{
  "$type": "site.standard.document",
  "description": "An exhaust mixer (32) for a gas turbine engine has a plurality of circumferentially distributed alternating inner and outer lobes (42,44), and a plurality of aerodynamic struts (50) positioned and oriented between adjacent inner lobes (42) in the core flow passage. The struts (50) are configured…",
  "path": "/patents/970018",
  "publishedAt": "2014-09-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/46",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "An exhaust mixer (32) for a gas turbine engine has a plurality of circumferentially distributed alternating inner and outer lobes (42,44), and a plurality of aerodynamic struts (50) positioned and oriented between adjacent inner lobes (42) in the core flow passage. The struts (50) are configured for diverting a portion of the core flow radially outwardly in troughs formed by the outer lobes (44) on the core flow side of the mixer (32).",
  "title": "Gas turbine engine exhaust mixer with aerodynamic struts"
}