Jeremy Paul Francisco Gonzalez
19Patents
1h-index
19Co-inventors
43Inventor score
Filing activity: Mar 25, 2016 → Mar 25, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US11434826B2 | Acoustic treatment panel for a turbojet engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US11248530B2 | Acoustic treatment panel for a turbojet engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US11939936B2 | Thrust reverser cascade including acoustic treatment | Emerging Cross-Sectional Technologies | 1 | Active |
| US12384552B2 | Method of reducing noise of aircraft having hybrid power plants | Emerging Cross-Sectional Technologies | 0 | Active |
| US10662876B2 | Turbomachine vane comprising an electroacoustic source with improved assembly mode, row of outlet guide vanes and turbomachine comprising such a vane | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11885280B2 | Thrust reverser cascade including acoustic treatment | Emerging Cross-Sectional Technologies | 0 | Active |
| US11149685B2 | Modified acoustic secondary nozzle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11788489B2 | Thrust reverser cascade including acoustic treatment | Emerging Cross-Sectional Technologies | 0 | Active |
| US11554534B2 | Method for in situ additive manufacturing of a coating on a turbomachine casing | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12320316B2 | Thrust reverser cascade including acoustic treatment | Emerging Cross-Sectional Technologies | 0 | Active |
| US10557417B2 | Acoustic absorber cell for a turbojet, and an associated acoustic treatment panel | Emerging Cross-Sectional Technologies | 0 | Active |
| US10967980B2 | Turbine engine propelled airplane having an acoustic baffle | Emerging Cross-Sectional Technologies | 0 | Active |
| US10408165B2 | Device with gratings for ejecting microjets in order to reduce the jet noise of a turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US10995702B2 | Heating system for convergent-divergent secondary nozzle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11572832B2 | Method for preparing a support and for acoustic management on a turbine engine or a nacelle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12173652B2 | Acoustic management, on a turbomachine or a nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US11472565B2 | Turbomachine nacelle having acoustically porous walls | Emerging Cross-Sectional Technologies | 0 | Active |
| US11000964B2 | Device for perforating an acoustic annular panel for a turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11560842B2 | Acoustic panel and associated propulsion unit | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.