{
  "$type": "site.standard.document",
  "description": "A variable guide vane (VGV) assembly (40) has: vanes (42) distributed about a central axis (11), each of the vanes (42) having an airfoil (42a) extending between first and second stems (42d, 42f); and a bushing ring (44) supporting the first stems (42d) of the vanes (42), the bushing ring (44)…",
  "path": "/patents/1410455",
  "publishedAt": "2023-06-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/162",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A variable guide vane (VGV) assembly (40) has: vanes (42) distributed about a central axis (11), each of the vanes (42) having an airfoil (42a) extending between first and second stems (42d, 42f); and a bushing ring (44) supporting the first stems (42d) of the vanes (42), the bushing ring (44) defining circumferentially distributed pockets (44e) receiving the first stems (42d) of the vanes (42), the bushing ring (44) having a first ring body (45) and a second ring body (47), the second ring body (47) defining at least one tab (47a) axially overlapping at least a portion of the first ring body (45) and defining a contact plane (P) therebetween, and at least one locking member (LM) extending radially through the contact plane (P) to removably secure the first ring body (45) and the second ring body (47) together.",
  "title": "VARIABLE GUIDE VANE ASSEMBLY FOR A GAS TURBINE ENGINE AND GAS TURBINE ENGINE"
}