11 Patents
- US125350122026Turbine Nozzle Assembly with Symmetrical Stress Relief Structure for Mounting Rail
GE Vernova Infrastructure Technology LLC
0 cites - US124978982025Turbine Blade Tip Shroud with Axially Offset Cutter Teeth, and Related Surface Profiles and Method
GE Infrastructure Technology LLC
0 cites - US124488942025Aerodynamic Turbomachine Component with Cooling Features and Method of Making
GE Infrastructure Technology LLC
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- US118852412024Turbine Nozzle Assembly with Stress Relief Structure for Mounting Rail
General Electric Company
0 cites - US118213362023Turbine Blade Tip Shroud with Axially Offset Cutter Teeth, and Related Surface Profiles and Method
General Electric Company
0 cites - US118149912023Turbine Nozzle Assembly with Stress Relief Structure for Mounting Rail
General Electric Company
0 cites - 0 cites
- 0 cites
- US116296012023Turbomachine Rotor Blade with a Cooling Circuit Having an Offset Rib
General Electric Company
0 cites - 0 cites