{
  "$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 has an inlet (52), an outlet (54), and a passage (56) extending between the inlet (52) and the…",
  "path": "/patents/994051",
  "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 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 (90). The support assembly (100) further includes an annular contact member (102) extending from the transition duct (50). The contact member (102) is 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"
}