{
  "$type": "site.standard.document",
  "description": "A unitary fan inlet case and bearing support structure (140) for a gas turbine engine includes an annular body (100) having a radially inward ring (120) connected to a radially outward ring (110) via a plurality of struts (130). A platform protrudes radially inward from the radially inward ring…",
  "path": "/patents/1402742",
  "publishedAt": "2024-11-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/162",
    "RTX CORP [US]"
  ],
  "textContent": "A unitary fan inlet case and bearing support structure (140) for a gas turbine engine includes an annular body (100) having a radially inward ring (120) connected to a radially outward ring (110) via a plurality of struts (130). A platform protrudes radially inward from the radially inward ring. The platform includes a radially outward facing surface and a radially inward facing surface. The annular body is a single unitary structure.",
  "title": "INTEGRATED FAN CASE AND BEARING SUPPORT FOR A GAS TURBINE ENGINE AND METHOD"
}