{
  "$type": "site.standard.document",
  "description": "The bypass duct has support struts, which are formed as guide vanes-support struts (3) with bigger thickness and chord length than the guide vanes (2) in an aligned aerodynamic form. A flow channel (4) existing between a suction side (7) of the guide vane-support strut and a guide vane (2.1)…",
  "path": "/patents/1009711",
  "publishedAt": "2011-08-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D5/141",
    "ROLLS ROYCE DEUTSCHLAND [DE]"
  ],
  "textContent": "The bypass duct has support struts, which are formed as guide vanes-support struts (3) with bigger thickness and chord length than the guide vanes (2) in an aligned aerodynamic form. A flow channel (4) existing between a suction side (7) of the guide vane-support strut and a guide vane (2.1) adjacent to the suction side is extended by a guide vane modifying in the geometry against other guide vanes depending on the respective formation of the guide vane-support strut for reducing the peak pressures of a circumferential pressure field.",
  "title": "Bypass duct with guide vane ring in a turbofan engine"
}