Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Interface ring for gas turbine fuel nozzle assemblies

Interface ring for gas turbine fuel nozzle assemblies

US Patent 9291102 · Granted Mar 22, 2016

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Converging duct with elongated and hexagonal cooling features2021
Method for constructing impingement/effusion cooling features in a component of 2021
Ducting arrangement with injector assemblies configured to form a shielding flow2021
Fuel injector including a lobed mixer and vanes for injecting alternate fuels in2020
Acoustic damping system for a combustor of a gas turbine engine2019
Flexible fuel combustion system for turbine engines2019
Film cooling hole arrangement for acoustic resonators in gas turbine engines2019
Film cooling hole arrangement for acoustic resonators in gas turbine engines2019
Cooling system for fuel nozzles within combustor in a turbine engine2019
Device for improved air and fuel distribution to a combustor2019
Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine en2018
Method and computer-readable model for additively manufacturing ducting arrangem2018