Gas Turbine Engine Architecture With Low Pressure Compressor Hub Between High And Low Rotor Thrust Bearings

Patent No. EP2597292 (titled "Gas Turbine Engine Architecture With Low Pressure Compressor Hub Between High And Low Rotor Thrust Bearings") was filed by Raytheon on Nov 15, 2012. The application was issued on Mar 19, 2025.

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SAFRAN AIRCRAFT ENGINESMay 11, 2021REGIMBEAU

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EP2597292

RAYTHEON
Application Number
EP12192792A
Filing Date
Nov 15, 2012
Status
Patent Maintained As Amended
Feb 14, 2025
Publication Date
Mar 19, 2025