{
  "$type": "site.standard.document",
  "description": "A bearing compartment of a gas turbine engine includes a case element (68), a towershaft bearing (64) located in the case element (68) and supportive of a towershaft (60), and a shaft bearing (66) located in the case element (68) and supportive of an engine shaft (50). An integral gear support (70)…",
  "path": "/patents/1412787",
  "publishedAt": "2024-12-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/162",
    "RTX CORP [US]"
  ],
  "textContent": "A bearing compartment of a gas turbine engine includes a case element (68), a towershaft bearing (64) located in the case element (68) and supportive of a towershaft (60), and a shaft bearing (66) located in the case element (68) and supportive of an engine shaft (50). An integral gear support (70) and bearing damper pedestal (82), includes a support base (76) secured to the case element (68), and a gear support arm (80) extending from the support base (76) to the towershaft bearing (64). The gear support arm (80) is supportive of the towershaft bearing (64). A bearing damper pedestal (82) extends from the support base (76) to the shaft bearing (66) and is located radially outboard of a bearing outer race (84) of the shaft bearing (66).",
  "title": "INTEGRAL GEAR SUPPORT AND BEARING DAMPER PEDESTAL OF A GAS TURBINE ENGINE"
}