Inventor
BRETTSCHNEIDER MARKUS
DE15 patents
Patents
15 patentsUS10458248B2Oct 29, 2019
Blade channel, blade cascade and turbomachine
MTU Aero Engines AG5 citations71
US10436044B2Oct 8, 2019
Guide vane segment for a turbomachine
MTU Aero Engines AG3 citations71
US9470094B2Oct 18, 2016
Blade cascade with side wall contours and continuous-flow machine
MTU Aero Engines AG4 citations71
US10934849B2Mar 2, 2021
Endwall contouring for a turbomachine
MTU Aero Engines AG2 citations70
US10704393B2Jul 7, 2020
Contouring of an airfoil array platform
MTU Aero Engines AG2 citations70
US12140041B2Nov 12, 2024
Stator vane for a turbomachine
MTU Aero Engines AG1 citations61
US10876410B2Dec 29, 2020
Turbomachine airfoil array
MTU Aero Engines AG1 citations60
US10753206B2Aug 25, 2020
Contouring a blade/vane cascade stage
MTU Aero Engines AG1 citations60
US10648339B2May 12, 2020
Contouring a blade/vane cascade stage
MTU Aero Engines AG1 citations60
US12305538B2May 20, 2025
Guide vane ring and rotor blade ring for a turbofan engine
MTU Aero Engines AG1 citations57
US10590773B2Mar 17, 2020
Contouring a blade/vane cascade stage
MTU Aero Engines AG0 citations50
US11319820B2May 3, 2022
Blade or guide vane with raised areas
MTU Aero Engines AG0 citations49
US10570743B2Feb 25, 2020
Turbomachine having an annulus enlargment and airfoil
MTU Aero Engines AG0 citations49
US11220911B2Jan 11, 2022
Guide vane airfoil for the hot gas flow path of a turbomachine
MTU Aero Engines AG0 citations46
US10876418B2Dec 29, 2020
Turbine center frame having a specifically designed annular space contour
MTU Aero Engines AG0 citations39