Pascal Gardes
23Patents
6h-index
32Co-inventors
69Inventor score
Filing activity: Aug 13, 2002 → Sep 29, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8740136B2 | Engine mount for an aircraft, to be placed between an engine and an engine mounting structure | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US6830970B2 | Inductance and via forming in a monolithic circuit | Electricity | 10 | Expired |
| US8561941B2 | Pin system for the connection assembly of an engine pylon underneath a wing of an aircraft | Emerging Cross-Sectional Technologies | 10 | Active |
| US7404249B2 | Method of manufacturing an inductance | Emerging Cross-Sectional Technologies | 9 | Expired |
| US6677657B2 | High-voltage periphery | Electricity | 6 | Expired |
| US10830089B2 | Turbofan comprising a series of rotatable blades for blocking off the bypass flow duct | Emerging Cross-Sectional Technologies | 6 | Active |
| US11193379B2 | Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct | Emerging Cross-Sectional Technologies | 3 | Active |
| US8256708B2 | Device for attaching an aircraft engine comprising a thrust force take-up device with a compact design | Performing Operations; Transporting | 2 | Active |
| US11220978B2 | Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct | Emerging Cross-Sectional Technologies | 2 | Active |
| US11255293B2 | Turbofan comprising a nacelle equipped with a reverser system and a mobile cascade grill | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US8167238B2 | Pylon caisson attachment on a wing, gripping a lateral panel of the caisson | Performing Operations; Transporting | 2 | Active |
| US7591958B2 | Thin glass chip for an electronic component and manufacturing method | Electricity | 2 | Active |
| US6884726B2 | Method for handling a thin silicon wafer | Electricity | 2 | Expired |
| US11105297B2 | Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct | Emerging Cross-Sectional Technologies | 1 | Active |
| US11215141B2 | Jet engine comprising a nacelle equipped with reverser flaps provided with vortex-generating means | 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 |
| US11136938B2 | Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports | Emerging Cross-Sectional Technologies | 0 | Active |
| US11274633B2 | Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct | Emerging Cross-Sectional Technologies | 0 | Active |
| US11565822B2 | Propulsion assembly for an aircraft, comprising a load support | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11161619B2 | Turbojet engine comprising a nacelle equipped with a fan case and with a fixed structure | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11473528B2 | Aircraft turbofan having a cowl articulated in rotation and a system for deploying said cowl | Emerging Cross-Sectional Technologies | 0 | Active |
| US11401886B2 | Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11359542B2 | Turbofan engine comprising a set of rotatable blades for blocking off the bypass flow duct and redirecting the air flow | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.