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Inventor profile of:

Eric John Stevens

City:

Mason, Ohio

Country:

United States

Published Applications:

13

Last publication date:

2024-11-21

Top Assignees for applications by Eric John Stevens

The entities that hold a legal rights for patent applications filed by inventor Stevens Eric John:

Recent patent applications by Stevens Eric John

Eric John Stevens from Mason, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2024-11-21
US20240384873A1
Mechanical engineering

TRAPPED VORTEX COMBUSTOR AND METHOD FOR OPERATING THE SAME

 #2 | 2022-03-24
US20220090788A1
Mechanical engineering

Trapped vortex combustor for a gas turbine engine with a driver airflow channel

 #3 | 2022-02-10
US20220042684A1
Mechanical engineering

COMBUSTION SYSTEM AND METHOD FOR ATTENUATION OF COMBUSTION DYNAMICS IN A GAS TURBINE ENGINE

 #4 | 2021-10-14
US20210317990A1
Mechanical engineering

Trapped vortex combustor and method for operating the same

 #5 | 2019-08-01
US20190234615A1
Mechanical engineering

Combustor and method of operation for improved emissions and durability

 #6 | 2019-04-18
US20190113235A1
Mechanical engineering

Tangential bulk swirl air in a trapped vortex combustor for a gas turbine engine

 #7 | 2019-03-21
US20190086092A1
Mechanical engineering

Trapped vortex combustor and method for operating the same

 #8 | 2019-03-21
US20190086088A1
Mechanical engineering

Combustor mixer purge cooling structure

 #9 | 2019-02-28
US20190063753A1
Mechanical engineering

Fuel nozzle assembly for high fuel/air ratio and reduced combustion dynamics

 #10 | 2019-02-28
US20190063752A1
Mechanical engineering

Combustor system for high fuel/air ratio and reduced combustion dynamics

 #11 | 2019-02-21
US20190056114A1
Mechanical engineering

Combustion system and method for attenuation of combustion dynamics in a gas turbine engine

 #12 | 2019-02-21
US20190056110A1
Mechanical engineering

Fuel nozzle with angled main injection ports and radial main injection ports

 #13 | 2018-11-08
US20180320900A1
Mechanical engineering

Trapped vortex combustor for a gas turbine engine with a driver airflow channel
InventorID:

2343324 ⎘