3 Patents
- US121737242024Method for Configuring a Leading Edge of a Compressor Stator Platform and the Corresponding Stator Platform
AECC COMMERCIAL AIRCRAFT ENGINE CO., Ltd.
0 cites - US120550482024Method for Rotor Blade Tip Clearance Control and Rotor Blade Manufactured by the Method
AECC COMMERCIAL AIRCRAFT ENGINE CO., Ltd.
0 cites - US120441332024Aeroengine Compressor and Position Holding Structure of Adjustable Stator Vane
AECC COMMERCIAL AIRCRAFT ENGINE CO., Ltd.
0 cites