{
  "$type": "site.standard.document",
  "description": "A transition piece (20) support for a turbomachine includes one or more support arms (40) extending across a diffuser flowpath (42) to the transition piece (20). The one or more support arms (40) include a streamwise surface (46) and a crosswise surface (48). A streamwise extent (50) of the…",
  "path": "/patents/1007938",
  "publishedAt": "2011-11-09T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D9/023",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A transition piece (20) support for a turbomachine includes one or more support arms (40) extending across a diffuser flowpath (42) to the transition piece (20). The one or more support arms (40) include a streamwise surface (46) and a crosswise surface (48). A streamwise extent (50) of the streamwise surface (46) is greater than a crosswise extent (52) of the crosswise surface (48) to reduce flow anomalies in a flow (32) of fluid across the one or more support arms (40). A turbomachine includes a combustor (14), a diffuser (34), a transition piece (20) operably connected to the combustor (14) and a transition piece support including one or more support arms (40) extending across a flow (32) of fluid to the transition piece (20). The support arms (40) include a streamwise surface (46) and a crosswise surface (48). A streamwise extent (50) of the streamwise surface (46) is greater than a crosswise extent (52) of the crosswise surface (48) to reduce flow anomalies in a flow (32) of fluid across the one or more support arms (40).",
  "title": "Reduced pressure loss transition support"
}