{
  "$type": "site.standard.document",
  "description": "A support assembly (100) for a turbine system (10) is disclosed. The support assembly (100) includes a transition duct (50) extending between a fuel nozzle and a turbine section. The transition duct (50) has an inlet (52), an outlet (54), and a passage (56) extending between the inlet (52) and the…",
  "path": "/patents/994045",
  "publishedAt": "2013-01-09T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D9/023",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A support assembly (100) for a turbine system (10) is disclosed. The support assembly (100) includes a transition duct (50) extending between a fuel nozzle and a turbine section. The transition duct (50) has an inlet (52), an outlet (54), and a passage (56) extending between the inlet (52) and the outlet (54) and defining a longitudinal axis (90), a radial axis (94), and a tangential axis (92). The outlet (54) of the transition duct (50) is offset from the inlet (52) along the longitudinal axis. The support assembly (100) further includes a plurality of protrusions (102) extending from the transition duct (50). The plurality of protrusions (102) are configured to allow movement of the transition duct (50) about at least one axis. A corresponding turbine system is also provided.",
  "title": "Support assembly for a turbine system and corresponding turbine system"
}