{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
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  "description": "An assembly (66) is provided for an aircraft propulsion system (20). This assembly (66) includes a first actuator (68), a second actuator (68) and a linkage system (70, 72). The linkage system (70, 72) is configured to transfer torque between the first actuator (68) and the second actuator (68)…",
  "path": "/patents/1413115",
  "publishedAt": "2025-07-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/72",
    "ROHR INC [US]"
  ],
  "textContent": "An assembly (66) is provided for an aircraft propulsion system (20). This assembly (66) includes a first actuator (68), a second actuator (68) and a linkage system (70, 72). The linkage system (70, 72) is configured to transfer torque between the first actuator (68) and the second actuator (68). The linkage system (70, 72) includes a first linkage shaft (90), a second linkage shaft (90) and a gearbox (92). The first linkage shaft (90) has a first centerline (94). The second linkage shaft (90) has a second centerline (94) offset from the first centerline (94). The gearbox (92) is coupled to and is between the first linkage shaft (90) and the second linkage shaft (90).",
  "title": "ACTUATION SYSTEM FOR A THRUST REVERSER OF AN AIRCRAFT PROPULSION SYSTEM"
}