{
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  "description": "An engine accessory system (62) for a gas turbine engine (10) includes a first accessory component (AC) mountable to an accessory gearbox (60) along a first accessory axis (b) transverse to a layshaft axis of rotation (L). A second accessory component (AC) is mountable along a second accessory axis…",
  "path": "/patents/1007527",
  "publishedAt": "2011-11-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/32",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "An engine accessory system (62) for a gas turbine engine (10) includes a first accessory component (AC) mountable to an accessory gearbox (60) along a first accessory axis (b) transverse to a layshaft axis of rotation (L). A second accessory component (AC) is mountable along a second accessory axis (c) transverse to the layshaft axis of rotation (L), the first and second accessory axis (b, c) defining a V-orientation.",
  "title": "Accessory gearbox with internal layshaft"
}