Inventor

Joel Meier Haynes

Inventor
Niskayuna, NY, US

Overview

23→
Patents
2001–2020
Patent span
Mechanical engineering
Primary field (CPC F)

Patents· 23 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 chambers25%
F23DBurners18%
F02CGas-turbine plants15%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants12%
F23CMethods or apparatus for combustion using fluid fuel or solid fuel suspended in  a carrier gas or air10%
Y02EReduction of greenhouse gas [ghg] emissions, related to energy generation, transmission or distribution4%
F01DNon-positive displacement machines or engines, e.g. steam turbines3%
F02KJet-propulsion plants3%
F23NRegulating or controlling combustion3%
Y02TClimate change mitigation technologies related to transportation3%
PatentTitleYear
10,767,866Micromixer for use with liquid fuel202010,480,791Fuel injector to facilitate reduced NO201910,288,291Air-shielded fuel injection assembly to facilitate reduced NO201910,280,760Turbine engine assembly and method of assembling the same201910,221,763Combustor for rotating detonation engine and method of operating same20199,771,869'Nozzle system and method for starting and operating gas turbines on lowBtu fuels'20179,599,017'Gas turbine engine and method of operating thereof'20179,557,050'Fuel nozzle and assembly and gas turbine comprising the same'20179,551,492'Gas turbine engine system and an associated method thereof'20179,366,189'System and method for reducing pressure oscillations within a gas turbine engine'20169,353,948'Gas turbine combustor including a coating having reflective characteristics for radiation heat and method for improved combustor temperature uniformity'20168,915,086'System for controlling combustion dynamics and method for operating the same'20148,789,375'Gas turbine combustor having counterflow injection mechanism and method of use'20148,387,390'Gas turbine combustor having counterflow injection mechanism'20137,908,864'Combustor nozzle for a fuel-flexible combustion system'20116,951,108'Gas turbine engine combustor can with trapped vortex cavity'20056,935,328'Method and apparatuses for gas ranges'20056,868,676'Turbine containing system and an injector therefor'20056,735,949'Gas turbine engine combustor can with trapped vortex cavity'20046,439,882'Dual fuel circuit gas burner'20026,439,881'Spiral-shaped atmospheric gas burner'20026,371,754'Flame stabilizing channel for increased turn down of gas burners'20026,315,552'Dual fuel circuit gas burner'2001

Career & activity timeline

Assembled from patent assignee/location history and declaration credentials.

2001–2020Patents assigned to GEN ELECTRIC (23)· patent assignee history
2001–2019Based in Niskayuna, NY, US· patent location history
2013–2017Patents assigned to HAYNES JOEL MEIER (5)· patent assignee history
2013–2020Based in Schenectady, NY, US· patent location history
2014Patents assigned to GOLDMEER JEFFREY SCOTT (1)· patent assignee history
2016Patents assigned to BRZEK BRIAN GENE (1)· patent assignee history
2016Patents assigned to DE BOCK HENDRIK PIETER JACOBUS (1)· patent assignee history

Inventor activity

Assignee and location history derived from the patent record.

Assignees
AssigneePatentsSpan
GEN ELECTRIC232001–2020
HAYNES JOEL MEIERself52013–2017
BRZEK BRIAN GENE12016
DE BOCK HENDRIK PIETER JACOBUS12016
GOLDMEER JEFFREY SCOTT12014
Locations
LocationPatentsSpan
Niskayuna, New York, US162001–2019
Schenectady, New York, US72013–2020