{
  "$type": "site.standard.document",
  "description": "Assemblies and methods for directing a flow of air (56) through a compressor section (14) of a gas turbine engine (10) are disclosed. A method includes receiving the flow of air (56) over a strut (42A) extending radially across a substantially annular gas path (22) of the gas turbine engine (10)…",
  "path": "/patents/1421192",
  "publishedAt": "2024-03-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/162",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "Assemblies and methods for directing a flow of air (56) through a compressor section (14) of a gas turbine engine (10) are disclosed. A method includes receiving the flow of air (56) over a strut (42A) extending radially across a substantially annular gas path (22) of the gas turbine engine (10), and at least partially confining and modifying a strut wake (68) generated in the flow of air (56) by the strut (42A) using one or more variable orientation guide vanes (24).",
  "title": "ASSEMBLY FOR A COMPRESSOR SECTION OF A GAS TURBINE ENGINE"
}