{
  "$type": "site.standard.document",
  "description": "A turbine engine comprises a case (42)and a centerbody (40) within the case (42) and separated from the case (42) by a core flowpath. A circumferential array of augmentor vanes (50) extends between the centerbody (40) and case (42). A circumferential array of resonators (80) is arranged within the…",
  "path": "/patents/999715",
  "publishedAt": "2012-08-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/30",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A turbine engine comprises a case (42)and a centerbody (40) within the case (42) and separated from the case (42) by a core flowpath. A circumferential array of augmentor vanes (50) extends between the centerbody (40) and case (42). A circumferential array of resonators (80) is arranged within the centerbody (40) each having a port open to the core flowpath. Each resonator (80) comprises a resonator body having a neck (84) and an enlarged main body (86) inboard of the neck (84). The main body (86) has a convex first circumferential side and a concave second circumferential side converging inboard, each first circumferential side nested with the second adjacent side of a first adjacent one of the resonators (80) and each second circumferential side nested with the first adjacent side of a second adjacent one of the resonators (80).",
  "title": "Turbine engine tailcone resonator"
}