{
  "$type": "site.standard.document",
  "description": "GAS TURBINE ENGINE AND MOUNT ASSEMBLY THEREFOR [0002] The gas turbine engine can have a casing (28), a rotor rotatable around a rotation axis (11) relative the casing (28), the casing (28) extending along and around the rotation axis (11), a first component (50) mounted externally to the casing…",
  "path": "/patents/1406241",
  "publishedAt": "2024-11-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/402",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "GAS TURBINE ENGINE AND MOUNT ASSEMBLY THEREFOR [0002] The gas turbine engine can have a casing (28), a rotor rotatable around a rotation axis (11) relative the casing (28), the casing (28) extending along and around the rotation axis (11), a first component (50) mounted externally to the casing (28) by a first mount (52), the first mount (52) defining a torsion axis (54) extending along a vertical radial direction (66) normal the rotation axis (11), the first component (50) having a center of gravity located on a first side relative the torsion axis (54), a second component (36) mounted externally to the casing on the second side, extending along the vertical radial direction from a bottom portion to a top portion, a second mount structurally connecting the bottom portion to the casing (28), and a structure (62) connecting the top portion to the first component on the second side relative the torsion axis (54).",
  "title": "GAS TURBINE ENGINE AND MOUNT ASSEMBLY THEREFOR"
}