Method for detecting the tip clearance of dynamic labyrinth tooth blades of an aircraft engine

IT202500022201A1Pending Publication Date: 2026-10-03HANGZHOU DIANZI UNIV
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Patent Information

Application Number
IT102025000022201
Authority / Receiving Office
IT · IT
Patent Type
Applications
Current Assignee / Owner
Priority Date
2025-04-03
Filing Date
2025-08-29
Publication Date
2026-10-03
Estimated Expiration
2035-08-29
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