3 Patents
- 0 cites
- US124804092025Blade Platform, Blade Ring, Impeller Disk and Gas Turbine Engine
AECC Commercial Aircraft Engine Co., Ltd.
0 cites - US121737242024Method for Configuring a Leading Edge of a Compressor Stator Platform and the Corresponding Stator Platform
AECC COMMERCIAL AIRCRAFT ENGINE CO., Ltd.
0 cites