Rodolphe Dudebout

Person

Phoenix, AZ, US

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine hydrogen supply system and method
- Patent number 12,092,032
- Issue date Sep 17, 2024
- Honeywell International Inc.
- Rodolphe Dudebout
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine injector module with thermally coupled fuel line...
- Patent number 11,988,386
- Issue date May 21, 2024
- Honeywell International Inc.
- Duane Peterson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Deswirl system for gas turbine engine
- Patent number 11,959,401
- Issue date Apr 16, 2024
- Honeywell International Inc.
- Shakeel Nasir
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Coating occlusion resistant effusion cooling holes for gas turbine...
- Patent number 11,674,686
- Issue date Jun 13, 2023
- Honeywell International Inc.
- Nagaraja Rudrapatna
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Combustor for gas turbine engine and method of manufacture
- Patent number 11,549,437
- Issue date Jan 10, 2023
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Plug resistant effusion holes for gas turbine engine
- Patent number 11,519,604
- Issue date Dec 6, 2022
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Plug resistant effusion holes for gas turbine engine
- Patent number 11,306,659
- Issue date Apr 19, 2022
- Honeywell International Inc.
- Rodolphe Dudebout
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Axially staged rich quench lean combustion system
- Patent number 11,287,133
- Issue date Mar 29, 2022
- Honeywell International Inc.
- Rodolphe Dudebout
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Plug resistant effusion holes for gas turbine engine
- Patent number 11,085,641
- Issue date Aug 10, 2021
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine components with air-cooling features, and relate...
- Patent number 10,895,157
- Issue date Jan 19, 2021
- Honeywell International Inc.
- Rodolphe Dudebout
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Axially staged rich quench lean combustion system
- Patent number 10,816,211
- Issue date Oct 27, 2020
- Honeywell International Inc.
- Rodolphe Dudebout
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine dual-wall hot section structure
- Patent number 10,775,044
- Issue date Sep 15, 2020
- Honeywell International Inc.
- Rodolphe Dudebout
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Methane conversion apparatus and process using a supersonic flow re...
- Patent number 10,166,524
- Issue date Jan 1, 2019
- UOP LLC
- Robert L. Bedard
- C07 - ORGANIC CHEMISTRY
Information Patent Grant
Gas turbine engines with plug resistant effusion cooling holes
- Patent number 10,101,030
- Issue date Oct 16, 2018
- Honeywell International Inc.
- Rodolphe Dudebout
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Methane conversion apparatus and process using a supersonic flow re...
- Patent number 9,656,229
- Issue date May 23, 2017
- UOP LLC
- Robert L. Bedard
- C10 - PETROLEUM, GAS OR COKE INDUSTRIES TECHNICAL GASES CONTAINING CARBON MON...
Information Patent Grant
Gas turbine engine combustors with effusion and impingement cooling...
- Patent number 9,410,702
- Issue date Aug 9, 2016
- Honeywell International Inc.
- Rodolphe Dudebout
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Reverse-flow annular combustor for reduced emissions
- Patent number 9,400,110
- Issue date Jul 26, 2016
- Honeywell International Inc.
- Rodolphe Dudebout
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Reverse-flow annular combustor for reduced emissions
- Patent number 9,080,770
- Issue date Jul 14, 2015
- Honeywell International Inc.
- Rodolphe Dudebout
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Quench jet arrangement for annular rich-quench-lean gas turbine com...
- Patent number 8,127,554
- Issue date Mar 6, 2012
- Honeywell International Inc.
- Frank J. Zupanc
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Quench jet arrangement for annular rich-quench-lean gas turbine com...
- Patent number 7,926,284
- Issue date Apr 19, 2011
- Honeywell International Inc.
- Frank J. Zupanc
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Combustor systems with liners having improved cooling hole patterns
- Patent number 7,905,094
- Issue date Mar 15, 2011
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Methods of forming fan-shaped effusion holes in combustors
- Patent number 7,812,282
- Issue date Oct 12, 2010
- Honeywell International Inc.
- Terrel E. Kuhn
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Heat shields for use in combustors
- Patent number 7,665,306
- Issue date Feb 23, 2010
- Honeywell International Inc.
- Thomas J. Bronson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Segmented effusion cooled gas turbine engine combustor
- Patent number 7,546,737
- Issue date Jun 16, 2009
- Honeywell International Inc.
- Jurgen C. Schumacher
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Advanced effusion cooling schemes for combustor domes
- Patent number 7,506,512
- Issue date Mar 24, 2009
- Honeywell International Inc.
- Jurgen C. Schumacher
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
System for coupling flow from a centrifugal compressor to an axial...
- Patent number 7,500,364
- Issue date Mar 10, 2009
- Honeywell International Inc.
- Jurgen C. Schumacher
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Rich quick mix combustion system
- Patent number 7,185,497
- Issue date Mar 6, 2007
- Honeywell International, Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Auxiliary power unit having a rotary fuel slinger
- Patent number 7,036,321
- Issue date May 2, 2006
- Honeywell International, Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Combustor hot streak alignment for gas turbine engine
- Patent number 6,554,562
- Issue date Apr 29, 2003
- Honeywell International, Inc.
- Rodolphe Dudebout
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Patents Applicationslast 30 patents

Information Patent Application
GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES
- Publication number 20240110520
- Publication date Apr 4, 2024
- Honeywell International Inc.
- Rodolphe Dudebout
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE INJECTOR MODULE WITH THERMALLY COUPLED FUEL LINE...
- Publication number 20230175696
- Publication date Jun 8, 2023
- Honeywell International Inc.
- Duane Peterson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COATING OCCLUSION RESISTANT EFFUSION COOLING HOLES FOR GAS TURBINE...
- Publication number 20220364727
- Publication date Nov 17, 2022
- Honeywell International Inc.
- Nagaraja Rudrapatna
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COMBUSTOR FOR GAS TURBINE ENGINE AND METHOD OF MANUFACTURE
- Publication number 20220260016
- Publication date Aug 18, 2022
- Honeywell International Inc.
- Rodolphe Dudebout
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PLUG RESISTANT EFFUSION HOLES FOR GAS TURBINE ENGINE
- Publication number 20210325045
- Publication date Oct 21, 2021
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
AXIALLY STAGED RICH QUENCH LEAN COMBUSTION SYSTEM
- Publication number 20210116128
- Publication date Apr 22, 2021
- HONEYWELL INTERNATIONAL INC.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
PLUG RESISTANT EFFUSION HOLES FOR GAS TURBINE ENGINE
- Publication number 20200378305
- Publication date Dec 3, 2020
- HONEYWELL INTERNATIONAL INC.
- Rodolphe Dudebout
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
PLUG RESISTANT EFFUSION HOLES FOR GAS TURBINE ENGINE
- Publication number 20200166211
- Publication date May 28, 2020
- HONEYWELL INTERNATIONAL INC.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
GAS TURBINE ENGINE DUAL-WALL HOT SECTION STRUCTURE
- Publication number 20200132304
- Publication date Apr 30, 2020
- HONEYWELL INTERNATIONAL INC.
- Rodolphe Dudebout
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AXIALLY STAGED RICH QUENCH LEAN COMBUSTION SYSTEM
- Publication number 20190063754
- Publication date Feb 28, 2019
- HONEYWELL INTERNATIONAL INC.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
GAS TURBINE ENGINE COMPONENTS WITH AIR-COOLING FEATURES, AND RELATE...
- Publication number 20180306114
- Publication date Oct 25, 2018
- HONEYWELL INTERNATIONAL INC.
- Rodolphe Dudebout
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20170216809
- Publication date Aug 3, 2017
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20170015606
- Publication date Jan 19, 2017
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
GAS TURBINE ENGINES WITH PLUG RESISTANT EFFUSION COOLING HOLES
- Publication number 20160061451
- Publication date Mar 3, 2016
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
GAS TURBINE ENGINE COMBUSTORS WITH EFFUSION AND IMPINGEMENT COOLING...
- Publication number 20150226433
- Publication date Aug 13, 2015
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
REVERSE-FLOW ANNULAR COMBUSTOR FOR REDUCED EMISSIONS
- Publication number 20140109581
- Publication date Apr 24, 2014
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20140058172
- Publication date Feb 27, 2014
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20140058178
- Publication date Feb 27, 2014
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20140058169
- Publication date Feb 27, 2014
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20140056769
- Publication date Feb 27, 2014
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20140056771
- Publication date Feb 27, 2014
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20140058173
- Publication date Feb 27, 2014
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20140058174
- Publication date Feb 27, 2014
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...
- Publication number 20140058176
- Publication date Feb 27, 2014
- UOP LLC
- Robert L. Bedard
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
COMBUSTION SYSTEM FOR A GAS TURBINE ENGINE AND METHOD FOR DIRECTING...
- Publication number 20130219911
- Publication date Aug 29, 2013
- Honeywell International Inc.
- Rodolphe Dudebout
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REVERSE-FLOW ANNULAR COMBUSTOR FOR REDUCED EMISSIONS
- Publication number 20120304647
- Publication date Dec 6, 2012
- Honeywell International Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
QUENCH JET ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COM...
- Publication number 20090139239
- Publication date Jun 4, 2009
- Honeywell International, Inc.
- Frank J. Zupanc
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
COMBUSTOR SYSTEMS WITH LINERS HAVING IMPROVED COOLING HOLE PATTERNS
- Publication number 20090084110
- Publication date Apr 2, 2009
- Honeywell International, Inc.
- Rodolphe Dudebout
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
HEAT SHIELDS FOR USE IN COMBUSTORS
- Publication number 20080314044
- Publication date Dec 25, 2008
- Honeywell International, Inc.
- Thomas J. Bronson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
METHODS OF FORMING FAN-SHAPED EFFUSION HOLES IN COMBUSTORS
- Publication number 20080223835
- Publication date Sep 18, 2008
- Honeywell International, Inc.
- TERREL E. KUHN
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR

Rodolphe Dudebout

Person

Patents Grantslast 30 patents

Gas turbine engine hydrogen supply system and method

Gas turbine engine injector module with thermally coupled fuel line...

Deswirl system for gas turbine engine

Coating occlusion resistant effusion cooling holes for gas turbine...

Combustor for gas turbine engine and method of manufacture

Plug resistant effusion holes for gas turbine engine

Plug resistant effusion holes for gas turbine engine

Axially staged rich quench lean combustion system

Plug resistant effusion holes for gas turbine engine

Gas turbine engine components with air-cooling features, and relate...

Axially staged rich quench lean combustion system

Gas turbine engine dual-wall hot section structure

Methane conversion apparatus and process using a supersonic flow re...

Gas turbine engines with plug resistant effusion cooling holes

Methane conversion apparatus and process using a supersonic flow re...

Gas turbine engine combustors with effusion and impingement cooling...

Reverse-flow annular combustor for reduced emissions

Reverse-flow annular combustor for reduced emissions

Quench jet arrangement for annular rich-quench-lean gas turbine com...

Quench jet arrangement for annular rich-quench-lean gas turbine com...

Combustor systems with liners having improved cooling hole patterns

Methods of forming fan-shaped effusion holes in combustors

Heat shields for use in combustors

Segmented effusion cooled gas turbine engine combustor

Advanced effusion cooling schemes for combustor domes

System for coupling flow from a centrifugal compressor to an axial...

Rich quick mix combustion system

Auxiliary power unit having a rotary fuel slinger

Combustor hot streak alignment for gas turbine engine

Patents Applicationslast 30 patents

GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES

GAS TURBINE ENGINE INJECTOR MODULE WITH THERMALLY COUPLED FUEL LINE...

COATING OCCLUSION RESISTANT EFFUSION COOLING HOLES FOR GAS TURBINE...

COMBUSTOR FOR GAS TURBINE ENGINE AND METHOD OF MANUFACTURE

PLUG RESISTANT EFFUSION HOLES FOR GAS TURBINE ENGINE

AXIALLY STAGED RICH QUENCH LEAN COMBUSTION SYSTEM

PLUG RESISTANT EFFUSION HOLES FOR GAS TURBINE ENGINE

PLUG RESISTANT EFFUSION HOLES FOR GAS TURBINE ENGINE

GAS TURBINE ENGINE DUAL-WALL HOT SECTION STRUCTURE

AXIALLY STAGED RICH QUENCH LEAN COMBUSTION SYSTEM

GAS TURBINE ENGINE COMPONENTS WITH AIR-COOLING FEATURES, AND RELATE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

GAS TURBINE ENGINES WITH PLUG RESISTANT EFFUSION COOLING HOLES

GAS TURBINE ENGINE COMBUSTORS WITH EFFUSION AND IMPINGEMENT COOLING...

REVERSE-FLOW ANNULAR COMBUSTOR FOR REDUCED EMISSIONS

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW RE...

COMBUSTION SYSTEM FOR A GAS TURBINE ENGINE AND METHOD FOR DIRECTING...

REVERSE-FLOW ANNULAR COMBUSTOR FOR REDUCED EMISSIONS

QUENCH JET ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COM...

COMBUSTOR SYSTEMS WITH LINERS HAVING IMPROVED COOLING HOLE PATTERNS

HEAT SHIELDS FOR USE IN COMBUSTORS

METHODS OF FORMING FAN-SHAPED EFFUSION HOLES IN COMBUSTORS