{
  "$type": "site.standard.document",
  "description": "A mechanical drive system for an accessory gearbox (24) of a gas turbine engine is provided. The gas turbine engine includes a high-pressure drive shaft (12) and a low-pressure drive shaft (14). The mechanical drive system includes a tower shaft (32) and a lay shaft (38). The tower shaft (38) is…",
  "path": "/patents/1074151",
  "publishedAt": "2005-09-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/32",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A mechanical drive system for an accessory gearbox (24) of a gas turbine engine is provided. The gas turbine engine includes a high-pressure drive shaft (12) and a low-pressure drive shaft (14). The mechanical drive system includes a tower shaft (32) and a lay shaft (38). The tower shaft (38) is connected by a first gear arrangement (34) to the low-pressure drive shaft (14) of the gas turbine engine. The lay shaft (38) is connected by a second gear arrangement (36) to the tower shaft (32), and connected to the accessory gearbox (24).",
  "title": "Mechanical drive system for an accessory gearbox"
}