Inventor

VISE STEVEN C

US40 patents

⚠️ This page may combine multiple inventors who share the name “VISE STEVEN C”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

VISE STEVEN C

GEN ELECTRIC

Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form

Gas turbine fuel nozzle having a fuel passage within a swirler

Combustion section with a primary combustor and a set of secondary combustors

Swirler-ferrule assembly

Fuel nozzle and swirler

Coupling a fuel nozzle purge flow directly to a swirler

Multi pressure drop swirler ferrule plate

Gas turbine fuel nozzle having a lip extending from the vanes of a swirler

Diffuser bleed assembly

Swirler with rifled venturi for dynamics mitigation

Swirler with integrated damper

Combustor with lean openings

Gas turbine engine fuel nozzle having a secondary fuel passage through a swirler

Combustor having a main chamber and one or more trapped vortex cavities

Gas turbine fuel nozzle having an inner air passage and plural outer fuel passages

Combustor

Turbine engine including a combustor

Combustor with lean openings

Gas turbine combustor dome with integrated flare swirler

Gas turbine and fuel nozzle assembly for mixing hydrogen fuel and steam to control flame speed

Combustor with dilution openings

Combustor with dilution openings

Combustion section with a primary combustor and a set of secondary combustors

Combustor including a steam injector operably injecting steam into a trapped vortex cavity

Combustion section with a primary combustor and a set of secondary combustors

Engine fuel nozzle and swirler

Combustion section with a primary combustion chamber and a secondary combustion chamber

Turbine engine combustor and combustor liner

Fuel nozzle and swirler

Turbine engine having a combustion section with a fuel nozzle

Diffuser with passlets

Gas turbine engine having a combustion section with steam provided to second combustor plenum

Turbine engine having a combustion section with a fuel nozzle assembly

Gas turbine nozzle having an inner air swirler passage and plural exterior fuel passages

Aerodynamic combustor liner design for emissions reductions

Active boundary layer control in diffuser

Fuel supply system for a combustor

Combustor

Ignition system and method of operating a combustion engine

GENERAL ELECTRIC COMPANY

Gas turbine engine, fuel nozzle assembly, and method