{
  "$type": "site.standard.document",
  "description": "The aircraft powerplant (22) includes an injector (74) and a fuel system (100) configured to deliver fuel to the injector (74). The fuel system (100) includes a first tank (114), a first circuit (106) and a second circuit (108) arranged in parallel with the first circuit (106) between the first…",
  "path": "/patents/1388803",
  "publishedAt": "2026-04-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D37/06",
    "RTX CORP [US]"
  ],
  "textContent": "The aircraft powerplant (22) includes an injector (74) and a fuel system (100) configured to deliver fuel to the injector (74). The fuel system (100) includes a first tank (114), a first circuit (106) and a second circuit (108) arranged in parallel with the first circuit (106) between the first tank (114) and the injector (74). The second circuit (108) includes a second tank. The fuel is directed from the first tank (114) to the injector (74) during a first mode through the first circuit (106) and independent of the second circuit (108). The fuel is directed from the second tank to the injector (74) during a second mode through the second circuit (108) and independent of the first circuit (106).",
  "title": "AIRCRAFT FUEL SYSTEM WITH REMOVABLE FUEL TANK"
}