{
  "$type": "site.standard.document",
  "description": "The present application provides a clocked combustor can array (370) for coherence reduction in a gas turbine engine having a number of combustor cans (380) positioned in a circumferential array (300). A first set (375) of the plurality of combustor cans (380) comprises a first orientation (385)…",
  "path": "/patents/974620",
  "publishedAt": "2014-05-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/24",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "The present application provides a clocked combustor can array (370) for coherence reduction in a gas turbine engine having a number of combustor cans (380) positioned in a circumferential array (300). A first set (375) of the plurality of combustor cans (380) comprises a first orientation (385); and a second set (390) of the plurality of combustor cans (380) comprises a second orientation (400). The first orientation (385) may be in a clocked position of about ninety degrees from the second orientation (400). The combustor cans (380) comprise oval or elliptical head ends and a plurality of fuel nozzles with vanes optionally oriented clockwise and counter-clock wise.",
  "title": "Can-annular combustor array for a gas turbine having oval or elliptical can heads twisted among themselves"
}