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19277730 · GAS TURBINE ENGINE HAVING A THRUST REVERSER SYSTEM WITH DRAG LINK CONNECTORS AT INTER-COMPRESSOR FRAME STRUCTURE

Filed 2025-07-23 · Granted · Patent 12553403 (2026-02-17) The official file ↗The patent and its PDF ↗ · Art unit 3741 · Examiner Kyle Robert Thomas Typical · CPC F02K 1/72 · General Electric Company · VENABLE LLP (GE Aviation)

Office actions
0
first was Notice of allowance
RCEs
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no appeal
To first action
2.5 mo
to disposition 6.9 mo
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