{
  "$type": "site.standard.document",
  "description": "In accordance with at least one aspect of the present disclosure, there is provided a fuel system (100) of an aircraft engine (10), comprising: a fuel conduit interface (102) connecting a fuel conduit (104) to a component of the fuel system (100); and a sweep line structure (107, 207, 121). The…",
  "path": "/patents/1403735",
  "publishedAt": "2025-07-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D37/32",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "In accordance with at least one aspect of the present disclosure, there is provided a fuel system (100) of an aircraft engine (10), comprising: a fuel conduit interface (102) connecting a fuel conduit (104) to a component of the fuel system (100); and a sweep line structure (107, 207, 121). The sweep line structure (107, 207, 121) includes an inner surface (108) facing toward, extending around, and defining a cavity (110) around the fuel conduit interface (102), and an outer surface (112) opposite the inner surface (108), the cavity (110) being fluidly sealed relative to the outer surface (112).",
  "title": "SWEEP FLOW STRUCTURES FOR FUEL SYSTEMS"
}