4 Patents
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- US119058522024Intermediate Element for a Blade/rotor Disc Connection in a Rotor of a Turbomachine, Associated Rotor for a Turbomachine, and Turbomachine
MTU AERO ENGINES AG
0 cites - US117539502023Rotor Blade with Blade Root Contour Having a Straight Portion Provided in a Concave Contour Portion
MTU AERO ENGINES AG
0 cites