{
  "$type": "site.standard.document",
  "description": "A fuel system (200) for a gas turbine engine (100) of an aircraft, including a main inlet feed conduit (122) fluidly connected to a primary manifold feed conduit (110a) and a secondary manifold feed conduit (110a, 110b). A primary manifold (110) fluidly connects the primary manifold feed conduit…",
  "path": "/patents/1402232",
  "publishedAt": "2025-07-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/22",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A fuel system (200) for a gas turbine engine (100) of an aircraft, including a main inlet feed conduit (122) fluidly connected to a primary manifold feed conduit (110a) and a secondary manifold feed conduit (110a, 110b). A primary manifold (110) fluidly connects the primary manifold feed conduit (110a) to a plurality of primary fuel injectors (120a), and a secondary manifold (111) fluidly connects the secondary manifold feed conduit (110b) to a plurality of secondary fuel injectors (120b).",
  "title": "PULSE WIDTH MODULATION DRIVE FOR STAGED FUEL MANIFOLDS"
}