Rodolphe Dudebout
31Patents
10h-index
57Co-inventors
78Inventor score
Filing activity: Jun 15, 2001 → Jun 5, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7185497B2 | Rich quick mix combustion system | Mechanical Engineering; Lighting; Heating | 97 | Expired |
| US6554562B2 | Combustor hot streak alignment for gas turbine engine | Emerging Cross-Sectional Technologies | 24 | Expired |
| US7665306B2 | Heat shields for use in combustors | Emerging Cross-Sectional Technologies | 21 | Active |
| US7506512B2 | Advanced effusion cooling schemes for combustor domes | Emerging Cross-Sectional Technologies | 20 | Active |
| US7546737B2 | Segmented effusion cooled gas turbine engine combustor | Emerging Cross-Sectional Technologies | 20 | Active |
| US7500364B2 | System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines | Mechanical Engineering; Lighting; Heating | 17 | Active |
| US9080770B2 | Reverse-flow annular combustor for reduced emissions | Emerging Cross-Sectional Technologies | 14 | Active |
| US7812282B2 | Methods of forming fan-shaped effusion holes in combustors | Emerging Cross-Sectional Technologies | 14 | Active |
| US7036321B2 | Auxiliary power unit having a rotary fuel slinger | Mechanical Engineering; Lighting; Heating | 14 | Expired |
| US7905094B2 | Combustor systems with liners having improved cooling hole patterns | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US9410702B2 | Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques | Emerging Cross-Sectional Technologies | 10 | Active |
| US9400110B2 | Reverse-flow annular combustor for reduced emissions | Emerging Cross-Sectional Technologies | 7 | Active |
| US7926284B2 | Quench jet arrangement for annular rich-quench-lean gas turbine combustors | Emerging Cross-Sectional Technologies | 6 | Active |
| US8127554B2 | Quench jet arrangement for annular rich-quench-lean gas turbine combustors | Emerging Cross-Sectional Technologies | 3 | Active |
| US10895157B2 | Gas turbine engine components with air-cooling features, and related methods of manufacturing the same | Emerging Cross-Sectional Technologies | 3 | Active |
| US10101030B2 | Gas turbine engines with plug resistant effusion cooling holes | Emerging Cross-Sectional Technologies | 2 | Active |
| US11085641B2 | Plug resistant effusion holes for gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US9656229B2 | Methane conversion apparatus and process using a supersonic flow reactor | Chemistry; Metallurgy | 1 | Active |
| US11306659B2 | Plug resistant effusion holes for gas turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US10816211B2 | Axially staged rich quench lean combustion system | Emerging Cross-Sectional Technologies | 1 | Active |
| US10775044B2 | Gas turbine engine dual-wall hot section structure | Emerging Cross-Sectional Technologies | 1 | Active |
| US12092032B1 | Gas turbine engine hydrogen supply system and method | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10166524B2 | Methane conversion apparatus and process using a supersonic flow reactor | Chemistry; Metallurgy | 0 | Active |
| US11287133B2 | Axially staged rich quench lean combustion system | Emerging Cross-Sectional Technologies | 0 | Active |
| US11988386B2 | Gas turbine engine injector module with thermally coupled fuel lines having respective outlets | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.