Pradeep Naik
114Patents
5h-index
68Co-inventors
69Inventor score
Filing activity: Sep 9, 2015 → Jul 8, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10502425B2 | Contoured shroud swirling pre-mix fuel injector assembly | Emerging Cross-Sectional Technologies | 13 | Active |
| US11067280B2 | Centerbody injector mini mixer fuel nozzle assembly | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US10295190B2 | Centerbody injector mini mixer fuel nozzle assembly | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US10935245B2 | Annular concentric fuel nozzle assembly with annular depression and radial inlet ports | Emerging Cross-Sectional Technologies | 6 | Active |
| US10352569B2 | Multi-point centerbody injector mini mixing fuel nozzle assembly | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US10976053B2 | Involute trapped vortex combustor assembly | Emerging Cross-Sectional Technologies | 5 | Active |
| US10393382B2 | Multi-point injection mini mixing fuel nozzle assembly | Emerging Cross-Sectional Technologies | 4 | Active |
| US11156361B2 | Multi-point injection mini mixing fuel nozzle assembly | Emerging Cross-Sectional Technologies | 4 | Active |
| US11181269B2 | Involute trapped vortex combustor assembly | Emerging Cross-Sectional Technologies | 3 | Active |
| US11022313B2 | Combustor assembly for a turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US11578868B1 | Combustor with alternating dilution fence | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10465907B2 | System and method having annular flow path architecture | Emerging Cross-Sectional Technologies | 3 | Active |
| US11286884B2 | Combustion section and fuel injector assembly for a heat engine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US11454396B1 | Fuel injector and pre-mixer system for a burner array | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11846426B2 | Gas turbine combustor having secondary fuel nozzles with plural passages for injecting a diluent and a fuel | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10976052B2 | Volute trapped vortex combustor assembly | Emerging Cross-Sectional Technologies | 2 | Active |
| US11156360B2 | Fuel nozzle assembly | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10890329B2 | Fuel injector assembly for gas turbine engine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11592182B1 | Swirler ferrule plate having pressure drop purge passages | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10808934B2 | Jet swirl air blast fuel injector for gas turbine engine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11692709B2 | Gas turbine fuel mixer comprising a plurality of mini tubes for generating a fuel-air mixture | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11686473B2 | Combustion liner | Emerging Cross-Sectional Technologies | 1 | Active |
| US12173898B1 | Combustion section with a primary combustor and a set of secondary combustors | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11774098B2 | Combustor for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10197279B2 | Combustor assembly for a turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.