{
  "$type": "site.standard.document",
  "description": "A combustor (100) includes a liner (102) defining a combustion chamber (105), and receiving an air and fuel mixing body (104). The mixing body (104) includes a forward face (114) facing into the combustion chamber (105). A plurality of circumferentially spaced columns (200-220) about a central axis…",
  "path": "/patents/1391071",
  "publishedAt": "2026-04-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F23D14/24",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A combustor (100) includes a liner (102) defining a combustion chamber (105), and receiving an air and fuel mixing body (104). The mixing body (104) includes a forward face (114) facing into the combustion chamber (105). A plurality of circumferentially spaced columns (200-220) about a central axis (Y) of the combustor (100) each have at least two fuel supply passages (124, 130) and two air supply passages (122) extending to the forward face (114). At least one of the two air supply passages (122) and one of the fuel supply passages (124, 130) extend along a direction with a circumferentially extending component in a first circumferential direction. The other of the two air supply passages (122) and the fuel supply passages (124, 130) extend with a circumferential component in a second opposed circumferential direction. A gas turbine engine (20) is also disclosed.",
  "title": "COMBUSTOR WITH TANGENTIAL FUEL AND AIR FLOW"
}