GE Avio was granted a patent for a turbine-blade damper assembly.

{
  "signal_id": "27ef87ab-a89e-5901-b503-5c87df899df5",
  "signal_type": "patents-company",
  "signal_subtype": "patentGrant",
  "detected_at": "2026-09-30T17:03:48+00:00",
  "company": {
    "name": "GE Aerospace",
    "domain": "geaerospace.com"
  },
  "data": {
    "cpc": [
      {
        "code": "F01D 5/26"
      },
      {
        "code": "F01D 5/16"
      },
      {
        "code": "F01D 25/06"
      },
      {
        "code": "F05D 2240/30"
      },
      {
        "code": "F05D 2260/96"
      }
    ],
    "tags": [
      "Intellectual Property",
      "Research & Development",
      "Engineering",
      "Machinery"
    ],
    "detail": "In September 2026 GE Avio patented a shaped damping component for reducing blade vibration in gas-turbine engines.",
    "summary": "GE Avio was granted a patent for a turbine-blade damper assembly.",
    "event_at": "2026-09-29",
    "inventors": [
      {
        "name": "Antonio Giuseppe D'Ettole",
        "status": "resolved",
        "is_primary": true,
        "linkedin_url": "https://www.linkedin.com/in/agdettole"
      },
      {
        "name": "Gianmaria Sartor",
        "status": "resolved",
        "is_primary": false,
        "linkedin_url": "https://www.linkedin.com/in/gianmariasartor"
      },
      {
        "name": "Veronica Iannotti",
        "status": "resolved",
        "is_primary": false,
        "linkedin_url": "https://www.linkedin.com/in/veronica-iannotti-5b8299159"
      },
      {
        "name": "Emanuele Rosso",
        "status": "unresolved",
        "is_primary": false
      }
    ],
    "event_kind": "grant_date",
    "grant_date": "2026-09-29",
    "source_url": "https://patents.google.com/patent/US12747668",
    "cpc_primary": {
      "code": "F01D 5/26"
    },
    "patent_title": "Damper assembly",
    "patent_number": "US12747668",
    "uspto_assignee": "GE Avio S.R.L.",
    "patent_abstract": "A damper assembly for a blade, the damper assembly defining a longitudinal direction, a lateral direction, and a vertical direction and including a base extending in the longitudinal direction from a first end to a second end, the base including a forward face, a rear face, and a top face, a first contact region defined on the top face between the first end and the second end, the first contact region defining a first curved surface, and a second contact region defined on the rear face between the first end and the second end, the second contact region defining a second curved surface. The first curved surface abuts the second curved surface at a common position in the longitudinal direction.",
    "precision_class": "structural",
    "invention_explanation": "A contoured support placed against a turbine blade to absorb movement and limit damaging vibration during engine operation.",
    "technologies_mentioned": [
      "turbine blades",
      "vibration damping",
      "gas-turbine engines"
    ]
  }
}

curl https://signals.autobound.ai/v1/signals/27ef87ab-a89e-5901-b503-5c87df899df5 \
  -H "X-API-KEY: $AUTOBOUND_API_KEY"

curl -X POST https://signals.autobound.ai/v1/companies/enrich \
  -H "X-API-KEY: $AUTOBOUND_API_KEY" \
  -H "Content-Type: application/json" \
  -d '{"domain":"geaerospace.com","limit":20}'