "/patents/944366",
  "publishedAt": "2016-04-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02B37/18",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "Various methods and systems are provided for adjusting a turbine boost control actuator based on a single common reference value. In one example, a method for an engine (104) includes adjusting a turbine boost control actuator to control an intake manifold pressure to a limit, the limit based at least in part on one or more of peak cylinder pressure, turbine speed, and a pressure difference across a turbine (125).",
  "title": "METHOD AND SYSTEMS FOR ADJUSTING A TURBINE BYPASS VALVE"
}