{
  "$type": "site.standard.document",
  "description": "An example turbomachine geared architecture support assembly (70; 100) includes a subpart having a more compliant portion (82; 108) and a less compliant portion (78; 104). The less compliant portion (78; 104) includes a stop (88; 108) that limits axial movement of a geared architecture (48) within…",
  "path": "/patents/1424646",
  "publishedAt": "2023-08-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D21/045",
    "RAYTHEON TECH CORP [US]"
  ],
  "textContent": "An example turbomachine geared architecture support assembly (70; 100) includes a subpart having a more compliant portion (82; 108) and a less compliant portion (78; 104). The less compliant portion (78; 104) includes a stop (88; 108) that limits axial movement of a geared architecture (48) within a turbomachine (20).",
  "title": "TURBOMACHINE GEARED ARCHITECTURE SUPPORT ASSEMBLY"
}