{
  "$type": "site.standard.document",
  "description": "According to one aspect of the invention, an ice separating apparatus (106;200) for a gas turbine engine includes a can (202) having a first end (218) and a tangential inlet (204) proximate the first end (218) of the can (202) to receive a fluid flow (210) within the can (202), wherein the fluid…",
  "path": "/patents/985657",
  "publishedAt": "2013-03-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B01D21/2411",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "According to one aspect of the invention, an ice separating apparatus (106;200) for a gas turbine engine includes a can (202) having a first end (218) and a tangential inlet (204) proximate the first end (218) of the can (202) to receive a fluid flow (210) within the can (202), wherein the fluid flow (210) includes fuel and ice. The apparatus (106;200) also includes a first conduit (206) within the can (202) to receive a separated fuel flow (230) proximate a second end (220) of the can (202), wherein the fluid flow separates ice from fuel to form the separated fuel flow (230).",
  "title": "Apparatus and method for separating ice from fuel in a gas turbine engine"
}