{
  "$type": "site.standard.document",
  "description": "A valve assembly for an engine (113), the valve assembly (201) can include a housing; an in-flow port (219) configured for connection with a drain line (203); a first out-flow port (221) configured for connection with a fuel line (205); a second out-flow port (223) configured for connection with a…",
  "path": "/patents/968406",
  "publishedAt": "2014-10-22T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/002",
    "BELL HELICOPTER TEXTRON INC [US]"
  ],
  "textContent": "A valve assembly for an engine (113), the valve assembly (201) can include a housing; an in-flow port (219) configured for connection with a drain line (203); a first out-flow port (221) configured for connection with a fuel line (205); a second out-flow port (223) configured for connection with a disposal line (213); and a passageway (215) that is rotatable with a handle (207), the passageway (215) being operable to redirect a flow of a fluid between the fuel line (205) and the disposal line (213). The handle (203) is configured to impede an attachment of the fluid source to a water wash connection (209) when the passageway (215) is in a position to direct the flow of the fluid from the drain line (203) to the fuel line (205).",
  "title": "Fuel drain valve for a turbine engine"
}