{
  "$type": "site.standard.document",
  "description": "Embodiments of a gas turbine engine actuation system are provided, as are embodiments of a high temperature actuator (64, 68, 72, 80) and methods for the manufacture thereof (100). In one embodiment, the actuation system includes an actuated component and a high temperature actuator, which has a…",
  "path": "/patents/969962",
  "publishedAt": "2014-09-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/162",
    "HONEYWELL INT INC [US]"
  ],
  "textContent": "Embodiments of a gas turbine engine actuation system are provided, as are embodiments of a high temperature actuator (64, 68, 72, 80) and methods for the manufacture thereof (100). In one embodiment, the actuation system includes an actuated component and a high temperature actuator, which has a rotor (84) mechanically linked to the actuated component and a stator (82) surrounding at least a portion of the rotor. The stator includes, in turn, a coil support structure (104) having a plurality of spokes (110) extending radially therefrom. A plurality of pre-formed electromagnetic coils (120) is circumferentially distributed about the coil support structure. Each of the plurality of pre-formed electromagnetic coils is inserted over at least one of the plurality of spokes in a radial direction. The stator further includes an inorganic dielectric material (124) in which each of the plurality of pre-formed electromagnetic coils is at least partially embedded.",
  "title": "Gas turbine engine actuation systems including high temperature actuators and methods for the manufacture thereof"
}