Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Nozzle device for feeding fuel into a combustion chamber of a gas turbine assembly, and gas turbine assembly

Nozzle device for feeding fuel into a combustion chamber of a gas turbine assembly, and gas turbine assembly

US Patent 12055294 · Granted Aug 6, 2024

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Combustion chamber assembly for operation with liquid and/or gaseous fuel, gas t2025
Combustion chamber assembly for an engine with at least one heat exchanger chann2025
Dual fuel gas turbine combustion chamber module having an annular combustion cha2025
Combustion chamber module having an annular combustion chamber2025
Combustion chamber module having an annular combustion chamber2025
Drive system for an aircraft, aircraft having a drive system and method for oper2025
Piloting arrangement, nozzle device, gas turbine arrangement and method2025
Fuel nozzle having different first and second discharge orifices for providing a2025
Connecting apparatus for the flow connection between a fuel feed line system and2025
Pilot arrangement, nozzle device, method and gas turbine arrangement2024
Measuring device comprising at least one fluid channel for guiding a measurement2023
Combustion chamber shingle arrangement of a gas turbine2020