🔗 Permalink

Inventor profile of:

Rodolphe Dudebout

City:

Phoenix, Arizona

Country:

United States

Published Applications:

Last publication date:

2024-09-17

Top Assignees for applications by Rodolphe Dudebout

The entities that hold a legal rights for patent applications filed by inventor Dudebout Rodolphe:

HONEYWELL INTERNATIONAL INC. 16 Morristown, NJ United States
Honeywell International Inc. 11 Charlotte, NC United States
UOP LLC 10 Des Plaines, IL United States
HONEYWELL INTERNATIONAL INC. 9 Morris Plains, NJ United States

Recent patent applications by Dudebout Rodolphe

Rodolphe Dudebout from Phoenix, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2024-09-17

US18329041

Mechanical engineering

Gas turbine engine hydrogen supply system and method

#2 | 2024-04-16

US18189739

Mechanical engineering

Deswirl system for gas turbine engine

#3 | 2024-04-04

US20240110520A1

Mechanical engineering

GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES

#4 | 2023-06-08

US20230175696A1

Mechanical engineering

Gas turbine engine injector module with thermally coupled fuel lines having respective outlets

#5 | 2022-11-17

US20220364727A1

Mechanical engineering

Coating occlusion resistant effusion cooling holes for gas turbine engine

#6 | 2022-08-18

US20220260016A1

Mechanical engineering

Combustor for gas turbine engine and method of manufacture

#7 | 2021-10-21

US20210325045A1

Mechanical engineering

Plug resistant effusion holes for gas turbine engine

#8 | 2021-04-22

US20210116128A1

Mechanical engineering

Axially staged rich quench lean combustion system

#9 | 2020-12-03

US20200378305A1

Mechanical engineering

Plug resistant effusion holes for gas turbine engine

#10 | 2020-05-28

US20200166211A1

Mechanical engineering

Plug resistant effusion holes for gas turbine engine

#11 | 2020-04-30

US20200132304A1

Mechanical engineering

Gas turbine engine dual-wall hot section structure

#12 | 2019-02-28

US20190063754A1

Mechanical engineering

Axially staged rich quench lean combustion system

#13 | 2018-10-25

US20180306114A1

Mechanical engineering

Gas turbine engine components with air-cooling features, and related methods of manufacturing the same

#14 | 2017-10-12

US20170291860A1

Chemistry; metallurgy

Methane conversion apparatus and process using a supersonic flow reactor

#15 | 2017-08-03

US20170216809A1

Performing operations; transporting

Methane conversion apparatus and process using a supersonic flow reactor

#16 | 2017-01-19

US20170015606A1

Chemistry; metallurgy

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR

#17 | 2016-03-03

US20160061451A1

Mechanical engineering

Gas turbine engines with plug resistant effusion cooling holes

#18 | 2015-08-13

US20150226433A1

Mechanical engineering

Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques

#19 | 2014-04-24

US20140109581A1

Mechanical engineering

Reverse-flow annular combustor for reduced emissions

#20 | 2014-02-27

US20140058178A1

Chemistry; metallurgy

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR

#21 | 2014-02-27

US20140058176A1

Performing operations; transporting

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR

#22 | 2014-02-27

US20140058174A1

Performing operations; transporting

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR

#23 | 2014-02-27

US20140058173A1

Performing operations; transporting

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR

#24 | 2014-02-27

US20140058172A1

Performing operations; transporting

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR

#25 | 2014-02-27

US20140058169A1

Performing operations; transporting

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR

#26 | 2014-02-27

US20140056771A1

Performing operations; transporting

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR

#27 | 2014-02-27

US20140056769A1

Performing operations; transporting

Methane conversion apparatus and process using a supersonic flow reactor

#28 | 2013-08-29

US20130219911A1

Mechanical engineering

COMBUSTION SYSTEM FOR A GAS TURBINE ENGINE AND METHOD FOR DIRECTING FUEL FLOW WITHIN THE SAME

#29 | 2012-12-06

US20120304647A1

Mechanical engineering

Reverse-flow annular combustor for reduced emissions

#30 | 2009-06-04

US20090139239A1

Mechanical engineering

Quench jet arrangement for annular rich-quench-lean gas turbine combustors

#31 | 2009-04-02

US20090084110A1

Mechanical engineering

Combustor systems with liners having improved cooling hole patterns

#32 | 2008-12-25

US20080314044A1

Mechanical engineering

Heat shields for use in combustors

#33 | 2008-09-18

US20080223835A1

Mechanical engineering

Methods of forming fan-shaped effusion holes in combustors

#34 | 2008-06-05

US20080127651A1

Mechanical engineering

Quench jet arrangement for annular rich-quench-lean gas turbine combustors

#35 | 2007-10-25

US20070245710A1

Mechanical engineering

Optimized configuration of a reverse flow combustion system for a gas turbine engine

#36 | 2007-07-26

US20070169484A1

Mechanical engineering

Segmented effusion cooled gas turbine engine combustor

#37 | 2007-05-24

US20070113557A1

Mechanical engineering

System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines

#38 | 2006-12-07

US20060272335A1

Mechanical engineering

Advanced effusion cooling schemes for combustor domes

#39 | 2006-02-23

US20060037323A1

Mechanical engineering

Film effectiveness enhancement using tangential effusion

#40 | 2005-11-10

US20050247065A1

Mechanical engineering

Rich quick mix combustion system

#41 | 2005-04-14

US20050076650A1

Mechanical engineering

Auxiliary power unit having a rotary fuel slinger

InventorID:

407176 ⎘