{
"$type": "site.standard.document",
"description": "A multiple fuel delivery system (100) for use with a gas turbine engine includes a first fuel tank (110) with a first fuel (120) therein, a second fuel tank (170) with a second fuel (180) therein, a mixing chamber (130), and a flow divider (250) downstream of the mixing chamber. The first fuel tankā¦",
"path": "/patents/976312",
"publishedAt": "2014-04-09T00:00:00.000Z",
"site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
"tags": [
"F02C3/24",
"GEN ELECTRIC [US]"
],
"textContent": "A multiple fuel delivery system (100) for use with a gas turbine engine includes a first fuel tank (110) with a first fuel (120) therein, a second fuel tank (170) with a second fuel (180) therein, a mixing chamber (130), and a flow divider (250) downstream of the mixing chamber. The first fuel tank (110) may be in communication with the mixing chamber (130) via a first fuel pump (140) and the second fuel tank (170) may be in communication with the mixing chamber (130) via a second fuel pump (190).",
"title": "Gas turbine engine with a multiple fuel delivery system"
}