{
  "$type": "site.standard.document",
  "description": "A turbomachine assembly includes a first combustor (30) configured to combust fuel and compressed air and a second combustor (32) configured to combust fuel and compressed air. Flow moves through the first combustor (30) in a first direction and flow moves though the second combustor (32) in a…",
  "path": "/patents/995157",
  "publishedAt": "2012-12-12T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/145",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A turbomachine assembly includes a first combustor (30) configured to combust fuel and compressed air and a second combustor (32) configured to combust fuel and compressed air. Flow moves through the first combustor (30) in a first direction and flow moves though the second combustor (32) in a second direction different than the first direction. The first combustor (30) is axially spaced from the second combustor (32). A corresponding operating method is also provided.",
  "title": "Turbomachine assembly with combustors having different flow directions and corresponding operating method"
}