Inventor

NAIK PRADEEP

IN132 patents

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

NAIK PRADEEP

GEN ELECTRIC

Contoured shroud swirling pre-mix fuel injector assembly

Involute trapped vortex combustor assembly

Swirler ferrule plate having pressure drop purge passages

Centerbody injector mini mixer fuel nozzle assembly

Annular concentric fuel nozzle assembly with annular depression and radial inlet ports

Involute trapped vortex combustor assembly

Volute trapped vortex combustor assembly

Fuel injector and pre-mixer system for a burner array

Multi-point centerbody injector mini mixing fuel nozzle assembly

Centerbody injector mini mixer fuel nozzle assembly

Gas turbine fuel nozzle having a fuel passage within a swirler

Combustor with an ignition tube

Combustor with alternating dilution fence

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 combustor having secondary fuel nozzles with plural passages for injecting a diluent and a fuel

Gas turbine fuel mixer comprising a plurality of mini tubes for generating a fuel-air mixture

Combustor liner having dilution openings with swirl vanes

Combustion liner

Combustion section and fuel injector assembly for a heat engine

Combustor swirler

Combustor assembly for a turbine engine

Jet swirl air blast fuel injector for gas turbine engine

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

Swirler opposed dilution with shaped and cooled fence

Multi-point injection mini mixing fuel nozzle assembly

Fuel nozzle assembly

Multi-point injection mini mixing fuel nozzle assembly

Combustor for a gas turbine engine

System and method having annular flow path architecture

Premixer for a combustor

Fuel injector assembly for gas turbine engine

Combustor with lean openings

Wavy annular dilution slots for lower emissions

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

Mixer vanes

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

Annular dome assembly for a combustor

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

Method of operating a gas turbine combustor comprising injecting a diluent into the primary and secondary combustion zones

Mixer vanes having a waveform profile

Varying dilution hole design for combustor liners

Combustion liner

Method of supplying fuel and air to a combustor with an ignition tube

Combustor

Fuel-air mixing assembly in a turbine engine

GENERAL ELECTRIC COMPANY

Combustion liner