{
  "abstract": "A nozzle segment separation tool for use with a pair of adjacent nozzle segments in a casing of a turbine. The nozzle segment separation tool may include a pair of support plates, a hydraulic cylinder positioned within the pair of support plates, a pushing bar attached to the hydraulic cylinder, a nozzle catch plate positioned within the pair of support plates, and a blocking pin inserted through the casing. The blocking pin forces the nozzle catch plate to engage a first nozzle segment of the pair of adjacent nozzle segments and blocks movement of the pushing bar such that the nozzle catch plate separates the pair of adjacent nozzle segments.",
  "assignees": [
    "GE INFRASTRUCTURE TECHNOLOGY LLC"
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  "authors": [
    "KORUS MATEUSZ",
    "SAJDAK LUKASZ",
    "SKALSKI RAFAL",
    "WOJCIECHOWSKI PIOTR"
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    "name": "Creative Commons Attribution 4.0 International",
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  "published_at": "2026-09-15T19:11:58.675056Z",
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  "source_date": "2026-03-05",
  "source_id": "US-2026061531-A1",
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  "supersedes": null,
  "title": "Separation tool and method for nozzle segments of gas turbines",
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