Guillaume Bulin
21Patents
6h-index
18Co-inventors
58Inventor score
Filing activity: May 14, 2007 → Oct 15, 2014
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8499822B2 | System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft | Emerging Cross-Sectional Technologies | 62 | Active |
| US8890343B2 | Electric generator disposed on a rotating turboprop part | Emerging Cross-Sectional Technologies | 38 | Active |
| US7818958B2 | Jet engine nacelle for an aircraft and aircraft comprising such a nacelle | Emerging Cross-Sectional Technologies | 12 | Active |
| US7703716B2 | Hinged device for doors of an aircraft nacelle and nacelle equipped with said hinged device | Performing Operations; Transporting | 10 | Active |
| US8677755B2 | Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method | Emerging Cross-Sectional Technologies | 9 | Active |
| US9175695B2 | Fluid-cooling device for a turbine engine propulsive unit | Emerging Cross-Sectional Technologies | 6 | Active |
| US8739516B2 | Turboreactor for aircraft | Emerging Cross-Sectional Technologies | 5 | Active |
| US8235657B2 | Turbojet for aircraft | Emerging Cross-Sectional Technologies | 5 | Active |
| US8381509B2 | Method and system for starting a turboshaft engine by cold weather | Emerging Cross-Sectional Technologies | 3 | Active |
| US8128022B2 | Device to handle and lock a cover of an aircraft nacelle | Performing Operations; Transporting | 3 | Active |
| US8684299B2 | Ancillary device with an air turbine for taxiing an aircraft on the ground | Emerging Cross-Sectional Technologies | 2 | Active |
| US8516792B2 | System for managing the heat fluxes of an aircraft | Emerging Cross-Sectional Technologies | 1 | Active |
| US8448420B2 | Aircraft nacelle that incorporates a device for reversing thrust | Emerging Cross-Sectional Technologies | 1 | Active |
| US8841584B2 | Electric deicing device for propfan-type propeller blades | Emerging Cross-Sectional Technologies | 1 | Active |
| US9643714B2 | Aircraft propulsion unit comprising a nacelle provided with a fan cowl locking and closing mechanism | Performing Operations; Transporting | 1 | Active |
| US8932016B2 | Deicing device for propfan-type propeller blades | Emerging Cross-Sectional Technologies | 0 | Active |
| US9821918B2 | Aircraft comprising a control device for a jet pipe nozzle with variable cross-section powered by two independent electrical power supplies | Emerging Cross-Sectional Technologies | 0 | Active |
| US8925295B2 | Air discharging device for an aircraft double-flow turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US9488131B2 | Device for controlling a variable section nozzle of an aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US8596037B2 | Nacelle with a displacement device for aircraft jet engine and aircraft including such nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US9657685B2 | Device for controlling a nozzle of variable cross-section of an aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.