Stephane Rousselin
42Patents
10h-index
51Co-inventors
74Inventor score
Filing activity: Nov 10, 2005 → Mar 7, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8136999B2 | Turbomachine shaft guidance | Mechanical Engineering; Lighting; Heating | 22 | Active |
| US8209834B2 | Centering a part inside a shaft | Emerging Cross-Sectional Technologies | 20 | Active |
| US7372175B2 | Two-spool bypass turbojet with a rear electricity generator, and an air flow connection device and system | Emerging Cross-Sectional Technologies | 14 | Expired |
| US7224082B2 | Turbomachine including an integrated electricity generator | Emerging Cross-Sectional Technologies | 14 | Expired |
| US7685828B2 | Electricity generation in a turbomachine | Emerging Cross-Sectional Technologies | 14 | Active |
| US8246310B2 | Turbomachine fan | Emerging Cross-Sectional Technologies | 13 | Active |
| US8246255B2 | Device for the axial locking of a guide shaft bearing in a turbomachine | Emerging Cross-Sectional Technologies | 13 | Active |
| US8051952B2 | Deoiling device and turbomachine comprising this device | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US7390167B1 | Compressor with centripetal air takeoff | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US8074455B2 | Gas turbine engine with a means of driving the accessory gear box, and method of fitting said engine | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US7619331B2 | Turbomachine with integral generator/starter | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US7553126B2 | Device for varying the section of the throat in a turbine nozzle | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US7596938B2 | Turbomachine with a deflector system | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US8529208B2 | Rotary assembly for a turbomachine fan | Emerging Cross-Sectional Technologies | 6 | Active |
| US8172509B2 | Device for detecting breakage of a turbomachine shaft | Emerging Cross-Sectional Technologies | 6 | Active |
| US7334999B2 | Turbomachine rotor including at least one disk reinforced by a composite ring | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US8057160B2 | Device for limiting turbine overspeed in a turbomachine | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US7568336B2 | Aeroengine fitted with heat exchanger means | Emerging Cross-Sectional Technologies | 5 | Active |
| US9200594B2 | Gas turbine engine having fan blades of adjustable pitch with cyclic setting | Emerging Cross-Sectional Technologies | 5 | Active |
| US8127525B2 | System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US8882453B2 | Rotor element with a fluid passage and passage-blocking member and turbine engine including the rotor element | Emerging Cross-Sectional Technologies | 4 | Active |
| US7766607B2 | Device for ventilating turbine disks in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US8587780B2 | Device for measuring the twist of a rotating shaft | Physics | 3 | Active |
| US8182202B2 | Coupling device for a turbine upstream guide vane, a turbine comprising same, and aircraft engine fitted therewith | Emerging Cross-Sectional Technologies | 3 | Active |
| US7855483B2 | Turbomachine with integral generator/starter | Mechanical Engineering; Lighting; Heating | 3 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.