Lionel CZAPLA
39Patents
3h-index
53Co-inventors
58Inventor score
Filing activity: Mar 20, 2018 → Jul 15, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10690088B2 | Jet engine comprising a nacelle equipped with reverser flaps | Emerging Cross-Sectional Technologies | 4 | Active |
| US11348565B2 | Assembly forming an acoustic insulator | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10995700B2 | Jet engine comprising a nacelle equipped with reverser flaps | Emerging Cross-Sectional Technologies | 3 | Active |
| US11867122B2 | Propulsion assembly for an aircraft | Emerging Cross-Sectional Technologies | 1 | Active |
| US12065260B2 | Aircraft comprising at least one hydrogen supply device and at least one sealed container, in which at least one item of equipment of said hydrogen supply device is positioned | Emerging Cross-Sectional Technologies | 1 | Active |
| US10669970B2 | Thrust reverser system having limited aerodynamic disturbance | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11815046B2 | Turbofan engine comprising a system for blocking the flow path of the bypass stream comprising veils | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11661203B2 | Aircraft pylon comprising a tubular primary structure including at least one twin-walled pipe, and aircraft comprising at least one such pylon | Performing Operations; Transporting | 1 | Active |
| US12246848B2 | Casing system containing a heat exchanger for reheating dihydrogen | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12078428B2 | Heat exchanger limiting the risk of contamination between two fluids and aircraft comprising at least one such heat exchanger | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11168644B2 | Jet engine comprising a nacelle equipped with a reverser system comprising inner doors and outer flaps | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12377996B2 | Propeller propulsion system with T-shaped chassis | Emerging Cross-Sectional Technologies | 0 | Active |
| US11242821B2 | Turbofan comprising a system comprising flexible screens for closing off the bypass duct | Emerging Cross-Sectional Technologies | 0 | Active |
| US12104554B2 | Aircraft propulsion assembly equipped with a thrust-reversing device comprising at least one inflatable barrier, and aircraft comprising at least one such propulsion assembly | Performing Operations; Transporting | 0 | Active |
| US11215141B2 | Jet engine comprising a nacelle equipped with reverser flaps provided with vortex-generating means | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11047262B2 | Aircraft propulsion system comprising an internal fixed structure with a discharge slot | Emerging Cross-Sectional Technologies | 0 | Active |
| US11572189B2 | Acoustic absorption structure comprising a liquid drainage system and propulsive assembly comprising such an acoustic absorption structure | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11840962B2 | Aircraft comprising a hydrogen supply device incorporating a hydrogen heating system positioned in the fuselage of the aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US12018614B2 | Dihydrogen supply system for an aircraft engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12397920B2 | Device for coupling a propulsion system to an engine pylon of an aircraft, and corresponding aircraft | Performing Operations; Transporting | 0 | Active |
| US12420944B2 | Module for a dihydrogen supply system for an aircraft engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11975858B2 | Aircraft nacelle comprising a connection between ducts comprising flanges which are oriented towards the interior, and aircraft comprising at least one nacelle of this type | Performing Operations; Transporting | 0 | Active |
| US12291350B2 | Powerplant for an aircraft | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10550796B2 | Turbojet engine comprising a nacelle equipped with reverser flaps | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12345206B2 | Propulsion assembly for an aircraft | Performing Operations; Transporting | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.