Camel Serghine
28Patents
3h-index
36Co-inventors
55Inventor score
Filing activity: Jun 4, 2014 → Aug 13, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10662875B2 | Propulsion unit with selective coupling means | Emerging Cross-Sectional Technologies | 7 | Active |
| US9748060B2 | Hybrid cutoff member for an electric circuit | Electricity | 4 | Active |
| US9951694B2 | System and method for emergency starting of an aircraft turbomachine | Emerging Cross-Sectional Technologies | 3 | Active |
| US10151246B2 | Assistance device for a free-turbine engine of an aircraft having at least two free-turbine engines | Emerging Cross-Sectional Technologies | 2 | Active |
| US11085376B2 | Integration of a phase-change material for limiting the temperature of fuel from an electronic module | Emerging Cross-Sectional Technologies | 2 | Active |
| US10415482B2 | Turboshaft engine comprising a controlled mechanical coupling device, helicopter equipped with such a turboshaft engine, and method for optimising the zero-power super-idle speed of such a helicopter | Emerging Cross-Sectional Technologies | 2 | Active |
| US11316394B2 | Electrical machine of a turbomachine comprising a rotor cooled by a cooling channel | Electricity | 2 | Active |
| US10054053B2 | Turbomachine designed to operate in turning gear mode | Emerging Cross-Sectional Technologies | 2 | Active |
| US10422285B2 | Hydraulic device for emergency starting a turbine engine, propulsion system of a multi-engine helicopter provided with one such device, and corresponding helicopter | Emerging Cross-Sectional Technologies | 1 | Active |
| US10253699B2 | Device and method for testing the integrity of a helicopter turbine engine rapid restart system | Emerging Cross-Sectional Technologies | 1 | Active |
| US12424913B2 | Aircraft electrical machine with improved heat transfer by means of a phase change material and associated method | Electricity | 0 | Active |
| US11492975B2 | Pneumatic device for rapidly reactivating a turbine engine, architecture for a propulsion system of a multi-engine helicopter provided with such a device, and corresponding helicopter | Emerging Cross-Sectional Technologies | 0 | Active |
| US12009732B2 | Electrical machine winding having improved cooling | Electricity | 0 | Active |
| US12428130B2 | Propulsion unit with foldable propeller blades and method for folding the blades | Performing Operations; Transporting | 0 | Active |
| US11264854B2 | Electric machine with phase change material for a turbomachine starter/generator | Emerging Cross-Sectional Technologies | 0 | Active |
| US12391124B2 | Hybrid-electric propulsion architecture and method for dissipating electrical energy in such an architecture | Emerging Cross-Sectional Technologies | 0 | Active |
| US12304645B2 | Hybrid propulsion system and method for controlling such a system | Emerging Cross-Sectional Technologies | 0 | Active |
| US11876415B2 | Electric machine with device for forcibly demagnetising permanent magnets | General | 0 | Revoked |
| US11827374B2 | Multi-rotor aircraft propulsion system with reconfigurable electric network | Emerging Cross-Sectional Technologies | 0 | Active |
| US10753280B2 | Turbomachine designed to operate in turning gear mode | Emerging Cross-Sectional Technologies | 0 | Active |
| US11923736B2 | Electric machine with device for forcibly demagnetising permanent magnets | Electricity | 0 | Active |
| US11891907B2 | Turbogenerator for aircraft, comprising an improved oil system | Emerging Cross-Sectional Technologies | 0 | Active |
| US12043404B2 | Hybrid propulsion chain for an aircraft comprising an auxiliary mechanical drive system | Emerging Cross-Sectional Technologies | 0 | Active |
| US12097947B2 | Propulsion unit with foldable propeller blades and method for folding the blades | Performing Operations; Transporting | 0 | Active |
| US10858999B2 | Removable pack for reactivating a turboshaft engine, architecture for a multi-engine system for propelling a helicopter, provided with such a pack, and corresponding helicopter | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.