14 Patents
- US126128832026Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US125601252026Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US125101042025Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US124979342025Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US124979232025Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US124488922025Composite Airfoil Assembly Having a Composite Airfoil and Spar
General Electric Company
0 cites - US124290672025Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US124289622025Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US124218542025Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US124162762025Trunnion-to-disk Connection for an Open Fan Configuration Aircraft Powerplant
GE Aviation Systems Limited
0 cites - US122920172025Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - US120128982024Gas Turbine Engine with Acoustic Spacing of the Fan Blades and Outlet Guide Vanes
General Electric Company
0 cites - 0 cites
- US119134082024Trunnion-to-disk Connection for an Open Fan Configuration Aircraft Powerplant
GE Aviation Systems Limited
0 cites