{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
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  "description": "A method for constructing a nozzle ring 40 for a turbocharger turbine nozzle 28 includes the steps of: providing a nozzle ring 42 in the form of an annular flat disk, the nozzle ring having a first face and an opposite second face; forming a plurality of circumferentially spaced circular bores 43…",
  "path": "/patents/1397406",
  "publishedAt": "2026-04-15T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B23P15/006",
    "GARRETT TRANSPORTATION I INC [US]"
  ],
  "textContent": "A method for constructing a nozzle ring 40 for a turbocharger turbine nozzle 28 includes the steps of: providing a nozzle ring 42 in the form of an annular flat disk, the nozzle ring having a first face and an opposite second face; forming a plurality of circumferentially spaced circular bores 43 extending through the nozzle ring 42 from the first face to the second face; providing a plurality of vanes 44, each vane having a circular vane shaft 46 extending from one end of the vane; inserting the vane shafts 46 respectively into the bores 43 in the nozzle ring from said first face thereof and orienting each vane 44 to achieve a desired setting angle for the vane; and rigidly affixing the vane shafts 46 to the nozzle ring 42 to fix the vanes at the desired setting angles.",
  "title": "METHOD FOR CONSTRUCTING A FIXED-VANE RING FOR A NOZZLE OF A TURBOCHARGER TURBINE"
}