{
  "$type": "site.standard.document",
  "description": "The operating method has a bypass flow (B) provided across the compressor (14) of the turbocharger, connected to the air intake channel of the IC engine, when a reduced pressure is obtained between the compressor and the throttle plate (36), relative to the pressure in the air intake line (26). The…",
  "path": "/patents/1088710",
  "publishedAt": "2004-03-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02B37/16",
    "ABB TURBO SYSTEMS AG [CH]"
  ],
  "textContent": "The operating method has a bypass flow (B) provided across the compressor (14) of the turbocharger, connected to the air intake channel of the IC engine, when a reduced pressure is obtained between the compressor and the throttle plate (36), relative to the pressure in the air intake line (26). The bypass flow is re-combined with the main flow (A) ahead of the throttle plate. Also included are Independent claims for the following; (a) an operating device for an exhaust gas turbocharger for an IC engine; (b) an exhaust gas turbocharger for an IC engine; (c) an IC engine provided with an exhaust gas turbocharger",
  "title": "Method and device for operating a turbocharger"
}