Inventor
Jonathan Dwight Berry
Inventor
Simpsonville, SC, US
Overview
Patents· 89 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F23Rprimary
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers32%
F02CGas-turbine plants14%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants12%
F01DNon-positive displacement machines or engines, e.g. steam turbines7%
F23DBurners7%
Y02TClimate change mitigation technologies related to transportation3%
F23CMethods or apparatus for combustion using fluid fuel or solid fuel suspended in a carrier gas or air3%
Y02EReduction of greenhouse gas [ghg] emissions, related to energy generation, transmission or distribution3%
C01BNon-metallic elements2%
B01JChemical or physical processes, e.g. catalysis or colloid chemistry2%
PatentTitleYear
11,047,248Curved seal for adjacent gas turbine components202111,002,190Segmented annular combustion system202110,995,620Turbomachine component with coating-capturing feature for thermal insulation202110,900,362Insert system for an airfoil and method of installing same202110,830,442Segmented annular combustion system with dual fuel capability202010,724,441Segmented annular combustion system202010,711,620Insert system for an airfoil and method of installing same202010,690,350Combustor with axially staged fuel injection202010,690,056Segmented annular combustion system with axial fuel staging202010,677,466Combustor inlet flow conditioner202010,655,541Segmented annular combustion system202010,641,176Combustion system with panel fuel injector202010,641,175Panel fuel injector202010,641,491Cooling of integrated combustor nozzle of segmented annular combustion system202010,605,459Integrated combustor nozzle for a segmented annular combustion system202010,584,880Mounting of integrated combustor nozzles in a segmented annular combustion system202010,584,876Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system202010,584,638Turbine nozzle cooling with panel fuel injector202010,563,869Operation and turndown of a segmented annular combustion system202010,520,193Cooling patch for hot gas path components201910,520,194Radially stacked fuel injection module for a segmented annular combustion system201910,408,455Fuel nozzle assembly with fuel inlet slots201910,352,571Catalytic ignition system201910,344,982Compact multi-residence time bundled tube fuel nozzle having transition portions of different lengths201910,196,976System and method for producing hydrogen rich fuel201910,107,499Fuel plenum for a fuel nozzle and method of making same201810,087,844Bundled tube fuel nozzle assembly with liquid fuel capability201810,072,847Method for repairing a bundled tube fuel injector201810,072,848Fuel injector with premix pilot nozzle20189,995,221Staged fuel and air injection in combustion systems of gas turbines20189,989,260Staged fuel and air injection in combustion systems of gas turbines20189,976,487Staged fuel and air injection in combustion systems of gas turbines20189,945,562Staged fuel and air injection in combustion systems of gas turbines20189,945,294Staged fuel and air injection in combustion systems of gas turbines20189,938,903Staged fuel and air injection in combustion systems of gas turbines20189,534,781'System and method having multi-tube fuel nozzle with differential flow'20179,476,592'System for injecting fuel in a gas turbine combustor'20169,435,540'Fuel injector with premix pilot nozzle'20169,388,985'Premixing apparatus for gas turbine system'20169,383,098'Radial flow fuel nozzle for a combustor of a gas turbine'20169,366,440'Fuel nozzles with mixing tubes surrounding a liquid fuel cartridge for injecting fuel in a gas turbine combustor'20169,285,121'Gas turbine cooling circuit including a seal for a perforated plate'20169,259,807'Method for repairing a bundled tube fuel injector'20169,243,803'System for cooling a multi-tube fuel nozzle'20169,212,822'Fuel injection assembly for use in turbine engines and method of assembling same'20159,175,855'Combustion nozzle with floating aft plate'20159,121,609'Method and apparatus for introducing diluent flow into a combustor'20159,103,551'Combustor leaf seal arrangement'20159,052,112'Combustor and method for purging a combustor'20158,991,149'Dry 3-way catalytic reduction of gas turbine NOX'20158,991,187'Combustor with a lean pre-nozzle fuel injection system'20158,984,887'Combustor and method for supplying fuel to a combustor'20158,938,978'Gas turbine engine combustor with lobed, three dimensional contouring'20158,931,283'Reformed multi-fuel premixed low emission combustor and related method'20158,925,324'Turbomachine including a mixing tube element having a vortex generator'20158,904,748'System and method for producing hydrogen rich fuel'20148,904,797'Sector nozzle mounting systems'20148,893,511'Systems and methods for a gas turbine combustor having a bleed duct'20148,800,289'Apparatus and method for mixing fuel in a gas turbine nozzle'20148,795,398'Apparatus for vaporizing and reforming liquid fuels'20148,769,956'Multi-premixer fuel nozzle support system'20148,752,362'Optical flame holding and flashback detection'20148,733,106'Fuel injector and support plate'20148,707,705'Impingement cooled transition piece aft frame'20148,689,559'Secondary combustion system for reducing the level of emissions generated by a turbomachine'20148,567,199'Method and apparatus of introducing diluent flow into a combustor'20138,550,809'Combustor and method for conditioning flow through a combustor'20138,528,337'Lobe nozzles for fuel and air injection'20138,522,555'Multi-premixer fuel nozzle support system'20138,495,881'System and method for thermal control in a cap of a gas turbine combustor'20138,474,266'System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle'20138,454,350'Diluent shroud for combustor'20138,448,443'Combustion liner thimble insert and related method'20138,397,482'Dry 3-way catalytic reduction of gas turbine NOx '20138,387,380'Catalytic burner apparatus for Stirling Engine'20138,381,532'Bled diffuser fed secondary combustion system for gas turbines'20138,381,526'Systems and methods of providing high pressure air to a head end of a combustor'20138,377,156'Fluid cooled reformer and method for cooling a reformer'20138,371,123'Apparatus for conditioning airflow through a nozzle'20138,276,391'Combustor liner cooling at transition duct interface and related method'20128,266,912'Reusable weld joint for syngas fuel nozzles'20128,252,251'Fluid cooled reformer and method for cooling a reformer'20128,234,872'Turbine air flow conditioner'20128,191,373'Interlocking retention strip'20127,976,594'Method and system for vaporization of liquid fuels'20117,921,653'Internal manifold air extraction system for IGCC combustor and method'20117,913,484'Catalytic burner apparatus for stirling engine'20116,612,830'Anode gas burner for inert gas generation, method and apparatus'20036,179,608'Swirling flashback arrestor'2001Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2001–2014Patents assigned to PRECISION COMBUSTION INC (6)· patent assignee history
2001–2003Based in Meriden, CT, US· patent location history
2011–2021Patents assigned to GEN ELECTRIC (83)· patent assignee history
2011–2021Based in Simpsonville, SC, US· patent location history
2011–2013Based in Simsonville, SC, US· patent location history
2012–2017Patents assigned to BERRY JONATHAN DWIGHT (37)· patent assignee history
2012–2016Based in Greenville, SC, US· patent location history
2013–2017Patents assigned to HUGHES MICHAEL JOHN (6)· patent assignee history
2013–2017Patents assigned to JOHNSON THOMAS EDWARD (6)· patent assignee history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| GEN ELECTRIC | 83 | 2011–2021 |
| BERRY JONATHAN DWIGHTself | 37 | 2012–2017 |
| HUGHES MICHAEL JOHN | 6 | 2013–2017 |
| JOHNSON THOMAS EDWARD | 6 | 2013–2017 |
| PRECISION COMBUSTION INC | 6 | 2001–2014 |
Locations
| Location | Patents | Span |
|---|---|---|
| Simpsonville, SC, US | 77 | 2011–2021 |
| Greenville, SC, US | 8 | 2012–2016 |
| Simsonville, SC, US | 2 | 2011–2013 |
| Meriden, CT, US | 2 | 2001–2003 |