Inventor
DUDEBOUT RODOLPHE
US31 patents
⚠️ This page may combine multiple inventors who share the name “DUDEBOUT RODOLPHE”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
HONEYWELL INT INC
26 patentsUS7185497B2Mar 6, 2007
Rich quick mix combustion system
HONEYWELL INT INC111 citations96
US7546737B2Jun 16, 2009
Segmented effusion cooled gas turbine engine combustor
HONEYWELL INT INC27 citations92
US7506512B2Mar 24, 2009
Advanced effusion cooling schemes for combustor domes
HONEYWELL INT INC36 citations92
US7665306B2Feb 23, 2010
Heat shields for use in combustors
HONEYWELL INT INC26 citations91
US7500364B2Mar 10, 2009
System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines
HONEYWELL INT INC23 citations91
US6554562B2Apr 29, 2003
Combustor hot streak alignment for gas turbine engine
HONEYWELL INT INC47 citations90
US7036321B2May 2, 2006
Auxiliary power unit having a rotary fuel slinger
HONEYWELL INT INC24 citations88
US11085641B2Aug 10, 2021
Plug resistant effusion holes for gas turbine engine
HONEYWELL INT INC6 citations83
US7926284B2Apr 19, 2011
Quench jet arrangement for annular rich-quench-lean gas turbine combustors
HONEYWELL INT INC11 citations83
US7905094B2Mar 15, 2011
Combustor systems with liners having improved cooling hole patterns
HONEYWELL INT INC15 citations83
US9410702B2Aug 9, 2016
Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques
HONEYWELL INT INC15 citations80
US9400110B2Jul 26, 2016
Reverse-flow annular combustor for reduced emissions
HONEYWELL INT INC9 citations79
US7812282B2Oct 12, 2010
Methods of forming fan-shaped effusion holes in combustors
HONEYWELL INT INC18 citations79
US12092032B1Sep 17, 2024
Gas turbine engine hydrogen supply system and method
HONEYWELL INT INC3 citations75
US11519604B2Dec 6, 2022
Plug resistant effusion holes for gas turbine engine
HONEYWELL INT INC2 citations72
US10895157B2Jan 19, 2021
Gas turbine engine components with air-cooling features, and related methods of manufacturing the same
HONEYWELL INT INC5 citations72
US10101030B2Oct 16, 2018
Gas turbine engines with plug resistant effusion cooling holes
HONEYWELL INT INC3 citations72
US10775044B2Sep 15, 2020
Gas turbine engine dual-wall hot section structure
HONEYWELL INT INC2 citations68
US11959401B1Apr 16, 2024
Deswirl system for gas turbine engine
HONEYWELL INT INC2 citations65
US11306659B2Apr 19, 2022
Plug resistant effusion holes for gas turbine engine
HONEYWELL INT INC1 citations62
US11287133B2Mar 29, 2022
Axially staged rich quench lean combustion system
HONEYWELL INT INC0 citations60
US10816211B2Oct 27, 2020
Axially staged rich quench lean combustion system
HONEYWELL INT INC1 citations60
US12372239B2Jul 29, 2025
Gaseous fuel nozzle for use in gas turbine engines
HONEYWELL INT INC0 citations52
US11674686B2Jun 13, 2023
Coating occlusion resistant effusion cooling holes for gas turbine engine
HONEYWELL INT INC0 citations51
US11549437B2Jan 10, 2023
Combustor for gas turbine engine and method of manufacture
HONEYWELL INT INC0 citations41
US11988386B2May 21, 2024
Gas turbine engine injector module with thermally coupled fuel lines having respective outlets
HONEYWELL INT INC0 citations40
UOP LLC
3 patentsUS10166524B2Jan 1, 2019
Methane conversion apparatus and process using a supersonic flow reactor
UOP LLC1 citations62
US9656229B2May 23, 2017
Methane conversion apparatus and process using a supersonic flow reactor
UOP LLC1 citations51
US10029957B2Jul 24, 2018
Methane conversion apparatus and process using a supersonic flow reactor
UOP LLC0 citations39